The present disclosure relates generally to a latch, and more specifically to a hook latch mechanism for use on aircraft.
Many types of latches are used in connection with aircraft to releasably secure two members or structures of the aircraft together in a closed position, such as the housing portions of an engine nacelle. Such latches are subjected to substantial forces during use while securing two aircraft members together in a closed position. Aircraft latches must also prevent inadvertent opening of the latch that could be caused by vibratory or other forces applied to the latch.
This background information is provided to provide some information believed by the applicant to be of possible relevance to the present disclosure. No admission is intended, nor is such an admission to be inferred or construed, that any of the preceding information constitutes prior art against the present disclosure. Other aims, objects, advantages and features of the disclosure will become more apparent upon reading of the following non-restrictive description of specific embodiments thereof, given by way of example only with reference to the accompanying drawings.
A latch mechanism of the present disclosure solves various design problems associated with a single link latch used in a restricted space as well as other applications. The following disclosure relates to a latch mechanism for use in latching a first body to a second body. Such a latch mechanism could be used in an aircraft to latch a first panel or structure to a second panel or structure. The latch mechanism includes a hook, a displaceable handle, and links connected between the handle and hook for the operation of the latch mechanism.
The present disclosure will be described hereafter with reference to the attached drawings which are given as a non-limiting example only, in which:
The exemplification set out herein illustrates embodiments of the disclosure that are not to be construed as limiting the scope of the disclosure in any manner Additional features of the present disclosure will become apparent to those skilled in the art upon consideration of the following detailed description of illustrative embodiments exemplifying modes of carrying out the disclosure as presently perceived.
While the present disclosure may be susceptible to embodiment in different forms, there is shown in the drawings, and herein will be described in detail, embodiments with the understanding that the present description is to be considered an exemplification of the principles of the disclosure. The disclosure is not limited in its application to the details of structure, function, construction, or the arrangement of components set forth in the following description or illustrated in the drawings. The disclosure is capable of other embodiments and of being practiced or of being carried out in various ways. Also, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting. The use of various phrases and terms is meant to encompass the items or functions identified and equivalents thereof as well as additional items or functions. Unless limited otherwise, various phrases, terms, and variations thereof herein are used broadly and encompass all variations of such phrases and terms. Furthermore, and as described in subsequent paragraphs, the specific configurations illustrated in the drawings are intended to exemplify embodiments of the disclosure. However, other alternative structures, functions, and configurations are possible which are considered to be within the teachings of the present disclosure. Furthermore, unless otherwise indicated, the term “or” is to be considered inclusive.
The terms herein should be broadly interpreted throughout this application to include all known as well as all hereafter discovered versions, equivalents, variations and other forms of the abovementioned terms as well as other terms. The present disclosure is intended to be broadly interpreted and not limited. For example, reference to a “rivet” includes rivets as well as other permanent or removable fasteners, such as screws, bolts, posts, pins, and plugs just to name a few.
An illustrative latch mechanism 10 in accordance with the present disclosure is shown in
Hook 12 includes an adjustable hook end 11 and a hook body 13 as shown in
Latch mechanism 10, including hook 12, is rotatable about an axis A extending through bushing 18 during opening and closing of latch mechanism 10 as suggested in
Handle 14 and linkage 16 control movement of hook 12 relative to a keeper 90 mounted on an adjacent component to the component that latch mechanism 10 is mounted to as suggested in
Latch mechanism 10 is shown in a locked position in
Trigger 17 includes a button pad 42 and a catch 44 as shown in
A pop-up spring 37 engages with retainer 46 to rotate handle 14 about axis C when catch 44 is released from retainer 46 as suggested in
An exploded assembly view of latch mechanism 10 is shown in
A rivet 33 extends through frame 15 and through hook body 13 to mount handle 14 for rotation about axis C relative to hook 12 as suggested in
Trigger 17 is coupled to frame 15 by a rivet 41 as suggested in
Adjustable hook end 11 includes a head 50 and an adjuster 53 as shown in
A pin 57 extends into a passage 25 of hook body 13 to engage with shaft 52 of head 50 as suggested in
A spring assembly 60 and a spring washer 54 extend into pocket 23 with adjuster 53 as suggested in
Another embodiment of an illustrative latch mechanism 210 in accordance with the present disclosure is shown in
Hook 212 includes an adjustable hook end 211 and a hook body 213 as shown in
Latch mechanism 210, including hook 212, is rotatable about an axis E extending through bushing 218 during opening and closing of latch mechanism 210 as suggested in
Handle 214 and linkage 216 control movement of hook 212 relative to a keeper 290 mounted on an adjacent component to the component that latch mechanism 210 is mounted to as suggested in
Latch mechanism 210 is shown in a locked position in
Trigger 217 includes a button pad 242 and a catch 244 as shown in
A pop-up spring 237 engages with retainer 246 to rotate handle 214 about axis G when catch 244 is released from retainer 246 as suggested in
An exploded assembly view of latch mechanism 210 is shown in
Rivet 236 extends through a hole 221 formed through hook body 213 and engages with links 232, 234 along axis F to mount links 232, 234 for rotation about axis F as suggested in
A rivet 233 extends through frame 215 and through hook body 213 to mount handle 214 on hook 212 for rotation about axis G as suggested in
Trigger 217 is coupled to frame 215 by a rivet 241 as suggested in
Adjustable hook end 211 includes a head 250 and an adjuster 253 as shown in
A pin 257 extends into a passage 225 of hook body 213 to engage with shaft 252 of head 250 as suggested in
A spring assembly 260 and a spring washer 254 extend into pocket 223 with adjuster 253 as suggested in
In illustrative embodiments, a latch mechanism 10 includes a hook 12 and a linkage connection 16 operatively associated with the hook 12 and a handle 14. A hook end 11 adjustably extends from a body 13 of the hook 12. A trigger assembly 17 is operatively coupled to the handle 14 and engages with a portion of the body 13 to retain the handle 14 in a latched position as shown in
In illustrative embodiments, the opening 28 of the body 13 is a relatively large passage having a generally partially arcuate shape. The arcuate shape is generally radially positioned from an axis B of the rivet 36. The mounting bushing 18 extends along a central axis A that travels through the passage 28 a generally consistent distance from the axis B throughout the range of travel. The first end of the auxiliary link 34 includes an elongated slot 39 providing some range of motion for movement of the rivet 45 attached to the handle 14. This range of motion helps the linkage 16 to be engaged in an over-center condition when the latch 10 is locked. This also provides some degree of travel of the handle 14 when the trigger 17 is actuated.
In illustrative embodiments, the latch mechanism 10 is shown in the open condition in
In illustrative embodiments, the high offset is defined by the parameters of the surrounding envelope, locking structure, and surface contour of the structure in which the latch mechanism 10 is installed. The present disclosure shows that the difficult problem of matching a contour profile of the surrounding structure can be solved through additional features that provide unique functions to achieve the goals and overcome the problems associated with this environment. The body 13 includes a pair of extending flanges which provide spaced away mounting points for the handle 14 that is attached thereto with a rivet 33.
In illustrative embodiments, a double torsion handle spring 31 is carried on the body 13 independent arms engaged against corresponding portions of the handle 14. The independent arms allow for independent engagement of each arm against the inside surface of the handle 14. This is useful because the handle 14, as shown in the Figures, is not a direct symmetric design. In other words, the handle 14 has an asymmetric configuration to accommodate a contour associated with the component to which it is attached. It can be seen that a first flange of the handle 14 has a different side dimension than a second flange of the handle 14, which has a larger corresponding side dimension. This allows the latch mechanism 10 to be housed in a generally orthogonal envelope and allows the handle 14 to be the component that accommodates the variation in the corresponding surface through which the handle 14 is positioned. In other words, the handle 14 accommodates the overall contour and structure of a panel, for example, through which an opening is formed and the handle 14 is flush mounted or flush positioned. As a result, both arms of the spring 31 transfer spring energy to the handle to pop the handle into the upward position when the trigger is disengaged. The double torsion handle spring 31 also may be designed to provide slightly greater force on one arm than the other to try to balance and equalize the overall force on the handle 14.
In illustrative embodiments, a trigger spring 47 and a pop-up spring 37 can also be made as double torsion springs similar to handle spring 31. As shown for example in
In illustrative embodiments, the hook end 11 includes a grip 51 and a shaft 52 that extends through a shaft passage 29 in the hook body 13. The shaft 52 includes threads that are engaged by an adjustment nut 53 retained in a nut pocket 23. The nut pocket 23 retains the nut 53 against horizontal movement along the passage 29 and provides rotary movement of the nut 53 to advance or retract the shaft 52 by engagement of the threads with corresponding threads inside the nut 53. The threaded shaft 52 provides controllable and retainable adjustment of the hook end 11 relative to the hook body 13. A detent component 60 has engageable detent structures that engage corresponding detent recesses on the nut 53 to retain the nut 53 in a selected adjustment. A sleeve 55 is provided in the shaft 52 to facilitate movement of the shaft 52 through the passage 29. A wave spring 54 is provided to provide some end load on the adjustment nut 53 retained in the pocket 23 and to retain the detent structures in engagement. The sleeve 55 axially inserts or telescopes through the wave spring 54 and a portion of the adjustment nut 53 to provide engagement within the pocket 23. A step rivet 57 is provided to extend through notches in the sleeve 55 and engage a hole 25 to retain the assembly against removal from pocket 23.
In illustrative embodiments, the latch mechanism 10 is used to retain components of a structure such as an aircraft having movable or removable components which can be retained in a closed or attached position by use of the latch mechanism 10. The hook 12 of this latch mechanism 10 engages a keeper 90 on the opposing component to provide a mechanical structural connection between the two components. When the latch mechanism 10 is disengaged or actuated to the opened position, the hook 12 can be disengaged from the keeper 90 to allow the structures to be disengaged.
In illustrative embodiments, the handle 14 is in a downward or locked position and the linkage 16 is in an over center condition to retain the latch mechanism 10 is a locked state as suggested in
In illustrative embodiments, the trigger 17 is actuated by pressing on a portion of the trigger button 42 marked “push” resulting in operating against the biasing force of the spring 47 to pivot the arms 44 about the corresponding rivet 41 to facilitate disengagement of the latch mechanism 10. The pop-up spring 37 forces the handle 14 away from the hook body 13 and though the opening to allow an operator to grasp an extending portion of the handle 14. The handle 14 is pivotable about the pivot point C extending through the spring rivet 33. The high offset provided by structure of the latch mechanism helps to minimize the sweep envelop or the space needed to allow the handle 14 to move. As the handle 14 is operated into the fully opened position, the links 32, 34 are placed in tension with the rivet 45 moving into the upward position in the slot 39 of the auxiliary link 34. Pulling or tension forces in the auxiliary link 34 are distributed over the link body that is strengthened because of the embossed portion. The handle 14 is moved downwardly to reengage the latch mechanism 10 and the hook 12 engages the corresponding keeper 90. Continued movement of the handle 14 downwardly causes the links 32, 34 to articulate and the rivet 45 moves from the upward position into a downward position in the slot 39 causing the axis A of the mounting bushing 18 to shift slightly below the centerline D, resulting in an over-center condition to help retain the latch mechanism 10 in a locked position.
In illustrative embodiments, where high profile handle contour is needed, auxiliary links are used in combination with load links in a latch mechanism. The auxiliary links transfer handle motion to the load links and mounting bushing to open and close the latch mechanism. These links eliminate the oversized handle shape due to the high offset from the mounting bushing to the handle pivot point. This also simplifies and reduces the manufacturing cost, envelope, and weight. The handle sweep envelope is also minimized.
While the present disclosure describes various exemplary embodiments, the disclosure is not so limited. To the contrary, the disclosure is intended to cover various modifications, uses, adaptations, and equivalent arrangements based on the principles disclosed. Further, this application is intended to cover such departures from the present disclosure as come within at least the known or customary practice within the art to which it pertains. It is envisioned that those skilled in the art may devise various modifications and equivalent structures and functions without departing from the spirit and scope of the disclosure as recited in the following claims. The scope of the following claims is to be accorded the broadest interpretation to encompass all such modifications and equivalent structures and functions.
This application claims priority under 35 U.S.C. § 119(e) to U.S. Provisional Application Ser. No. 62/306,620, filed Mar. 10, 2016, which is expressly incorporated by reference herein.
Number | Name | Date | Kind |
---|---|---|---|
2904141 | Henrichs | Sep 1959 | A |
4053177 | Stammreich | Oct 1977 | A |
4116479 | Poe | Sep 1978 | A |
4159137 | Richter | Jun 1979 | A |
4183564 | Poe | Jan 1980 | A |
4318557 | Bourne et al. | Mar 1982 | A |
4602812 | Bourne | Jul 1986 | A |
4618557 | Dan et al. | Oct 1986 | A |
4743052 | Stammreich | May 1988 | A |
4768815 | Harmon | Sep 1988 | A |
4828299 | Poe | May 1989 | A |
4858970 | Tedesco | Aug 1989 | A |
4877274 | Poe | Oct 1989 | A |
4991885 | Poe | Feb 1991 | A |
5152559 | Henrichs | Oct 1992 | A |
5445422 | Weinerman | Aug 1995 | A |
5620212 | Bourne et al. | Apr 1997 | A |
5984382 | Bourne et al. | Nov 1999 | A |
6279971 | Dessenberger, Jr. | Aug 2001 | B1 |
6325428 | Do | Dec 2001 | B1 |
6343815 | Poe | Feb 2002 | B1 |
7066501 | Meineke | Jun 2006 | B2 |
8573934 | Soulier | Nov 2013 | B2 |
8864185 | Do | Oct 2014 | B2 |
8864189 | Fournie et al. | Oct 2014 | B2 |
8925979 | Hernandez | Jan 2015 | B2 |
9004548 | Joret | Apr 2015 | B2 |
9273488 | Yu | Mar 2016 | B1 |
9580945 | Artin | Feb 2017 | B2 |
9617767 | Baic | Apr 2017 | B1 |
9677306 | DeFrance | Jun 2017 | B2 |
10173782 | Hernandez | Jan 2019 | B2 |
10443279 | Kim | Oct 2019 | B2 |
20080129056 | Hernandez et al. | Jun 2008 | A1 |
20090051170 | Baic | Feb 2009 | A1 |
20110133489 | Hemeury et al. | Jun 2011 | A1 |
20110174929 | Rowbut et al. | Jul 2011 | A1 |
20110227350 | Do | Sep 2011 | A1 |
20120102842 | Fournie | May 2012 | A1 |
20120151724 | DeFrance | Jun 2012 | A1 |
20130328326 | DeFrance | Dec 2013 | A1 |
20150259957 | Hernandez | Sep 2015 | A1 |
20160069118 | Artin | Mar 2016 | A1 |
20170058583 | Kim et al. | Mar 2017 | A1 |
20170260782 | Kim et al. | Sep 2017 | A1 |
Number | Date | Country |
---|---|---|
0839714 | May 1998 | EP |
1091059 | Apr 2001 | EP |
1927711 | Jun 2008 | EP |
2547848 | Aug 2015 | EP |
Number | Date | Country | |
---|---|---|---|
20170260782 A1 | Sep 2017 | US |
Number | Date | Country | |
---|---|---|---|
62306620 | Mar 2016 | US |