The present invention relates generally to electrical connectors and more particularly to a male multi-pin connector device and method of providing repeatable consistent connection with a female receptacle connector.
Making electrical contact across multiple pins for continuity across industrial cables can be accomplished with a variety of conventional connectors to include military standard connectors such as a D38999 series connector. Within military applications and in industry environments there are a multitude of applications where fine control over multiple contact pin engagements into contact pin receptacles is desirable.
Plug-type connectors connected to testing circuitry may be repeatedly connected and disconnected to test a given device periodically and/or to test a number of devices. For example, testing of missile launch circuitry may be desired at periodic intervals. Testing of other aircraft circuitry or a launch connector may be desirable as well. It would be desirable if multiple connecting and disconnecting operations could be done without damaging either the connector which is connected to the launch circuitry or the tester connector. A means of verification of pin and receptacle mating between the female connector and the male tester connector is also desirable.
Conventional male plug-type connectors with conventional female-socket-type connectors can be difficult to connect and disconnect in on-site applications. Ease of use of a connector is also desirable for test connectors to be used in areas of restricted accessibility, reach, and visibility. Conventional connectors may comprise a large lever or handle for a means of inserting and extracting pins in a connector. In certain applications, such as testing aircraft circuitry for an air-intercept missile 120 (AIM-120) launcher rail, a means of assessing contact pin position, other than electrical measurements, may not be possible. Conventional levers to establish electrical connection and disconnection may create an undesirable off axis moment about the connector. This can lead to stress, loosening, and bending of the connector pins.
It would be desirable to have a connector which did not induce undesirable physical forces on the electrical contact pins. Limiting an applied force upon the connector during mechanical mating may also be desired, contributing to a long usable service life of the connector. Applications with multi-pin connections or heavy cables can exacerbate these challenges. Applications not within easy reach of the user can add to the challenges of providing finely controlled and reliable connections and disconnections.
The present invention addresses some of the issues presented above by providing a method and device for displacing a set of connector pins with a controlled on axis force and a stop catch upon full pin insertion and full pin extraction, while providing device reliability. Aspects of the present invention are provided for summary purposes and are not intended to be all inclusive or exclusive. Embodiments of the present invention may have any of the aspects below.
One aspect of the present invention is to ensure electrical connection by providing full pin insertion into the female socket.
Another aspect of the present invention is to minimize any moment on the pins by using balanced on axis motion to displace the pin plunger.
Another aspect of the present invention is to provide fine manual control of pin displacement during insertion and extraction from the female receptacle.
Another aspect of the present invention is to use alignment pins to ensure alignment of the desired pin configuration with the female plug.
Another aspect of the present invention is a connector which provides an affirmative forward stop for complete pin insertion and maximum pin displacement. Yet another aspect of the present invention is a connector which provides an affirmative stop for full pin retraction for both ease of use and safety.
Another aspect of the present invention is compatibility with conventional female military connectors as well as conventional female socket-type connectors.
Another aspect of the present invention is its ease of assembly and disassembly.
Another aspect of an exemplary embodiment of the present invention may be its relative ease of use in connecting to and testing of a circuitry for a missile launcher rail.
Another aspect of the present invention is its ready insertion into a missile launcher rail, in accordance with an exemplary launcher rail mount embodiment.
Another aspect of the present invention is its compatibility with a multitude of anchoring surfaces, in accordance with an exemplary anchor mount embodiment.
Another aspect of the present invention is its use of an anchored stationary housing, which contributes to the ease of use, fine control of electrical connection, device longevity, and safety.
Another aspect of the present invention is its use of an anchored stationary housing in combination a rotatable coupling ring with triple start threads to provide leverage and control of pin displacement.
Another aspect of the present invention may be the ability to prevent excess force from being applied to any mechanical mating, such as contact pin engagement via torque limiting means in a coupling ring.
Another aspect of an the present invention may be the ability to reach a minimum torque load before mechanical engagement of, for example, contact pins with receptacles occurs. This aspect may be particularly desirable for connections in high vibration conditions.
Another aspect of the present invention may be the use of threads for axial pin plunger displacement in combination with exterior markings across the coupling ring and stationary housing can provide visual verification of contact pin position relative to female receptacles.
Those skilled in the art will further appreciate the above-noted features and advantages of the invention together with other important aspects thereof upon reading the detailed description that follows in conjunction with the drawings.
For more complete understanding of the features and advantages of the present invention, reference is now made to the detailed description of the invention along with the accompanying figures, wherein:
The invention, as defined by the claims, may be better understood by reference to the following detailed description. The description is meant to be read with reference to the figures contained herein. This detailed description relates to examples of the claimed subject matter for illustrative purposes, and is in no way meant to limit the scope of the invention. The specific aspects and embodiments discussed herein are illustrative of ways to make and use the invention, and are not intended to limit the scope of the invention. Parallel numbers across figures typically refer to like elements for ease of reference. Reference numbers may also be unique to a respective figure or embodiment and need not be consistent across figures.
Towards the back end 501 of the connector, a snap ring 550 clamps around an outer circumference of an internal plunger 560. A rear washer 547 is positioned just forward of the snap ring and just aft of an edge of the coupling ring 540. As also shown in
Referring again to
In this cross sectional view, internal threads 548 of the coupling ring 540 can be seen both engaging external threads 525 and open to the interior of the coupling ring 540. In accordance with an embodiment of the present invention, external stationary housing threads 525 and internal coupling ring threads are triple start threads, providing fine control of pin translation in a heavy and large connector.
As the coupling ring 540 turns clock wise, front washer 543 presses on a step of the internal plunger 560 and the plunger moves forward relative to the stationary housing 520. The threads of the coupling ring 548 engage more of the stationary housing external threads 525 and fewer open internal threads, or none as shown, are visible. As the plunger 560 slides forward in the stationary housing 520, a void 520-3 is created between an inner diameter of the stationary housing 520 and an outer diameter of the internal plunger 560.
In alternate embodiments, the diameter of, number of, and arrangement of the pin receptacles may vary as needed to accommodate varying pin contact diameters of a connector, in accordance with the present invention. Multiple receptacle configurations may be compatible with a same contact pin configuration. Actual pin number, size, and arrangement may vary in accordance with respective launcher rail requirements. A female connector 693 may not have housing 690, and may only have a housing 691,
In accordance with exemplary embodiments alignment pins 717-1, 717-2 and contact pins 715 are attached to the internal plunger. A shoulder 717,
The connecting cable 699 of the female connector 690, shown in
Referring again to
With the contact pins fully retracted, the user aligns alignment pins of the connector with the alignment pin receptacles of the female connector 930 and the user inserts the plug of the female connector to be tested into the coupling end of the stationary housing 930,
Referring to
The present invention provides a means of finally controlling forward and backward movement of an internal connector plunger along its axial center. A coupling ring with an internal triple start thread rotates on an external triple start thread of a stationary housing. With the stationary housing anchored in a missile launch rail, the coupling ring is rotated clockwise, the ring pushes the non-rotating internal connector plunger forward. Forward movement can continue with clockwise rotation until the forward washer has made contact with an aft most edge of the stationary housing. In accordance with an exemplary embodiment of the present invention, the contact pins attached to the internal plunger can displace a distance of approximately 0.500 inches.
The total displacement distance of the internal plunger may be readily varied across embodiments of the present invention by increasing respective lengths of the coupling ring, stationary housing, and internal plunger. The configuration of the anchor mount of the stationary housing may also be varied in alternate embodiments to permit the secure mounting of the connector in alternate missile launcher rails. Contact pin and alignment configurations may also be varied across embodiments to accommodate alternate female connectors, perhaps on different aircraft or, again, on different missile launcher rail circuitry.
The triple start threads provide fine control over pin insertion into and extraction from the female plug via a hand grip about the coupling ring. Connector design translates this ring rotation about the plunger axis to a balanced circumferential force pushing the plunger forward or aft in a direction parallel to the plunger axis, and in turn, parallel to the contact pins. A left or right force 10-115, 10-116,
The present invention greatly minimizes any normal forces applied to the axis of the connector. Referring to
Upon full forward displacement of the internal plunger, the contact pins and alignment pins are in contact with the female mating connector of the launcher rail. The rail is now ready for electrical testing. When the test is complete, the coupling ring can be rotated counter clockwise to move the internal connector plunger backward, which disengages the two connectors. Turning to
In practice, as a user turns the coupling ring, the internal connector plunger moves forward or backward, only the coupling ring rotates, the internal connector plunger does not rotate. Rotation of the internal plunger would tangle the wires inside the connector. The internal connector plunger moves forward and backward by the force of the coupling ring against the front and rear washers, which apply force to the connector plunger. The front and rear washers facilitate slippage of the coupling ring alleviating torsion on the internal plunger.
In accordance with an exemplary embodiment of the present invention, a user may verify that the plunger is in the rear most position by visual inspection of the connector opening at the coupling end of the stationary housing, noting the relative position of the alignment pins and contact pins to the outermost edge of the coupling end. Alternatively, the user may inspect the external threads of the stationary housing for one-half inch of exposed threads. Similarly, a user may verify full forward position of the contact pins by rotating the coupling ring clockwise until the internal threads of the coupling ring mate with all the external threads of the stationary housing.
An exemplary embodiment of the present invention has been successfully connected to and disconnected from a launch circuit's female connector and a missile launcher rail compatible with an AIM-120. Contact pins were repeatedly engaged and disengaged with the subject female receptacles using the device and method of an exemplary embodiment of the present invention. The anchor mount, 122 in
An exemplary embodiment of the present invention has been successfully connected and disconnected multiple times, electrically and mechanically to an AIM-120 missile launcher rail. Its relative small size approaches that of conventional D38999 series III connectors. As shown and described, the limiting forward and aft stops provide a user assurance that contact pins are properly engaged and disengaged, respectively. Manual rotation of the coupling ring provides a user friendly means of overcoming multi-pin contact insertion and extraction forces. Likewise the rotational action in combination with triple start threads yield movement of the pin assembly that is well-controlled. Embodiments of the present invention may readily include axial and radial torque limiting and loading features.
The present invention may be a suitable substitute for many conventional male plug-type pin connectors used with conventional female socket-type pin receptacle connectors. The present invention provides a connector with a leveraging means of overcoming the insertion and extraction forces in multi-pin connections, without the need for excessive force, and without the application of a bending moment on contact pins.
Since rotation of the coupling ring provides the translation of the internal plunger, additional features could be accommodated in the present invention. A torque limiting feature could prevent excess force from being applied to any mechanical mating, such as contact pin engagement. The coupling ring could include springs and or detents that would be loaded to a desired torque and allow slippage to happen if an overload situation is encountered.
A torque load threshold feature could be accommodated with the present invention. If a threshold torque was desired before actual rotation of the coupling ring is desired, springs or detents could be incorporated into the coupling ring and stationary housing connection to ensure that a desired minimum load was achieved before the coupling ring was able to rotate. This feature may be desirable for connections in high vibration conditions.
The use of threads for axial pin plunger displacement in combination with exterior markings across the coupling ring and stationary housing can provide visual verification of contact pin position relative to female receptacles. The use of triple start threads in combination with pairs of markings across the coupling ring and the stationary housing enables the user to control and ascertain the position of contact pins relative to the female connectors. In accordance with an exemplary embodiment, it may be desirable to engage specific contacts first, perhaps ensuring grounding. For example in a linear switch application, the user may verify a first pin plunger displacement by lining up a grounding pair of hash marks. Once grounding was accomplished further rotation could be applied to engage remaining, perhaps high amperage, contact pins. Similarly, in disconnection actions, a staggered disengagement of pins is readily achieved with the fine threaded motion and hash mark pairings.
While specific alternatives to steps of the invention have been described herein, additional alternatives not specifically disclosed but known in the art are intended to fall within the scope of the invention. Thus, it is understood that other applications of the present invention will be apparent to those skilled in the art upon reading the described embodiments and after consideration of the appended claims and drawings.
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