The present disclosure relates to an electrical connector system, more specifically a relatively small connector system having a male connector assembly and a female connector assembly. The male connector assembly includes a male housing assembly and a male terminal assembly having a male terminal, a spring member with at least one contact arm with a bent segment and an openable enclosure jacket. The male terminal assembly also includes a compression limiting means that prevents an external force from overly deforming the contact arm inward. Preventing excessive depression of the contact arm is desirable because it can damage the contact arm and/or the spring member thereby introducing a failure mode to the male connector assembly that can cause the overall connector system to become inoperable and unusable.
Over the past several decades, the number of electrical components used in automobiles, and other on-road and off-road vehicles such as pick-up trucks, commercial vans and trucks, semi-trucks, motorcycles, all-terrain vehicles, and sports utility vehicles (collectively “motor vehicles”) has increased dramatically. Electrical components are used in motor vehicles for a variety of reasons, including but not limited to, monitoring, improving and/or controlling vehicle performance, emissions, safety and creates comforts to the occupants of the motor vehicles. Considerable time, resources, and energy have been expended to develop power distribution components that meet the varied needs and complexities of the motor vehicle market; however, conventional power distribution components suffer from a variety of shortcomings.
Motor vehicles are challenging electrical environments for both the electrical components and the connector assemblies due to several conditions, including but not limited to, space constraints that make initial installation difficult, harsh operating conditions, large ambient temperature ranges, prolonged vibration, heat loads, and longevity, all of which can lead to component and/or connector failure. For example, incorrectly installed connectors, which typically occur in the assembly plant, and dislodged connectors, which typically occur in the field, are two significant failure modes for the electrical components and motor vehicles. Each of these failure modes leads to significant repair and warranty costs. For example, the combined annual accrual for warranty by all of the automotive manufacturers and their direct suppliers is estimated to be between $50 billion and $150 billion, worldwide. In light of these challenging electrical environments, considerable time, money, and energy have been expended to find power distribution components that meet the needs of the markets. This disclosure addresses the shortcomings of conventional power distribution components. A full discussion of the features and advantages of the present disclosure is deferred to the following detailed description, which proceeds with reference to the accompanying drawings.
The present disclosure relates to an electrical connector system having a male connector assembly and a female connector assembly. The male connector assembly includes a male housing assembly and a male terminal assembly having a male terminal, a spring member with at least one contact arm with a significantly bent configuration and an openable jacket that encloses a substantial extent of the male terminal and the spring member. The male terminal assembly also includes a compression limiting means that prevents an external force from overly deforming the contact arm inward. Preventing excessive depression of the contact arm is desirable because it can damage the contact arm and/or the spring member thereby introducing a failure mode to the male connector assembly that can cause the overall connector system to become inoperable and unusable.
According to another aspect, the female connector assembly includes a female housing assembly and a female terminal assembly. The female housing assembly includes a side wall arrangement that is designed to receive the female terminal assembly and thereby facilitate coupling of the male terminal assembly with the female terminal assembly. Also, the female housing assembly minimizes the chance that a foreign object accidentally makes contact with the female terminal assembly and provide a failure mode that can cause the overall connector system to become inoperable and unusable.
Other aspects and advantages of the present disclosure will become apparent upon consideration of the following detailed description and the attached drawings wherein like numerals designate like structures throughout the specification.
The accompanying drawings, which are included to provide further understanding and are incorporated in and constitute a part of this specification, illustrate disclosed embodiments and together with the description serve to explain the principles of the disclosed embodiments. In the drawings:
In the following detailed description, numerous specific details are set forth by way of examples in order to provide a thorough understanding of the relevant teachings. However, it should be apparent to those skilled in the art that the present teachings may be practiced without such details. In other instances, well-known methods, procedures, components, and/or circuitry have been described at a relatively high-level, without detail, in order to avoid unnecessarily obscuring aspects of the present teachings.
While this disclosure includes several embodiments in many different forms, it should be understood that the present disclosure is to be considered as an exemplification of the principles of the disclosed methods and systems, and is not intended to limit the broad aspects of the disclosed concepts to the embodiments illustrated. As will be realized, the disclosed methods and systems are capable of other and different configurations and several details are capable of being modified without departing from the scope of the disclosed methods and systems. For example, one or more of the following embodiments, in part or whole, may be combined consistently with other disclosed methods and systems. Accordingly, the drawings and detailed descriptions are to be regarded as illustrative in nature, not restrictive or limiting.
The Figures show seven embodiments of a connector system 10, 1010, 2010, 3010, 4010, 5010, 6010 or components thereof designed to mechanically and electrically couple one device or component to another device or component within a power distribution system or environment. For example, a first device or component can be removable coupled to a second device or component via the connector system 10. The first device or component may be a current supplying device or component—such as charge coupler 2 (see
Various aspects of a first embodiment of the connector system 10 are explained in greater detail below. In general terms, the connector system 10 comprises: (i) a male connector assembly 50, and (ii) a female connector assembly 650.
The various seven embodiments of the connector system 10 provide numerous improvements over conventional connectors. With regard to the first embodiment, these improvements include: (i) a male terminal body 104 that includes a base portion 110 and at least one contact arm 180a-180d with a portion 182a-182d that is substantially co-planar with said base portion 110, (ii) a male terminal body 104 with an anti-rotation projection 114, which is configured to help prevent the spring member 300 from rotating within the receptacle 105, (iii) the contact arms 180a-180d have a geometric bent or creased portion 178a-178d with a free end 190a-190d that does not abut a planar outer surface of the spring arms 312a-312d, when the spring member 300 is positioned in the receptacle 105, (iv) the male terminal body 104 and the spring member 300 are configured in a manner that prevents the spring member 300 from being inserted into the receptacle 105 when the contact arms 180a-180d are in the ready to use position PU because the bent or creased portion 320a-320d of the spring member 300 would contact and engage (e.g., get snagged on) the free ends 190a-190d of the contact arms 180a-180d, (v) a separate spring member 300 with a geometric bent or creased portion 320a-320d of the spring arms 312a, 312b, (vi) a male terminal assembly 100 with means for limiting compression 314 of the contact arms 180a-180d that could lead to damage of the male terminal assembly 100, (vii) a spring member 300 with two spring arms 312a-312d, wherein the width of one spring arm 312a increases, between two points, such as along its length while the width of the second spring arm 312b decreases, between two points, such as along its length, (viii) a jacket 400 that includes spring openings 434a,434b formed in a frontal jacket segment 430, which are configured to receive an extent of the spring member 300, (ix) the jacket 400 including an arrangement of deflecting projections 418 that are configured to engage the contact arm 180a-d, as discussed below. While the foregoing list includes some of the numerous improvements that are included in the first embodiment of the connector system 10, it should be understood that other improvements are disclosed herein and that each and every improvement disclosed herein is not necessary or essential to the configuration, operation, or functionality of the disclosed connector system 10. Other similar embodiments of the connector system 10 are disclosed in
Various aspects of a fourth embodiment of the connector system 3010 are disclosed herein and shown in
Various aspects of a seventh embodiment of the connector system 6010 are disclosed herein and shown in
The male connector assembly 50 includes multiple components designed to be coupled to a separate device or component (e.g., charge coupler 2, radiator fan, heated seat, power distribution component, or another current drawing component). The male connector assembly 50 is primarily composed of: (i) the male housing assembly 70, and (ii) the male terminal assembly 100 with the male terminal 101, spring member 300, and jacket 400, wherein during operation of the connector system 10 at least a substantial extent of the male terminal assembly 100 resides within the male housing assembly 70.
a. Male Housing Assembly
Referring to
The external arrangement of side walls 76 includes: (i) two opposed side walls 78a, 78b with a plurality of projections 80 and recesses 82, (ii) a curvilinear bottom wall 78c that extends between the opposed side walls 78a, 78b, and (iii) a deformable top wall 78d with a female receiver opening 84 formed therethrough. Each of the walls 78a-78d are spaced a housing distance DH away (shown in
Rearward of wall plane PW (shown in
When the connector assembly 50 is in the fully coupled state, SFC: (i) the locking tabs 426 of the jacket 400 are positioned forward of the retaining wall surfaces 90, (ii) the retaining body 96 is positioned adjacent a first extent of the connector arrangement of side walls 86, and the securing projections 97a, 97b are positioned below an opposed second extent of the connector arrangement of side walls 86, and (iii) the retaining projections 98a, 98b extend into the retaining opening 95, and are positioned rearward of the male terminal body 104. This configuration of structures helps prevent rearward movement of the male terminal assembly 100, while securing the male terminal assembly in the housing 70. In fact, this combination ensures a force that is less than 200 Newtons will not dislodge the male terminal assembly 100 from the housing 70. The combination of the recesses 698, 82, projections 80, 697 forms a system 10 with keyed configuration, wherein the male connector assembly 50 can only mate with the female connector assembly 650 when the male connector assembly 50 is in a specific orientation relative to the female connector assembly 650.
The male housing assembly 70 is formed from a non-conductive plastic and is designed to protect and isolate the conductive male terminal assembly 100 from accidental contact with foreign objects. In other embodiments, the male terminal retaining means 94 may be replaced with any structure that would perform a similar function and is disclosed in any application incorporated herein by reference. Some of these structures may include other types of mechanical/structural members or bodies that generate a biasing force on the male terminal assembly 100, magnets, springs, or other types of retaining means. In further embodiments, the housing 70 may include: (i) a connector position assurance (CPA) assembly that includes a readable or scannable indicia, which meets USCAR Specifications, including USCAR-12, USCAR-25, and USCAR-2, (ii) an EMI shield, (iii) additional layers of non-conductive and/or conductive materials, and/or (iv) a larger footprint (e.g., charge coupler 2) to accept multiple male terminal assemblies 50. Other similar male housing assemblies are disclosed in applications incorporated herein by reference, and features of these housing assemblies may be incorporated into the male housing assembly 70 of the male connector assembly 50 disclosed herein.
b. Male Terminal Assembly
i. Means for Limiting Compression
Unlike conventional male terminal assemblies, the male terminal assembly 100 disclosed herein includes the means for limiting compression 314. Said means for limiting compression 314 is designed to prevent an external force FE from excessively deforming or overly depressing the contact arms 180a-180d and the spring arm 316a-316d toward the center of the connector 50. Prevention of excessive deformation or depression of the contact arm 180a-180d and the spring arm 312-312d is desirable because said deformation or depression can damage the contact arm 180a-180d, the spring member 312a-312d, or a combination of the contact arm 180a-180d and the spring member 312a-312d to a point that the terminal assembly 100 becomes damaged, inoperable and/or unusable. Thus, said means for limiting compression 314 reduces this potential failure mode of the terminal assembly 100. While reducing this potential failure mode is beneficial, it should be understood that means for limiting compression 314 should not interfere with normal or operational deformation DNC (see
ii. Male Terminal
In particular,
The above described interior spring wall 108e is positioned within said base or intermediate portion 110 and includes a frontal surface 112 configured to be positioned adjacent to a rear surface of the spring member 300 (when the spring member is positioned within the male terminal body 104). The frontal surface 112 of the interior spring wall 108e is not co-planar but has a staggered configuration. In other words, the interior spring wall 108e includes a recess that forms an anti-rotation projection 114. As best shown in
The side walls 108b, 108d, top wall 108a, and bottom wall 108c each include the following structure/anti-structures that extend forward from the second base plane PB2: (i) at least one contact arm 180a-180d with two primary portions 182a-182d and 178a-178d, and preferably a plurality of contact arms 180a-180d, (ii) supporting ribs 116a-116c, and (iii) contact arm gaps or voids 120a-120g that are positioned between either the contact arms 180a-180d and the adjacent supporting rib 116a-116c or adjacent contact arms 180a, 180d, wherein the supporting ribs 116a-c have an overall length that is less than an overall length of the contact arms 180a-d. This configuration creates multiple structure/anti-structures within the side walls 108b, 108d, top wall 108a, and bottom wall 108c, wherein said structure/anti-structures may include seven distinct structure/anti-structures integrally formed (i.e., not separate) with one another. For example, the bottom wall 108c includes: (i) a geometric bent or creased portion 178c, (ii) a first, rear, or linear extent 182c of a contact arm 180c, (iii) a portion of a second supporting rib 116b, (iv) a portion of a third supporting rib 116c, (v) a fourth contact arm gap or void 120d, (vi) a fifth contact arm gap or void 120e, and (vii) an extent of the base or intermediate portion 110.
The contact arm voids 120a-120g are formed in the walls 108a-108d and delineate the contact arms 180a-180d and the supporting ribs 116a-116c. For example, the second contact arm void 120b is positioned between the first supporting rib 116a and the second contact arm 180b, while the third contact arm void 120c is positioned between the second contact arm 180b and the second supporting rib 116b. The male terminal body 104 only includes three supporting ribs 116-116c. In other words, the male terminal body 104 lacks a supporting rib positioned adjacent to the top wall 108a and the second side wall 108d. Said body 104 lacks this supporting rib due to the configuration/formation of the interior spring wall 108e. The supporting ribs 116a-116c include three segments, which include a first linear segment, a curvilinear segment, and a second linear segment. The first and second linear segments are substantially co-planar with the associated wall 108a-108d. This configuration allows the supporting ribs 116a-116c to be extend around the corners of the male terminal body 104.
Said supporting ribs 116a-116c extend from base portion 100 (second base plane PB2), along the first or rear extent 182a-182d of a contact arm 180a-180d, but do not extend along the geometric bent or creased portion 178c of the contact arms 180a-180d. In other words, the distal ends 118a-118c of the supporting ribs 116a-116c are not positioned forward of a bend plane PB corresponding to the bend portion 178c. As shown in the Figures, the distal ends 118a-118c of the supporting ribs 116a-116c are not connected to one another or any other structures. Accordingly, the length of said supporting ribs 116a-116c has been determined by balancing: (i) too long they will not provide adequate support to the contact arms 180a-180d and/or jacket 400 at or near the distal ends 118a-118c of the supporting ribs 116a-116c, and (ii) too short they will not provide adequate support to the contact arms 180a-180d and/or jacket 400. Nevertheless, in other embodiment, the supporting ribs 116a-116c may be lengthened to extend along the entire contact arm 180a-180d, shortened to only extend along a portion of the first or rear extent 182a-182d of a contact arm 180a-180d, an additional supporting rib may be added between contact arms 180c and 180d, or omitted in their entirety.
As best shown in
Referring specifically
Unlike conventional connectors, the disclosed contact arms 180a-180d have an elongated first or rear extent 182a-182d that does not extend away from the base portion 110 at a uniform outward sloping angle or substantially uniform outward sloping angle. In other words and as best shown in
As shown in
As discussed in greater detail below, the third or downwardly sloping extent 188a-188d, and specifically the contact surface 189a-189d, is configured to contact an extent of the female connector assembly 650 when the male terminal assembly 100 is inserted into the female terminal assembly 700. This interaction between these components causes the contact arms 180a-180d to be deflected or displaced inward and towards the center of the male terminal assembly 100 and the spring member 700. This inward deflection of the contact arms 180a-180d causes the spring member 700 to act as a wedge to help ensure that a proper mechanical and electrical connection is created between the contact arms 180a-180d and the female receptacle 702.
As shown in
As shown in
The male terminal 101 is typically formed from a single piece of material (e.g., metal); thus, the male terminal 101 is a one-piece male terminal 101 and has integrally formed features. To integrally form these features, the male terminal 101 is typically formed using a die-cutting process. However, it should be understood that other types of forming the male terminal 101 may be utilized, such as casting or using an additive manufacturing process (e.g., 3D printing). In other embodiments, the features of the male terminal 101 may not be formed from a one-piece or be integrally formed, but instead formed from separate pieces that are welded together. In forming the male terminal 101, it should be understood that any number (e.g., between 1 and 100) of contact arms 180a-180d may be formed within the male terminal 101. The male terminal 101, male terminal body 104, the contact arms 180a-180d, or an extent of the contact arms 180a-180d may be plated or coated with a secondary material (e.g., nickel) to help reduce corrosion, reduce insertion forces, or improve conductivity. Additionally, the contact arms 180a-180d or a portion of the contact arms 180a-180d may have rounded or beveled edges.
iii. Spring Member
Unlike conventional spring members, the spring member 300 disclosed herein includes a spring arm 312a-312d with a geometry that substantially matches the geometry of the associated contact arm 180a-180d. In other words, the spring arms 312a-312d include a geometric bent or creased portions 320a-320d that substantially matches the geometric bent or creased portions 178a-178d of the contact arms 180a-180d. In addition to the geometric bent or creased portions 320a-320d, the spring member 300 is unique due to its inclusion of: (i) a first pair or primary pair of spring arms, which include the top, primary, or first spring arm 312a and the bottom or third spring arm 312c, (ii) a second pair or secondary pair of spring arms, which include the first side spring arm, secondary spring arm, or second spring arm 312b and a second side spring arm or fourth spring arm 312d. The geometry of the top and bottom spring arms 312a, 312c substantially mirror one another, and the geometry of the first side and second side spring arms 312b, 312d substantially mirror one another. Additionally, the geometry of the spring arms contained in the first pair of spring arms (top and bottom spring arms 312a, 312c) does not match the geometry of the spring arms contained in the second pair of spring arms (side spring arms 312b, 312d).
The top and bottom spring arms 312a, 312c include: (i) the initial or linear base extent 316a, 316c that extends from the first or curvilinear spring section 308a, 308c (line S2) to a second or upwardly sloping extent 322a, 322c (line S3), and (ii) a geometric bent or creased portion 320a, 320c extends forward from the initial or linear extent 316a, 316c (line S3). Said geometric bent or creased portion 320a, 320c includes: (i) the second or upwardly sloping extent 322a, 322c that extends between the initial extent 316a, 316c (line S3) and an exterior apex 324a, 324c (line S4) of the spring arm 312a, 312c, (ii) a third or downwardly sloping extent 326a, 326c that extends downward from an external apex 324a, 324c (line S4) to an over-compression extent 328a, 328c (line S5), and (iii) the over-compression extent 328a, 328c extending between the third or downwardly sloping extent 326a, 326c (line S5) and a forward-most extent that provides a frontal end 330a, 330c. The geometric bent or creased portion 320a, 320c of the spring arms 312a, 312c is configured to complement the geometric bent or creased portion 178a, 178c of the contact arm 180a, 180c.
As shown in
This configuration allows a majority of creased portion 320a, 320c to have a width that substantially match the width of the creased portion 178a, 178c. Matching the widths of the spring arm 312a, 312c and contact arms 180a, 180c at the point the male terminal assembly 100 is configured to contact the female terminal assembly 700 is beneficial because it limits the width required for contact arm openings 414, 470 that are formed in the jacket 400 and male terminal housing 70. Additionally, including additional material to the spring member 300 in a location that is substantially rearward of the creased portion 178a, 178c of the contact arms 180a, 180c allows the designer to increase the force required to deform the spring arms 312a, 312c in comparison to a spring member that lacked this additional material. Nevertheless, it should be understood that in other embodiments, the width of the spring arms 312a, 312c may be constant along the entire length of the arm 312a, 312c, have only two different widths, or may have more than the disclosed number of widths.
The side spring arms 312b, 312d include: (i) the initial or linear extent 316b 316d that extends from the first or curvilinear spring section 308b, 308d (line S2) to a second or upwardly sloping extent 322b, 322d (line S3), and (ii) a geometric bent or creased portion 320b, 320d extends forward from the initial or linear extent 316b, 316d (line S3). Said geometric bent or creased portion 320b, 320d includes: (i) the second or upwardly sloping extent 322b, 322d that extends between the initial extent 316b, 316d (line S3) and an exterior apex 324b, 324d (line S4) of the spring arm 312b, 312d, (ii) a third or downwardly sloping extent 326b, 326d that extends downward from an external apex 324b, 324d (line S4) to a fourth extent, jacket extent, or jacket projection extent 329b, 329d (line S6), and (iii) the jacket extent 329b, 329d extending forward from the third or downwardly sloping extent 326b, 326d (line S6) to a free-end 330b, 330d. The geometric bent or creased portion 320b, 320d of the spring arms 312b, 312d is configured to complement the geometric bent or creased portion 178b, 178d of the contact arm 180b, 180d.
As shown in
Unlike conventional spring, the disclosed spring member includes spring arms 312a-312d with three unique or different widths. In this embodiment, the spring member 300 includes two spring arms 312a, 312b, wherein the width of one spring arm 312a increases, between two points (e.g., 336a-336b, 340a-340b), along its length and the width of the second spring arm 312b decreases, between two points (e.g., 332a-332b, 334a-334b), along its length. Additionally, the spring member 300 has: (i) the first and fourth spring arm widths W1SA. W4SA are equal, (ii) second and fifth spring arm widths W2SA, W5SA are equal, (iii) the first and fourth spring arm widths W1SA, W4SA are larger than the second and fifth spring arm widths W2SA, W5SA, and (iii) the third spring arm width W3SA is larger than the first, second, fourth, and fifth spring arm widths W1SA, W2SA, W4SA, W5SA. In other words, the widths of the curvilinear spring sections 308a-308d and linear extents 316a-316d of the spring member 300 are substantially equal, the widths of the downwardly sloping extents 326a-326d are substantially equal, and the widths of the over-compression extents 328a, 328c is not equal (i.e., greater than) to the jacket extents 329b, 329d.
Unlike conventional spring members, the spring member 300 includes a first portion of the means for limiting compression 314. Said first portion of the means for limiting compression 314 is the first combination of limiting structures 315a, which include: (i) the over-compression extent 328a, 328c, and (ii) edges of the adjacent side spring arms 312b, 312d. The over-compression extent 328a, 328c has opposed flanges that extend outwardly and transversely from the downwardly sloping extent 326a, 326c and that define an over-compression spring arm width W3SA that is larger than other spring arms widths (e.g., first, second, fourth, and fifth). In fact, the over-compression width W3SA is larger than the inner surface width W1S that extends between inner surfaces 342a of the jacket extends 329b, 329d of the side spring arms 312b, 312d. As such, the outer edge 340a, 340b the over-compression extent 328a, 328c are positioned outside or beyond the inner surfaces 342a of the side spring arms 312b, 312d. Additionally, the outer edge 340a, 340b of the over-compression extents 328a, 328c are positioned outside or beyond the inner surfaces 346 of the linear extent 316b, 316d of the side spring arms 312b, 312d. The application of an external force FE on the contact arms 180a, 180c can only deform the contact arms 180a, 180c, to the max compression distance DMC because the frontal end 330a, 330c contacts the forward spring arm edges 334a, 334b of the side spring arms 312b, 312d. In this embodiment the max compression distance DMC is less than 1.25 mm, preferably less than 1.0 mm, and most preferably 0.5 mm. Limiting the extent the contact arms 180a, 180c can be deformed or depressed to the max compression distance DMC prevents the contact arms 180a, 180c, spring arms 312a, 312c, and a combination thereof helps prevent said arms 180a, 180c from being overly deformed or depressed (e.g., a distance that is greater than the max compression distance DMC) toward the center of the connector 50. While said first combination of limiting structures 315a provides this beneficial features, it should be understood that structures 315a are configured in a manner to ensure they do not interfere with normal or operational deformation (see
As shown in
The spring member 300 is typically formed from a single piece of material (e.g., metal); thus, the spring member 300 has a one-piece construction with integrally formed components. In particular, the following features are integrally formed: (i) the curvilinear spring section 308a-308d, and (ii) the spring arm 312a-312d. To integrally form these features, the spring member 300 is typically fabricated using a die forming process. that mechanically forces the spring member 300 into shape. As discussed in greater detail below and in PCT/US2019/036010, when the spring member 300 is formed from a flat sheet of metal (as shown in
Positioning the spring member 300 within the male terminal 101 occurs across multiple steps or stages (see
The first partially assembled state, S1PA is shown in
Other unique features of this system 10 can be seen once the male terminal 101 and the spring member 300 are in the second partially assembled state, S2PA. For example, the free ends 190a-190d of the contact arms 180a-180d do not abut a planar outer surface 313a-313d of the spring arms 312a-312d. Instead, the entirety of the contact arms 180a-180d are supported by the spring arms 312a-312d, such that the system 10 lacks a substantial gap formed between the outer surface 313a-313d of the spring arms 312a-312d and the inner surface of the contact arms 180a-180d. Omitting the gap between these structures and positioning the spring arm 312a-312d in this manner allows a majority of the outer surface 2313a-2313d of the spring arm 312a-312d to underlie and abut an inner surface of the contact arm 180a-180d. It should be understood that a minor/insubstantial gap may be formed between the outer surface 313a-313d of the spring arms 312a-312d and the inner surface of the contact arms 180a-180d due to manufacturing capabilities and restraints due to the movement of the male terminal body 104 from the ready to receive position PR and ready to use position PU. This positional arrangement causes the disclosed system 10 to apply the spring biasing force FSB in a different manner than how the spring biasing force FSB is applied in fourth, fifth, sixth, and seventh embodiments of the systems 3010, 4010, 5010, and 6010 disclosed here. Specifically, the spring members 3300, 4300, 5300, 6300 in these other embodiments of the systems 3010, 4010, 5010, and 6010 apply the spring biasing force FSB on one (or possible two) locations and in a direction that is substantially perpendicular to a majority of an outer surface of the spring member 300. In contrast, the disclosed spring member 300 does not: (i) apply the spring biasing force FSB one (or possible two) locations, nor (ii) apply the spring biasing force FSB in a direction that is substantially perpendicular to a majority of an outer surface of the spring member 300.
iv. Jacket
The jacket 400 is configured to surround a majority of the male terminal body 104 and provide an arrangement of contact arm deflecting projections 418. The upper and lower segments 402, 460 of the jacket 400, each include a wall arrangement 404, 462 having a U-shaped configuration. In particular, the wall arrangement 404 of the upper segment 402 includes: (i) a top wall 406, and (ii) opposed side walls 408a, 408b. The opposed side walls 408a, 408b include: (i) a number of securement features 410 that are designed to secure the jacket 400 to the male terminal body 102, (ii) at least one contact arm deflecting projection 420 that is configured to protect front and/or rear extents of the contact arms 180a, 180b, 180d, (iii) contact arm recess 424, and (iv) opposed locking tabs 426. In this embodiment, said securement features 410 include a plurality of depressions 412a-412d with internal apexes 413a-413d that are configured to make contact with the side walls of the male terminal body 104. Said contact between the upper segment 402 and the side walls of the male terminal body 104 ensure the formation of a proper electrical connection between the jacket 400 and the male terminal body 104, whereby preventing possible arcing due to intermediate connections. In other embodiments, the plurality of depressions 412a-412d may be replaced with another means designed to secure the jacket 400 to the body 104 and prevent possible arcing. Said means may include welding or forming the jacket as a part of the male terminal body 102. The locking tabs 426 are formed from an extent of the side walls 408a, 408b and are a part of the male terminal retaining means 94. As discussed above, the locking tabs 426 are configured to be positioned in front of the retaining wall surfaces 90 of the male housing assembly 70, when the male connector assembly 50 is in the coupled state SC. The contact arm recess 424 extends upward from a lower edge of the opposed side walls 408a, 408b and is designed to ensure that the jacket 400 does not interfere with the operation or assembly of the male terminal 100. Adjacent to the contact arm recess 424 is a deflecting projection 420, wherein said projection 420 is positioned between recess 424 and a rear extent of the male terminal 101.
The top wall 406 extends between the opposed side walls 408a, 408b and includes: (i) securement features 410, (ii) a contact arm opening 414, and (iii) a plurality of deflecting projections 420. The contact arm opening 414 is configured to receive an extent of the contact arm 180a-180d, when the male terminal assembly is in the assembled state SA. The front and back of the contact arm opening 414 are flanked by deflecting projections 420. Said deflecting projections 420 extend at an outward angle from the jacket 400 (more particularity, the top wall 406) and have an upper edge that is positioned below the apex 186a-186d of the associated contact arm 180a-180d. The deflecting projections 420 are designed to: (i) help protect the contact arm 180a-180d from external impact forces FIE that may damage said contact arm 180a, 180b, 180d, and (ii) ensure that they do not interfere with the movement of the contact arms 180a-180d during operation of the connector system 10. This embodiment includes: (i) a first deflecting projection 420 positioned: (a) adjacent to the contact arm opening 414, and (b) between a frontal edge of the contact arm opening 414 and the frontal segment 430 of the jacket 400, and (ii) a second deflecting projections 420 positioned: (i) adjacent to the contact arm opening 414, and (ii) between a rear edge of the contact arm opening 414 and the rear extent of the jacket 400. The angle between the outer surface of the top wall 406 of the jacket 400 and the outer surface of the first deflecting projections 420 is approximately equal to the angle formed between a plane that is parallel with the top wall 108a of the male terminal body 104 and the third or downwardly sloping extent 188a-188d of the contact arms 180a-180d. The angle between the outer surface of the top wall 406 of the jacket 400 and the outer surface of the second deflecting projections 420 is approximately equal to the angle formed between a plane that is parallel with the top wall 108a of the male terminal body 104 and the second or upwardly sloping extent 184a-184d of the contact arms 180a-180d. It should be understood that in other embodiments, the deflecting projections 420 may be formed in the male terminal housing 70, may be omitted, there length may be increased or decreased, or may include peripheral supports designed to support the outer edges of the deflecting projections 420. In addition to these features, the securement features 410 formed in the top wall 106 include: (i) an additional or top wall depression 412e, and (ii) a rear retaining tab 416 designed to wrap around an extent of the male terminal body 104 to secure said jacket 400 to said body 104 (see
The jacket's 400 frontal segment 430 includes: (i) a frontal wall 432 with spring arm openings 434a, 434b formed there through, and (ii) contact arm deflecting projections 440 configured to protect a front extent of the contact arms 180b, 180d. As will be described in greater detail below, the spring arm openings 434a, 434b are configured to receive an extent of the spring member 400 (i.e., jacket extent 329b, 329d) in order to help prevent over-compression of the contact arms 180b, 180d. Like the upper and lower segments 402 and 462, said deflecting projections 440 extend at an outward angle from the jacket 400 (more particularity, an extent of the frontal wall 432) and are designed to help protect the contact arm 180a-180d from the external impact forces FIE that may damage said contact arm 180a-180d.
The jacket's 400 wall arrangement 462 of the lower segment 460 includes: (i) a bottom wall 466, and (ii) opposed side walls 468a, 468b. The bottom wall 466 extends between the opposed side walls 468a, 468b and includes: (i) contact arm opening 470, (ii) contact arm deflecting projections 480 that are configured to protect front and rear extents of the contact arms 180c, and (iii) securement features 410. The contact arm opening 470 is configured to receive an extent of the contact arm 180a-180d, when the male terminal assembly is in the assembled state SA. The front and back of the contact arm opening 470 are flanked by deflecting projections 480. Said deflecting projections 480 extend at an outward angle from the jacket 400 (more particularity, the bottom wall 466) and are designed to help protect the contact arm 180a-180d from the external impact forces FIE that may damage said contact arm 180a-180d. In this embodiment: (i) a first deflecting projections 480 is positioned: (a) adjacent to the contact arm opening 470, and (b) between a frontal edge of the contact arm opening 470 and the frontal segment 430 of the jacket 400, and (ii) a second deflecting projections 480 is positioned: (i) adjacent to the contact arm opening 470, and (ii) between a rear edge of the contact arm opening 470 and the rear extent of the jacket 400. The angle between the outer surface of the bottom wall 466 of the jacket 400 and the outer surface of the first deflecting projections 480 is approximately equal to the angle formed between a plane that is parallel with the top wall 108c of the male terminal body 104 and the third or downwardly sloping extent 188a-188d of the contact arms 180a-180d. The angle between the outer surface of the bottom wall 466 of the jacket 400 and the outer surface of the second deflecting projections 480 is approximately equal to the angle formed between a plane that is parallel with the bottom wall 108c of the male terminal body 104 and the second or upwardly sloping extent 184a-184d of the contact arms 180a-180d. In addition to these deflecting projections 480, the securement features 410 formed in the bottom wall 106 include a plurality of peripheral retaining tabs 474, which are designed to wrap around an extent of the male terminal body 104 to secure said jacket 400 to said body 104 (see
Moving the male terminal assembly from the third partially assembled state, S3PA to the fully coupled state, SFC occurs across multiple steps or stages. First, the male terminal assembly must move from the third partially assembled state, S3PA to an assembled state before the assembler can move the connector to the coupled state SC.
Next, as shown in
Unlike conventional connector assemblies, the disclosed male terminal assembly 100 includes the means for limiting compression 314. Said means for limiting compression 314 is further comprised of the second combination of limiting structures 315b, which is formed from the interaction between structures contained in two separate components (i.e., spring member 300 and jacket 400). In other words, positing the jacket extent 329b, 329d of the spring member 300 in the spring arm openings 434a, 434b formed in the jacket 400 will provide said second combination of limiting structures 315a (see
Finally, as shown in
The female connector assembly 650 is comprised of: (i) the female housing assembly 670 and (ii) the female terminal assembly 700.
a. Female Housing Assembly
The female housing assembly 670 is designed to: (i) receive the female terminal assembly 700, (ii) facilitate the coupling of the male terminal assembly 100 with the female terminal assembly 700, (iii) minimize the chance that a foreign object accidentally makes contact with the female terminal assembly 700, and (iv) meet industry standards, such as USCAR specifications. The female housing assembly 670 includes a sidewall 672 having a configuration that substantially matches the configuration of the female terminal assembly 700. In the embodiment shown in the figures, the female terminal assembly 700 has a cuboidal configuration, and preferably a rectanguloid configuration to match the rectanguloid of the male terminal assembly 100. The sidewall 672 of the female housing assembly 670 also includes a plurality of projections 697 configured to be received by the recesses 82, and the projections 80 are configured to be received by the recesses 698. Finally, the female housing assembly 670 includes coupling projection 699, which is design to interact with the female receiver opening 84 of the male housing assembly 70. The female housing assembly 670 also includes a female terminal retaining means 690 that includes: (i) a retaining body 692, (ii) retaining openings 694 formed in the sidewall 672 of the female housing assembly 670, and (iii) terminal body projection receiver 961. The retaining body 692 is a U-shaped structure that includes retaining projections 696 that extend downward from the upper crossing member that extends between the legs of the U-shaped structure. When the assembly 650 is in the fully coupled state, SFC: (i) the retaining body 692 is positioned adjacent an extent of the sidewall 672, (ii) the retaining projection 696 extend into the retaining opening 694, and are positioned rearward of the male terminal body 104, and (iii) the terminal body projection 713 is positioned in the terminal body projection receiver 691.
The sidewall 672 of the female housing assembly 670 extends past the upper most surface of the female terminal assembly 700 to allow for the formation of a male compression means 674 in an extent of the sidewall 672. As shown in the Figures, the male compression means 674 is a sloped or ramped surface 676 that extends from an outermost edge 673 of the sidewall 672 to the upper most edge 700a of the female terminal assembly 700. In the disclosed embodiment, the sloped or ramped surface 676 extends from each of the outermost edge 673 and has a substantially linear configuration. However, it should be understood that the sloped or ramped surface 676 may only extend from a portion of the outermost edge 673. The male compression means 674, shown as the sloped or ramped surface 676, is designed to compress the contact arms 180a-180d as the male terminal assembly 100 moves from being separated from the female terminal assembly 700 in a disconnected state SDC to being positioned within an extent of the female terminal assembly 700 in a connected state SC (see
This sloped or ramped surface 676 is made from a polymer or plastic material and, as such has a coefficient of friction that is lower than a coefficient of friction associated with a metal surface. In other words, a first friction value is formed when the extent (e.g., a contact arm 180a-180d) of the male terminal assembly 100 engages with a male terminal compression means 674 formed from a non-metallic material (e.g., plastic). In an alternative embodiment, a second friction value would be formed if the extent (e.g., a contact arm 180a-180d) of the male terminal assembly 100 was to engage with a male terminal compression means formed from a metallic material (e.g., copper). Comparing the friction value from the disclosed embodiment to the friction value alternative embodiment, it should be understood that the first or friction value from the disclosed embodiment is less than the second or friction value alternative embodiment.
The lower coefficient of friction reduces the force that is required to insert the male terminal assembly 100 into the female terminal assembly 700. This is beneficial because: (i) industry specifications, including USCAR 25, has requirements that the insertion force F1 cannot be greater than 45 Newtons for a class 2 connector and 75 Newtons for a class 3 connector and (ii) the use of a greater spring biasing force FSB, which thereby increases the insertion force F1, is desirable to help ensure that the contact arms of the male terminal assembly remain in contact with the inner surface 704 of the receptacle 702 of the female terminal assembly 700. Further, this lower coefficient of friction is beneficial because the connector system 10 can move from the disconnected state SPC to a connected state SC while meeting class 2/class 3 USCAR specifications without requiring a lever assist. Eliminating the lever assist reduces the size, weight, and cost of manufacturing the connector system 10. It should be understood that to further reduce the coefficient of friction, the sloped or ramped surface 676 may be coated with a substance that reduces this coefficient or the sloped or ramped surface 676 may be made from a material that has an even lower coefficient of friction.
Due to the configuration of the male and female connectors 50, 650, different levels of force are required as the connector system 10 moves from the disconnected state SDC to the connected state SC. For example, a first force F11 is required to move the male terminal assembly 100 when an extent (e.g., a contact arm 180a-180d) of the male terminal assembly 100 is in sliding engagement with the male terminal compression means 674 and a second force F12 is required to move the male terminal assembly 100 when the extent (e.g., a contact arm 180a-180d) male terminal assembly 100 is positioned in the female terminal receiver 702. Comparing the forces, it should be understood that the second force F12 is less than the first force F11. This is beneficial because it provides the user with a tactical feedback to inform the user that the male terminal assembly 100 is properly seated within the female terminal assembly 700. In fact, this tactical feedback fells to the user like the male terminal assembly 100 is being pulled into the female terminal assembly 700.
To minimize the chance that the male connector assembly 50 can be accidently disconnected from the female connector assembly 650, the female connector assembly 650 may include an optional non-deformable female CPA structure that is designed and configured to interact with the male CPA structures, when the connector assemblies 50, 650 are coupled to one another. Said non-deformable female CPA structure is integrally formed with the sidewall 672 of the female housing assembly 670. Additional details about the structure and/or function of the female CPA structure are disclosed in PCTUS2019/036070, PCTUS2020/049870, PCTUS2021/033446, all of which are incorporated herein by reference.
b. Female Terminal
The female terminal assembly 700 of the female connector assembly 650 is comprised of: (i) a female terminal connection member 701, and (ii) the female terminal body 710. Specifically, the female terminal connection member 701 is coupled to the female terminal body 710. In this embodiment, the female terminal connection member 701 is a wire receiver, wherein said wire receiver has a blade shaped structure that is configured to receive an extent of a structure (e.g., lead or wire) that connects the female terminal assembly 700 to a device (e.g., an alternator) outside of the connector system 10. A wire is typically welded to the wire receiver; however, other methods (e.g., forming the wire as a part of the wire receiver) of connecting the wire to the wire receiver are contemplated by this disclosure. In other embodiments, the female terminal connection member 701 may be a crimping connection, a circuit board connector, have a U-shaped configuration, or any other type of connection member 102 that mechanically and electrically couples the female terminal body 710 to an external device, part, or extent.
The female terminal body 710 of the female connector assembly 650 includes a sidewall 712 having an inner surface 704 that forms cylindrical terminal receptacle 702 with a receiver distance DR that extends between opposed points on the inner surface 704 of the sidewall 712. As discussed above, the receiver distance DR is: (i) less than the sidewall distance DS and (ii) equal to or greater than the rearmost edge distance DRE. Additionally, the receiver distance is between 0.1% and 15% smaller than a male terminal assembly distance that extends between the outermost extents of opposed contact arms 180a-180d. Forming a terminal receptacle 702 with a receiver distance that is less than the male terminal assembly distance ensures that the contact arms 180a-180d are compressed when the male terminal assembly 100 is inserted into the female terminal assembly 700. This compression of the male terminal assembly 100 compresses the spring member 300. As such, the spring member 300 exerts an outwardly directed biasing force FSB on the contact arms 180a-180d to help ensure that they remain in contact with the inner surface 704 of the terminal receptacle 702 to facilitate the electrical and mechanical coupling of the male terminal assembly 100 with the female terminal assembly 700.
The female terminal assembly 700 is typically formed from metal and preferably a highly conductive metal, such as copper. The female terminal assembly 700 may be plated or clad with Ni—Ag. In other embodiments, the sidewall 712 may be made from a different material, and/or the female terminal assembly 700 may not be plated or clad with Ni—Ag. Once the female terminal assembly 700 is fabricated, it can be coupled to the wire, part, component, or device via the female terminal connection member 701.
The connector system 10 can move from a disconnected state SDC to a partially connected state SPC, where the contact arms 180a-180d of the male connector assembly 50 in contact with the ramped or sloped surface 676 of the female connector assembly 650. This ramped or sloped surface 676 gently and smoothly compresses the contact arms 180a-180d until they can easily slide into and make contact with the inner surface 704 of the female receptacle 702. This process is described in greater detail within PCT/US2019/36070 and is incorporated herein. Once the male connector assembly 50 is connected to the female connector assembly 650, the connector system 10 has moved from the partially connected state SPC to the connected state SC. If present, a force is applied to the CPA that causes it to interact with an extent of the external component and the installer can scan an extent of the CPA that is visible through the opening within the housing, as described within PCT/US2020/049870.
The male terminal body 104, including the contact arms 180a-180d, may be formed from a first material such as copper, a highly-conductive copper alloy (e.g., C151 or C110), aluminum and/or another suitable electrically conductive material. The first material preferably has an electrical conductivity of more than 80% of IACS (International Annealed Copper Standard, i.e., the empirically derived standard value for the electrical conductivity of commercially available copper). For example, C151 typically has 95% of the conductivity of standard, pure copper compliant with IACS. Likewise, C110 has a conductivity of 101% of IACS. In certain operating environments or technical applications, it may be preferable to select C151 because it has anti-corrosive properties desirable for high-stress and/or harsh weather applications. The first material for the male terminal body 104 is C151 and is reported, per ASTM B747 standard, to have a modulus of elasticity (Young's modulus) of approximately 115-125 gigapascals (GPa) at room temperature and a coefficient of terminal expansion (CTE) of 17.6 ppm/degree Celsius (from 20-300 degrees Celsius) and 17.0 ppm/degree Celsius (from 20-200 degrees Celsius).
The spring member 300 may be formed from a second material such as spring steel, stainless steel (e.g., 301SS, ¼ hard), and/or another suitable material having greater stiffness (e.g., as measured by Young's modulus) and resilience than the first material of the male terminal body 104. The second material preferably has an electrical conductivity that is less than the electrical conductivity of the first material. The second material also has a Young's modulus that may be approximately 193 GPa at room temperature and a coefficient of terminal expansion (CTE) of 17.8 ppm/degree Celsius (from 0-315 degrees Celsius) and 16.9 ppm/degree Celsius (from 0-100 degrees Celsius). In contemplated high-voltage applications, the cross-sectional area of copper alloy forming the first connector is balanced with the conductivity of the selected copper alloy. For example, when a copper alloy having lower conductivity is selected, the contact arms 180a-180d formed therefrom have a greater cross-sectional area so as to adequately conduct electricity. Likewise, selection of a first material having a higher conductivity may allow for contact arms 180a-180d having a relatively smaller cross-sectional area while still meeting conductivity specifications.
In an example embodiment, the CTE of the second material may be greater than the CTE of the first material, i.e., the CTE of the spring member 300 is greater than the CTE of the male terminal body 104. Therefore, when the assembly of the male terminal body 104 and the spring member 300 is subjected to the high-voltage and high-temperature environment typical for use of the electrical connector described in the present disclosure, the spring member 300 expands relatively more than the male terminal body 104. Accordingly, the outward force FSB produced by the spring member 300 on the contact arms 180a-180d of the male terminal body 104 is increased in accordance with the increased temperature, which is reference to below as a thermal spring force FST.
An example application of the present disclosure, such as for use in a charge coupler, is suitable for deployment in a class 5 automotive environment, such as that found in passenger and commercial vehicles. Class 5 environments are often found under the hood of a vehicle, e.g., alternator, and present 150° Celsius ambient temperatures and routinely reach 200° Celsius. When copper and/or highly conductive copper alloys are subjected to temperatures above approximately 150° Celsius said alloys become malleable and lose mechanical resilience, i.e., the copper material softens. However, the steel forming the spring member 300 retains hardness and mechanical properties when subjected to similar conditions. Therefore, when the male terminal body 104 and spring member 300 are both subjected to high-temperature, the first material of the male terminal body 104 softens and the structural integrity of the spring member 300, formed from the second material, is retained, such that the force applied to the softened contact arms 180a-180d by the spring member 300 more effectively displaces the softened contact arms 180a-180d outward relative the interior of the male terminal body 104, in the fully connected position SFC.
The male terminal body 104, spring member 300, and female terminal body 710, are configured to maintain conductive and mechanical engagement while withstanding elevated temperatures and thermal cycling. Further, the male terminal body 104 and female terminal body 710 may undergo thermal expansion as a result of the elevated temperatures and thermal cycling, which increases the outwardly directed force FSB applied by the male terminal body 104 on the female terminal body 710. The configuration of the male terminal body 104, spring member 300, and the female terminal body 710 increase the outwardly directed connective force therebetween while the connector system 10 withstands thermal expansion resulting from thermal cycling in the connected position PC.
Based on the above exemplary embodiment, the Young's modulus and the CTE of the spring member 300 is greater than the Young's modulus and the CTE of the male terminal body 104. Thus, when the male terminal body 104 is used in a high power application that subjects the connector system 10 to repeated thermal cycling with elevated temperatures (e.g., approximately 150° Celsius) then: (i) the male terminal body 104 become malleable and loses some mechanical resilience, i.e., the copper material in the male terminal body 104 softens and (ii) the spring member 300 does not become as malleable or loses as much mechanical stiffness in comparison to the male terminal body 104.
Thus, when utilizing a spring member 300 that is mechanically cold forced into shape (e.g., utilizing a die forming process) and the spring member 300 is subjected to elevated temperatures, the spring member 300 will attempt to at least return to its uncompressed state, which occurs prior to insertion of the male terminal assembly 100 within the female terminal assembly 700, and preferably to its original flat state, which occurs prior to the formation of the spring member 300. In doing so, the spring member 300 will apply a generally outward directed thermal spring force FST, (as depicted by the arrows labeled “FST” in
Further illustrated in
In this second embodiment of the system 1010, an extent of the means for limiting compression 314 from the first embodiment of the system 10 was replaced with an alternative extent of the means for limiting compression 1314. In particular, the second combination of limiting structures 315b (i.e., jacket extents 329b, 329d of the spring member 300 and the spring arm openings 434a, 434b formed in the jacket 400) was replaced with an alternative combination of structures 1315b (i.e., contact extensions 1331b, 1331d). Here, the contact extensions 1331b, 1331d disclosed in this embodiment 1010 replace the jacket extents 329b, 329d from the first embodiment of the system 10. In this embodiment, the application of an external force FE on the contact arms 1180b, 1180d can only deform the contact arms 1180b, 1180d, the alternative max compression distance DAMC because the frontal end 1330b, 1330d contact one another. Limiting the extent the contact arms 1180b, 1180d be deforming or depressing to the alternative max compression distance DAMC prevents the contact arms 1180b, 1180d, spring arms 1312b, 1312d, and a combination thereof from being overly deformed or depressed (e.g., a distance that is greater than the alternative max compression distance DAMC) toward the center of the connector 1050. The alternative max compression distance DAMC in this embodiment is twice as large as the max compression distance DMC, but is still small enough to reduce system 1010 failures due to over compression by the external force FE. In other words, the compression distance that the system 1010 fails at larger than the alternative max compression distance DAMC, which is larger than the max compression distance DMC, which is larger than the normal or operational deformation distance the system 1010 experiences when the system 1010 is in the connected state SCN. The design of this terminal assembly 1100 may be more desirable over the first embodiment of the terminal assembly 100 because the means for limiting compression 1314 is completely contained in a single structure (i.e., the spring member 1300), which in turn may increase the durability and longevity of the system 1010.
Unlike the first two embodiments of the male terminal assembly 100, 1100 disclosed herein, the spring arm 2312a-2312d does not have a geometry that substantially matches the geometry of the associated contact arm 2180a-2180d. As such, the spring arm 2312a-2312d does not have an outer surface 2313a-2313d that underlie and abuts a majority of an inner surface of the associated contact arm 2180a-2180d. Instead, the free end 2330a-2330d of the spring arms 2312a-2312d are positioned under the apex 2186a-2186d of the bent or creased portion 178a-178d of the contact arms 180a-180d. This configuration forms a gap G (which has a right triangular shape) between the upwardly sloping extent 233a, the vertical extent 2353a-2353d of the spring arms 2312a-2312d, and the linear extent 2316a-2316d of the spring arms 2312a-2312d. Like the first two embodiments of the system 10, 1100, the free ends 2190a-2190d of the contact arms 2180a-2180d do not abut a planar outer surface 2313a-2313d of the spring arms 2312a2-312d. Other structures, functions, or positional relationships may be obvious to one of skill in the art based on
The spring member 2300 disclosed in this embodiment replaces prior versions of the means for limiting compression 314, 1314 with structures that are fully integrated into the spring member 2300. Here, said means for limiting compression 2314 is formed from a combination of the compression tabs 2370 and edges 2332a-2332b, 2334a-2334b of adjacent spring arms 2312a-2312d. Said compression tabs 2370 include: (i) lateral projections 2371a-2371b that extend outward from forward curvilinear extent 2351a, 2351c (line S5, S6) and terminate at external surfaces 2373a-2373b, and (ii) substantially vertical wings 2375a-2375b that extend outward from linear extents 2316b, 2316d (line S7, S8) and terminate at external surfaces 2376a-2376b. In other words, the means for limiting compression 2314 in this embodiment includes: (i) a first combination of limiting structures 2315a, namely-lateral projections 2371a-2371b and edges 2334a-2334b of the adjacent side spring arms 2312b, 2312d, and (ii) a second combination of limiting structures 2315b, namely-substantially vertical wings 2375a-2375b and edges 2332a-2332b of the adjacent side spring arms 2312a, 2312c.
The external surfaces 2373a-2373b of the lateral projections 2371a-2371b are positioned outside of or beyond the inner surfaces 2346 of opposed linear extents 2316b, 2316d. In other words, the length between the external surfaces 2373a-2373b of the lateral projections 2371a-2371b is greater than the inner linear surface width WILS, which extends between the inner surfaces 2346 of opposed linear extents 2316b, 2316d. The application of an external force FE on the contact arms 2180a, 2180c can only deform the contact arms 2180a, 2180c, the max compression distance DMC because an inner surface 2372 of the lateral projections 2371a-2371b contacts the forward spring arm edges 2334a, 2334b of the side spring arms 2312b, 2312d (specifically, the edges of the forward curvilinear extent 2351b, 2351d of the side spring arms 2312b, 2312d). In this embodiment the max compression distance DMC is less than 1.25 mm, preferably less than 1.0 mm, and most preferably 0.85 mm. Limiting the extent the contact arms 2180a, 2180c can be deformed or depressed to the max compression distance DMC prevents the contact arms 2180a, 2180c, spring arms 2312a, 2312c, and a combination thereof helps prevent said arms 2180a, 2180c from being overly deformed or depressed (e.g., a distance that is greater than the max compression distance DMC) toward the center of the connector 2050.
The external surfaces 2376a-2376b of the substantially vertical wings 2375a-2375b are positioned outside of or beyond the inner surfaces 2346 of opposed linear extents 2316a, 2316c. In other words, the length between the external surfaces 2376a-2376b of the substantially vertical wings 2375a-2375b is greater than the inner linear surface width WILS, which extends between the inner surfaces 2346 of opposed linear extents 2316a, 2316c. The application of an external force FE on the contact arms 2180b, 2180d can only deform the contact arms 2180b, 2180d, the max compression distance DMC because an inner surface 2374 of the substantially vertical wings 2375a-2375b contacts the linear extent edges 2332a, 2332b of the top and bottom spring arms 2312a, 2312c (specifically, the edges of the linear extents 2316a, 2316b of the side spring arms 2312b, 2312d). In this embodiment the max compression distance DMC is less than 1.25 mm, preferably less than 1.0 mm, and most preferably 0.85 mm. Limiting the extent the contact arms 2180b, 2180d can be deformed or depressed to the max compression distance DMC prevents the contact arms 2180b, 2180d, spring arms 2312b, 2312d, and a combination thereof helps prevent said arms 2180b, 2180d from being overly deformed or depressed (e.g., a distance that is greater than the max compression distance DMC) toward the center of the connector 2050.
a. Male Terminal Assembly
The bent or creased configuration of the contact arms 3180a-3180d provides the connector system 3010 with several advantages over previous designs. For example, this design includes a vertical extent 3194a-3194d that supports the external apex 3186a-3186d of said contact arm 3180a-3180d. This added support increases the durability of the contact arm 3180a-3180d over the contact arm 3180a-3180d designs shown in PCT/US2019/036010—namely, the designs shown in
Referring to
As shown in
As discussed in greater detail below, the third or downwardly sloping extent 3188a-3188d, and specifically the contact surface 3189a-3189d, is configured to contact an extent of the female connector assembly 650 when the male terminal assembly 3100 is inserted into the female terminal assembly 700. This interaction between these components causes the contact arms 3180a-3180d to be deflected or displaced inward and towards the center of the male terminal assembly 3100 and the spring member 700. This inward deflection of the contact arms 3180a-3180d causes the spring member 700 to act as a wedge to help ensure that a proper mechanical and electrical connection is created between the contact arms 3180a-3180d and the female receptacle 702.
As shown in
As shown in
As shown in
The male terminal 3101 is typically formed from a single piece of material (e.g., metal); thus, the male terminal 3101 is a one-piece male terminal 3101 and has integrally formed features. To integrally form these features, the male terminal 3101 is typically formed using a die-cutting process. However, it should be understood that other types of forming the male terminal 3101 may be utilized, such as casting or using an additive manufacturing process (e.g., 3D printing). In other embodiments, the features of the male terminal 3101 may not be formed from a one-piece or be integrally formed, but instead formed from separate pieces that are welded together. In forming the male terminal 3101, it should be understood that any number (e.g., between 1 and 100) of contact arms 3180a-3180d may be formed within the male terminal 3101. The male terminal 3101, male terminal body 104, the contact arms 3180a-3180d, or an extent of the contact arms 3180a-3180d may be plated or coated with a secondary material (e.g., nickel) to help reduce corrosion, reduce insertion forces, or improve conductivity. Additionally, the contact arms 3180a-3180d or a portion of the contact arms 3180a-3180d may have rounded or beveled edges.
b. Spring Member
As best shown in
The spring member 3300 disclosed in this embodiment includes a centering means 3380. Said disclosed centering means 3380 does not rely on outwardly extending lateral projection, but; instead, relies on corrugations 3382a-3382b formed in at least one and preferable two opposed spring arms 3312b, 3312d. As best shown in
The spring member 3300 disclosed in this embodiment replaces prior versions of the means for limiting compression 314, 1314, 2134 with structures that are fully integrated into the spring member 3300. Said means for limiting compression 3314 can best be seen in
The external surfaces 3373a-3373b of the lateral projections 3371a-3371b are positioned outside of or beyond the inner surfaces 3346 of opposed corrugations 3382a-3382b. In other words, the length between the external surfaces 3373a-3373b of the lateral projections 3371a-3371b is greater than the inner linear surface width WILS, which extends between the inner surfaces 3346 of opposed corrugations 3382a-3382b. The application of an external force FE on the contact arms 3180a, 3180c can only deform the contact arms 3180a, 3180c, the max compression distance DMC because an inner surface 3372 of the lateral projections 3371a-3371b contacts the forward spring arm edges 3334a, 3334b of the side spring arms 3312b, 3312d. In this embodiment the max compression distance DMC is less than 1.25 mm, preferably less than 1.0 mm, and most preferably 0.85 mm. Limiting the extent the contact arms 3180a, 3180c can be deformed or depressed to the max compression distance DMC prevents the contact arms 3180a, 3180c, spring arms 3312a, 3312c, and a combination thereof helps prevent said arms 3180a, 3180c from being overly deformed or depressed (e.g., a distance that is greater than the max compression distance DMC) toward the center of the connector 3050.
The external surfaces 3376a-3376b of the substantially vertical wings 3375a-3375b are positioned outside of or beyond the inner surfaces 3346 of opposed linear extents 3316a, 3316c. In other words, the length between the external surfaces 3376a-3376b of the substantially vertical wings 3375a-3375b is greater than the inner linear surface width WILS, which extends between the inner surfaces 3346 of opposed linear extents 3316a, 3316c. The application of an external force FE on the contact arms 3180b, 3180d can only deform the contact arms 3180b, 3180d, the max compression distance DMC because an inner surface 3374 of the substantially vertical wings 3375a-3375b contacts the linear extent edges 3332a, 3332b of the top and bottom spring arms 3312a, 3312c (specifically, the edges of the linear extents 3316a, 3316b of the side spring arms 3312b, 3312d). In this embodiment the max compression distance DMC is less than 1.25 mm, preferably less than 1.0 mm, and most preferably 0.85 mm. Limiting the extent the contact arms 3180b, 3180d can be deformed or depressed to the max compression distance DMC prevents the contact arms 3180b, 3180d, spring arms 3312b, 3312d, and a combination thereof helps prevent said arms 3180b, 3180d from being overly deformed or depressed (e.g., a distance that is greater than the max compression distance DMC) toward the center of the connector 3050.
The spring arms 3312a-3312d are generally planar and are positioned substantially perpendicular to the outer surface of the rear wall 3306. This configuration is beneficial over the previously disclosed spring arms that extend outward at an angle because insertion force calculations are simplified, size of the terminal assembly 3100 is reduced, centering of the spring member is more reliable, and other benefits that may be obvious to one of skill in the art based on this disclosure. Unlike the spring arm 31 that is disclosed within FIGS. 4-8 of PCT/US2018/019787, the free end 3330a-3330d of the spring arms 3312a-3312d do not have a curvilinear end component. But for the small corrugations 3382a-3382b, the spring arms 3312a-3312d have a substantially planar outer surface. This configuration is beneficial because it ensures that the forces associated with the spring 3300 are applied substantially perpendicular to the ends of the male terminal body 3104. In contrast, the curvilinear components of the spring arm 31 disclosed within FIGS. 4-8 of PCT/US2018/019787 do not apply a force in this manner.
In an alternative embodiment that is not shown, the spring member 3300 may include recesses and associated strengthening ribs. As discussed in PCT/US2019/036010, these changes to the configuration of the spring member 3300 alter the forces that are associated with the spring 3300. In particular, the spring biasing force SBF is the amount of force applied by the spring member 3300 to resist the inward deflection of the free end of the spring member 3300 when the male terminal assembly 3100 is inserted within the female terminal assembly 700. Specifically, this inward deflection occurs during the insertion of the male terminal assembly 3100 because an extent of the outer surface of the male terminal body 3104 is slightly larger than the interior of the female receptacle 704. Thus, when the male terminal assembly 3100 is inserted into the female terminal assembly 2430, the extent of the outer surface is forced towards the center of the male terminal 3101. This inward force on the outer surface displaces the free end 3330a-3330d of the spring member 3300 inward (i.e., towards the center). The spring member 3300 resists this inward displacement by providing a wedging effect or spring biasing force SF. In other embodiments, the spring arms 3312a-3312d may be coupled to other structures to restrict their omnidirectional expansion or compression. The number and width of individual spring arms 3312a-3312d and openings may vary. In addition, the width of the individual spring arms 3312a-3312d is typically equal to one another; however, in other embodiments, one of the spring arms 3312a-3312d may be wider than other spring arms.
Referring to
The spring arms 6312a-6312d are generally planar and are positioned such that the outer surface 6313a-6313d of the spring arms 6312a-6312d is substantially perpendicular to the outer surface of the rear wall 6306. Unlike the spring arm 31 that is disclosed within FIGS. 4-8 of PCT/US2018/019787, the free end 6318 of the spring arms 6312a-6312d do not have a curvilinear component. Instead, the spring arms 6312a-6312d have a substantially planar outer surface 6313a-6313d. This configuration is beneficial because it ensures that the forces associated with the spring member 6300 are applied to the frontal spring contact segment 6196a-6196d and the intermediate spring contact segment 6198a-6198d of the contact arms 6180a-6180d. In contrast, the curvilinear components of the spring arm 31 that are disclosed within FIGS. 4-8 of PCT/US2018/019787 do not apply a force in this manner.
In an alternative embodiment that is not shown, the spring member 6300 may include recesses and associated strengthening ribs. As discussed in PCT/US2019/036010, these changes to the configuration of the spring member 6300 alter the forces that are generated by or applied by the spring member 6300. In particular, the spring biasing force FSB is the amount of force that is applied by the spring member 6300 to resist the inward deflection of the free end 6318 of the spring member 6300 when the male terminal assembly 6100 is inserted within the female terminal assembly 700. Specifically, this inward deflection occurs during the insertion of the male terminal assembly 6100 due to the fact that an extent of an outer surface of the male terminal body 6104 is slightly larger than the interior of the female receptacle 702. Thus, when the male terminal assembly 6100 is inserted into the female terminal assembly 700, the extent of the outer surface is forced towards the center of the male terminal 6101. This compression force FCOM on the outer surface of the male terminal body 6104 displaces the free end 6318 of the spring member 6300 inward (i.e., towards the center). The spring member 6300 resists this inward displacement by providing an outwardly directed spring biasing force FSB. In other embodiments, the spring arms 6312a-6312d may be coupled to other structures to restrict their omnidirectional expansion. The number and width of individual spring arms 6312a-6312d and openings may vary. In addition, the width of the individual spring arms 6312a-6312d is typically equal to one another; however, in other embodiments one of the spring arms 6312a-6312d may be wider than other spring arms.
The system 10, 1010, 2010, 3010, 4010, 5010, and 6010 is compliant to T4/V4/D2/M2, wherein the system 10, 1010, 2010, 3010, 4010, 5010, and 6010 meets and exceeds: (i) T4 is exposure of the system 10 to 150° C., (ii) V4 is severe vibration, (iii) D2 is 200k mile durability, and (iv) M2 is less than 45 Newtons of force is required to connect the male terminal assembly 100, 1100, 2100, 3100, 4100, 5100, 6100 to the female terminal assembly 700, 1700, 2700, 3700, 4700, 5700, 6700. In addition to being T4/V4/D2/M2 compliant, the system 10, 1010, 2010, 3010, 4010, 5010, and 6010 is push, click, tug, scan (PCTS) compliant, wherein additional information about this standard is disclosed within PCT/US2020/049870.
It should be understood that the male terminal assemblies 100, 1100, 2100, 3100, 4100, 5100, 6100 and the female terminal assemblies 700, 1700, 2700, 3700, 4700, 5700, 6700 disclosed within this application having the following specifications regarding carrying at 55° C. rise over ambient (RoA) or 80° C. with a derating of 80%: (i) wherein the outside perimeter of the male terminal assembly 100, 1100, 2100, 3100, 4100, 5100, 6100 is 8 mm and its rated to carry 210 amps with a 16 mm2 wire. Additionally, the system 10 meets the mile durability of USCAR-20, has a contact mating force that is between 10 Newtons and 30 Newtons, preferably 15 Newtons, has a unmating force that may be larger than the mating force and is between 10 Newtons and 30 Newtons, preferably 18 Newtons, meet vibration standards of 31 Gs, and is ISL/TPA compatible. These substantial increases in current carrying capacity, while meeting the USCAR specifications provides considerable advantages of the prior art connectors. The connector systems 10, 1010, 2010, 3010, 4010, 5010, and 6010 also meet applicable USCAR-38 specifications.
It should be understood that alternative configurations for means for limiting compression 314, 1314, 3314, 4314, 5314, 6314 are contemplated by this disclosure. For example, in other embodiments the means for limiting compression 3314 may be: (i) projections that extend outward from the spring arms and are received by openings in the jacket, (ii) structures that extend from one side wall of the jacket to an opposing side wall of the jacket, wherein said structure is configured to interact with the inner surface of the spring member, (iii) contact arm noses, wherein said contact arm noses are configured to interact with one another, (iv) structure that extends across the contact opening formed in the jacket and is positioned in the gap formed between the spring member and contact arm, (v) interactions between opposed spring arms or contact arms, (vi) interactions between jacket and either the spring arms or contact arms, (vii) interactions between the housing assembly and either the contact arms or spring arms, or (viii) any combination of these structures. It should also be understood that these compression tabs are not designed herein as a centering means 3380; however, said compression tabs could be extended to provide a centering means. Additionally, alternative male terminal housings are contemplated by this disclosure. For example, the housings may include any number of male terminal assemblies 100, 1100, 2100, 3100, 4100, 5100, 6100 (e.g., between 2-30, preferably between 2-8, and most preferably between 2-4) may be positioned within a housing. Additionally, alternative configurations for female terminal assemblies. For example, the housings may include any number of female terminal assemblies (e.g., between 2-30, preferably between 2-8, and most preferably between 2-4) may be positioned within a housing. Further, the female connector assembly may be reconfigured to accept these multiple male terminal assemblies into a single female terminal assembly. It should also be understood that the male terminal assemblies 100, 1100, 2100, 3100, 4100, 5100, 6100 may have any number of contact arms (e.g., between 2-100, preferably between 2-50, and most preferably between 2-8) and any number of spring arms (e.g., between 2-100, preferably between 2-50, and most preferably between 2-8). As discussed above, the number of contact arms may not equal the number of spring arms. For example, there may be more contact arms then spring arms. Alternatively, there may be less contact arms then spring arms.
Materials and Disclosure that are Incorporated by Reference
PCT Application Nos. PCT/US2022/037508, PCT/IB2022/057772, PCT/US2021/057959, PCT/US2021/047180, PCT/US2021/043788, PCT/US2021/043686, PCT/US2021/033446, PCT/US2020/050018, PCT/US2020/049870, PCT/US2020/014484, PCT/US2020/013757, PCT/US2019/036127, PCT/US2019/036070, PCT/US2019/036010, and PCT/US2018/019787, U.S. patent application Ser. No. 16/194,891 and U.S. Provisional Applications 63/286,072, and 63/286,080, each of which is fully incorporated herein by reference and made a part hereof.
SAE Specifications, including: J1742_201003 entitled, “Connections for High Voltage On-Board Vehicle Electrical Wiring Harnesses-Test Methods and General Performance Requirements,” last revised in March 2010, each of which is fully incorporated herein by reference and made a part hereof.
ASTM Specifications, including: (i) D4935-18, entitled “Standard Test Method for Measuring the Electromagnetic Shielding Effectiveness of Planar Materials,” and (ii) ASTM D257, entitled “Standard Test Methods for DC Resistance or Conductance of Insulating Materials,” each of which are fully incorporated herein by reference and made a part hereof.
American National Standards Institute and/or EOS/ESD Association, Inc Specifications, including: ANSI/ESD STM11.11 Surface Resistance Measurements of Static Dissipative Planar Materials, each of which is fully incorporated herein by reference and made a part hereof.
DIN Specification, including Connectors for electronic equipment-Tests and measurements-Part 5-2: Current-carrying capacity tests; Test 5b: Current-temperature derating (IEC 60512 May 2:2002), each of which are fully incorporated herein by reference and made a part hereof.
USCAR Specifications, including: (i) SAE/USCAR-2, Revision 6, which was last revised in February 2013 and has ISBN: 978-0-7680-7998-2, (ii) SAE/USCAR-12, Revision 5, which was last revised in August 2017 and has ISBN: 978-0-7680-8446-7, (iii) SAE/USCAR-21, Revision 3, which was last revised in December 2014, (iv) SAE/USCAR-25, Revision 3, which was revised on March 2016 and has ISBN: 978-0-7680-8319-4, (v) SAE/USCAR-37, which was revised on August 2008 and has ISBN: 978-0-7680-2098-4, (vi) SAE/USCAR-38, Revision 1, which was revised on May 2016 and has ISBN: 978-0-7680-8350-7, each of which are fully incorporated herein by reference and made a part hereof.
Other standards, including Federal Test Standard 101C and 4046, each of which is fully incorporated herein by reference and made a part hereof. While some implementations have been illustrated and described, numerous modifications come to mind without significantly departing from the spirit of the disclosure; and the scope of protection is only limited by the scope of the accompanying claims. For example, the overall shape of the of the components described above may be changed to: a triangular prism, a pentagonal prism, a hexagonal prism, octagonal prism, sphere, a cone, a tetrahedron, a cuboid, a dodecahedron, an icosahedron, an octahedron, a ellipsoid, or any other similar shape.
It should be understood that the following terms used herein shall generally mean the following:
Headings and subheadings, if any, are used for convenience only and are not limiting. The word exemplary is used to mean serving as an example or illustration. To the extent that the term includes, have, or the like is used, such term is intended to be inclusive in a manner similar to the term comprise as comprise is interpreted when employed as a transitional word in a claim. Relational terms such as first and second and the like may be used to distinguish one entity or action from another without necessarily requiring or implying any actual such relationship or order between such entities or actions.
Phrases such as an aspect, the aspect, another aspect, some aspects, one or more aspects, an implementation, the implementation, another implementation, some implementations, one or more implementations, an embodiment, the embodiment, another embodiment, some embodiments, one or more embodiments, a configuration, the configuration, another configuration, some configurations, one or more configurations, the subject technology, the disclosure, the present disclosure, other variations thereof and alike are for convenience and do not imply that a disclosure relating to such phrase(s) is essential to the subject technology or that such disclosure applies to all configurations of the subject technology. A disclosure relating to such phrase(s) may apply to all configurations, or one or more configurations. A disclosure relating to such phrase(s) may provide one or more examples. A phrase such as an aspect or some aspects may refer to one or more aspects and vice versa, and this applies similarly to other foregoing phrases.
Numerous modifications to the present disclosure will be apparent to those skilled in the art in view of the foregoing description. Preferred embodiments of this disclosure are described herein, including the best mode known to the inventors for carrying out the disclosure. It should be understood that the illustrated embodiments are exemplary only, and should not be taken as limiting the scope of the disclosure.
This application claims the benefit from U.S. provisional patent application Nos. 63/286,072 and 63/286,080, both of which were filed on Dec. 5, 2021, and are incorporated herein by this reference.
Filing Document | Filing Date | Country | Kind |
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PCT/IB2022/061786 | 12/5/2022 | WO |
Number | Date | Country | |
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63286072 | Dec 2021 | US | |
63286080 | Dec 2021 | US |