The present invention relates to a cinch latch, which connects a first structural element to a keeper on a second structural element. More specifically, the invention relates to aircraft panel latches having a hook at one end and an over-center locking linkage at the other.
A wide variety of latching mechanisms for use in aircraft exist in the prior art because aircraft have many components, such as fuselage panels including cowlings and the like, which must be opened and closed very securely. For example, tension latches mounted on one panel cinch to a keeper on a second panel to hold one of the movable panels closed. Other latches include sliding toggle linkages to minimize the kinematic envelope of the latch. These linkages rotate around a mounting pin to produce the latch reach. The complexity of quality aircraft latches makes them relatively large and heavy. Since every component of an aircraft should be as light as possible, it would be desirable to provide a quality latch having a reduced size and weight compared to the prior art.
To reduce weight, aircraft panels are relatively thin, which translates to an associated reduction in sturdiness. As a result, the aircraft panels and other structures to which the above-described latches are attached are delicate and can be easily damaged. For example, with some prior art latches, the free end of an open latch may obstruct the opening defined by the movable panel. Therefore, when closing the movable panel, it can strike the latch and be damaged if the latch is not properly retracted. This problem is often encountered with open overhead panels where gravity biases the latch assembly in the closed direction, thereby orienting the hook in an extended position pointing upwardly. This configuration occurs if the center of gravity of the latch is “behind” (in the direction away from the hook) the pivot point of the panel mounting pin. If this occurs, the hook end of the latch could be jammed against the edge of the mating substructure if the latch isn't first pulled away before attempting to close the panel. This weight distribution problem is often solved by adding unnecessary or “dead” weight to the hook end of the latch so that it hangs downward and away from the load plane. However, this solution contradicts a salient aircraft design consideration of weight reduction. Therefore, it would be desirable to provide a quality latch that reduces the risk of accidental damage to the surrounding aircraft structures to which it is attached.
The invention comprises a latch mechanism with an arrangement of components that places the center of gravity of the mechanism in front of the mounting pin. Therefore, in applications where the latch swings in the vertical plane, the hook will necessarily hang downward away from the keeper when the latch is opened without the need for adding dead weight. This functionality has been achieved in part by locating the mounting pin slot at the very end of the latch arm and arranging the toggle linkage so that the linkage-to-hook pivot joint is on the body of the latch arm in front of the mounting pin. In one embodiment of the invention, the alignment function of the hook body employs a rod and cylinder slide mechanism in place of the hook body slot.
The latch includes a unique nesting toggle linkage that minimizes overall latch volume. Each link of the linkage has a U-shaped lateral cross section with a central channel that receives the other link when the latch is closed. Furthermore, the links fold toward each other instead of away from each other while closing, which reduces the latch's overall length when fully closed. The latch may include a keeper detector, which prevents the actuation handle from closing if the keeper is not captured by the hook. The keeper detector helps prevent unsuccessful latching and provides a visual indication when a panel is closed but the keeper is not engaged.
Before explaining at least one embodiment of the invention in detail, it is to be understood that the invention is not limited in its application or to the details of construction in the following description or illustrated in the drawings. The invention encompasses numerous other embodiments and can be carried out in various ways.
A latch in accordance with one preferred embodiment of the invention is illustrated and described with respect to
The upper link 1 is constructed of thin sheet metal and has side walls that surround other internal components of the latch to minimize the latch's overall volume and weight. The upper link 1 operably pivots about a mounting pin 8 that connects the latch to an associated fixed structure such as a portion of an aircraft (not shown). Rivets 7 straddle the front walls of the upper link and hingedly connect it to the front of a lower link 10, which nests inside a central channel of the upper link 1. The lower link 10 is also pivotally connected to an elongate latch arm 6 by a pin 5. The rear walls of the latch arm 6 include a pair of slots 6b in which the mounting pin 8 can translate. Each link includes a center channel between opposing thin sidewalls forming a U-shaped lateral cross section. When assembled, the body of the latch arm 6 nests within the lower link 10, which in turn nests within the upper link 1. This nested configuration provides a very compact device as better appreciated when viewing
A handle 3 is rotatably connected to the lower link 10 and the upper link 1 by a pin 17, which carries a spring 22 that biases the handle upward away from the lower link 10 toward the open position of the latch. The location of the pin 17 permits a small amount of free travel of the handle. Likewise, another spring 18 biases the lower link upward away from the latch arm 6 to hold the latch open. The handle 3 actuates the latch between open and closed positions. After a limited amount of free movement restricted by the back end of the handle abutting the lower link 10, continued lifting of the handle 3 will lift the lower link upward, extending the hook and releasing the latch as best seen in
Referring now to
As described above, the handle extends and retracts a latch arm 6 having hook 4 at the front end. The hook 4 engages and grabs a keeper (not shown) in the closed position and applies a tensile clinch load between the keeper and the latch mounting pin 8.
The handle 3 includes a trigger 2 that releasably locks the handle 3 in a closed position. The trigger 2 is pivotally attached to the handle 3 by a pin 20, which includes a concentric sleeve 21 about which the handle can pivot to a limited extent. The trigger 2 releasably holds the handle 3 down in the configuration shown in
An exploded view of the latch arm 6, and the other latch components, is shown in
The trigger 2 is connected to the handle 3 by a pin 20. Another spring 12 biases the trigger 2 upwardly so that its top surface is flush with the top of the handle 3 when the latch is closed and locked as shown in
The various components discussed above are shown assembled and in the locked position viewed from the side and the top in
The compact design of the latch is best illustrated in
In
In
In
Another preferred embodiment of the invention is shown in
With the operational explanation of
The foregoing description is considered as illustrative only of the principles of the invention. Further, since numerous modifications and changes will readily occur to those skilled in the art, it is not desired to limit the invention to the exact construction and operation shown and described, and accordingly all suitable modifications and equivalents should be considered encompassed within the scope of the invention.
This application is a continuation-in-part of U.S. patent application Ser. No. 14/657,373 entitled “Toggle Link Latch” filed on Mar. 13, 2015, priority from which is hereby claimed.
Number | Name | Date | Kind |
---|---|---|---|
2714032 | Mills | Jul 1955 | A |
2904141 | Henrichs | Sep 1959 | A |
2927812 | Smith | Mar 1960 | A |
3259412 | Wheeler | Jul 1966 | A |
4053177 | Stammreich | Oct 1977 | A |
4602812 | Bourne | Jul 1986 | A |
4743052 | Stammreich et al. | May 1988 | A |
5620212 | Bourne | Apr 1997 | A |
5915765 | Sternberger | Jun 1999 | A |
5984382 | Bourne | Nov 1999 | A |
6036238 | Lallament | Mar 2000 | A |
6279971 | Dessenberger | Aug 2001 | B1 |
6325428 | Do | Dec 2001 | B1 |
6343815 | Poe | Feb 2002 | B1 |
8864185 | Do | Oct 2014 | B2 |
8925979 | Hernandez | Jan 2015 | B2 |
9677306 | DeFrance | Jun 2017 | B2 |
20080129056 | Hernandez et al. | Jun 2008 | A1 |
20100026482 | Grichener | Feb 2010 | A1 |
Number | Date | Country |
---|---|---|
0206648 | Dec 1986 | EP |
WO 2009009732 | Jan 2009 | WO |
Entry |
---|
International Search Report and Written Opinion of the International Searching Authority. PCT/US17/51980 dated Dec. 1, 2017. |
EPO, European Search Report, dated Nov. 18, 2015, Publisher: European Patent Office, Published in: European Patent Office. |
Number | Date | Country | |
---|---|---|---|
20160264250 A1 | Sep 2016 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 14657373 | Mar 2015 | US |
Child | 14733412 | US |