The present disclosure relates generally to a latch for an aircraft engine nacelle, and more specifically to a locking mechanism for such a latch.
A variety of latches are used on aircraft to retain various components of the aircraft in a locked condition under circumstances such as flight and storage of the aircraft. During maintenance or repair periods the latches must operate to unlock the corresponding panel, cowling or other device from the aircraft. For example, upon a cowling the latch is disengaged to allow the cowling to be operated away from the engine components which it houses. The cowling, once opened, allows the aircraft maintenance professional to access the engine components. At the end of the repair event the cowling is closed. The latch is used to lock the cowling in the closed condition to retain the engine components in the housed condition.
As an additional matter, the maintenance professional may use a device to “clip” the latches closed to keep them from projecting out from the aircraft body or housing. The latches are clipped in a closed or lower profile position to prevent the latches from becoming bumped or from bumping the maintenance professional. Clipping the latches does not necessarily close or lock the latch but allows the latch to be maintained in a much lower profile against the aircraft housing or body. Since the latches are in a lower profile configuration, they reduce the chance of the maintenance professional bumping into them either with his body or with a piece of equipment. This can be useful to protect the latches as well as the maintenance professional. However, clipped latches can inadvertently appear to be locked and as such may fail to be locked. Additionally, even if the latches are operated to attempt to lock them a potential issue with the latch mechanism might interfere with complete locking and as such could inadvertently unlatch during operation. It would be desirable to develop a system and assembly to be used with a latch to help provide assurances that the latch will, in fact, be closed and locked in the proper position.
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.
The present disclosure includes a clevis-sensing lock assembly for use with a latching system. The clevis-sensing lock can be installed into the latching system and provides structures which function to prevent operation of the clevis in the unlocked position. A device such as a key or tool is used to unlock the latch and allow it to open. The structure and function of the clevis-sensing lock retains this device in the lock to prevent its removal unless the latch is in the fully closed position. Once in the fully closed position the lock can be closed and the device removed. Additionally, an indicator or flag can be added to the device to further enhance the visibility of the locked or unlocked condition of the latch. The lock provides structures which function to interfere with the operation of the clevis until the latch is in the desired closed and confirmed locked position. The clevis-sensing lock can be used with a specially designed latch or retrofitted to be used with a variety of latches. The variety of latches can be remanufactured to provide the same or substantially the same envelope of operation using virtually the same components but replacing portions of the trigger assembly with the lock assembly.
According to the present disclosure, a latch mechanism includes a hook-handle assembly, a clevis, and a clevis-sensing lock. The hook-handle assembly may include a hook member, a handle, and a linkage arrangement coupled between the hook member and handle. The clevis may include a hook-end receiver and a coupler portion spaced apart from the hook-end receiver to at least partially define an opening therebetween.
In illustrative embodiments, the hook-end receiver may be configured to engage with a hook end of the hook member as the handle moves from an open position extending away from the clevis toward a closed position extending toward the clevis.
In illustrative embodiments, the clevis-sensing lock may be coupled to the handle to move with the handle. The clevis-sensing lock may include a block, a lock cylinder received in the block and configured to rotate relative to the block, and an interference member coupled to the lock cylinder to rotate with the lock cylinder relative to the block.
In illustrative embodiments, the interference member may be configured to pass through the opening of the clevis and rotate relative to the block to engage an underside of the clevis and the lock cylinder may be configured to control rotation of the interference member.
In illustrative embodiments, the latch mechanism may further include a tumbler arrangement coupled between the lock cylinder and the block and configured to control rotation of the lock cylinder relative to the block.
In illustrative embodiments, the tumbler arrangement may include a detent spring, a detent pin positioned between the lock cylinder and the detent spring, and a tumbler pin positioned between the detent pin and the lock cylinder. The detent spring may be configured to bias the detent pin toward the tumbler pin. The detent pin may be configured to engage with the block and the lock cylinder to restrict rotation of the lock cylinder when an interface between the detent pin and the tumbler pin is misaligned from a lower surface of the lock cylinder.
In illustrative embodiments, the latch mechanism may further include a key configured to be received in the lock cylinder to engage with the tumbler pin and to align the interface between the detent pin and the tumbler pin with the lower surface of the lock cylinder.
In illustrative embodiments, the latch mechanism may further include a key having a head and a shaft coupled to the head. The shaft may be configured to be received in the lock cylinder to engage with the tumbler arrangement to allow rotation of the lock cylinder and the head may be configured to extend away from the handle to provide an indication of an unlocked state of the clevis-sensing lock.
In illustrative embodiments, the key may further include a protrusion extending outward from the shaft and configured to engage with the handle to trap the shaft within the lock cylinder when the lock cylinder is rotated relative to the block.
In illustrative embodiments, the lock cylinder may be formed to include an annular groove and an axial slot extending toward the interference member from the annular groove.
In illustrative embodiments, the latch mechanism may further include a cross-pin configured to slide in the annular groove and axial slot of the lock cylinder to control rotation of the lock cylinder.
In illustrative embodiments, the latch mechanism may further include the clevis may further include a fin extending from an upper surface clevis opposite the underside. The fin may be configured to move the cross-pin out of the axial slot and into the annular groove to allow rotation of the lock cylinder as the handle moves toward the closed position.
In illustrative embodiments, the lock cylinder may be formed to include a groove extending at least partially around a circumference of the lock cylinder. A fastener may extend through the handle and the block to couple the clevis-sensing lock to the handle and may be received in the groove of the lock cylinder.
In illustrative embodiments, the groove of the lock cylinder may be configured to limit rotation of the lock cylinder relative to the block.
According to the present disclosure, a method of operating a latch mechanism may include inserting a key into a clevis-sensing lock through an aperture formed in a handle of a hook-handle assembly, rotating the key to disengage an interference member of the clevis-sensing lock from a clevis, moving the handle relative to the clevis to disengage a fin of the clevis from the clevis-sensing lock to engage a cross-pin of the clevis-sensing lock with a lock cylinder of the clevis-sensing lock to block rotation of the key such that the key is trapped in the clevis-sensing lock, and moving the handle to disengage a hook member of the hook-handle assembly from the clevis.
In illustrative embodiments, the method may further include moving the handle toward the clevis to engage the hook member with the clevis, moving the handle toward the clevis to engage the fin with the clevis-sensing lock to disengage the cross-pin from the lock cylinder to allow rotation of the key, rotating the key such that the interference member is engaged with an underside of the clevis, and removing the key from the clevis sensing lock.
In illustrative embodiments, inserting the key may include extending a shaft of the key into the lock cylinder and engaging a tumbler arrangement to allow rotation of the interference member.
In illustrative embodiments, removing the key may include removing the shaft from the lock cylinder and disengaging the tumbler arrangement to block rotation of the interference member.
According to the present disclosure, a clevis-sensing lock may include a block, a lock cylinder, a cross-pin, a tumbler arrangement, a coupler shaft, and an interference member. The block may be formed to include a cylinder-receiving bore extending into the block and a pin-receiving slot extending into the block to intersect with the cylinder-receiving bore. The lock cylinder may be configured to be received in the cylinder-receiving bore of the block and rotate relative to the block. The lock cylinder may include a first end and a second end spaced apart from the first end. The lock cylinder may be formed to include an annular groove, an axial slot extending toward the first end of the lock cylinder from the annular groove, and a key-receiving bore extending from the second end toward the first end.
In illustrative embodiments, the cross-pin may be positioned within the pin-receiving slot of the block and configured to slide in the annular groove and axial slot of the lock cylinder to control rotation of the lock cylinder.
In illustrative embodiments, the tumbler arrangement may be coupled between the lock cylinder and the block and configured to control rotation of the lock cylinder.
In illustrative embodiments, the coupler shaft may be positioned within the key-receiving bore and coupled with the lock cylinder to rotate therewith.
In illustrative embodiments, the interference member may be coupled to the coupler shaft at the first end of the lock cylinder to rotate with the lock cylinder.
In illustrative embodiments, the clevis-sensing lock may further include a guide pin having a head and a hole extending through the head. The block may be formed to include a cavity configured to receive the guide pin. The cross-pin may extend through the hole of the guide pin.
In illustrative embodiments, the tumbler arrangement may include a detent spring, a detent pin positioned between the lock cylinder and the detent spring, and a tumbler pin positioned between the detent pin and the lock cylinder. The detent spring may be configured to bias the detent pin toward the tumbler pin. The detent pin may be configured to engage with the block and the lock cylinder to restrict rotation of the lock cylinder when an interface between the detent pin and the tumbler pin is misaligned from a lower surface of the lock cylinder.
In illustrative embodiments, the clevis-sensing lock may further include a fastener extending through the block. The lock cylinder may be formed to include a groove extending at least partially around a circumference of the lock cylinder. The fastener may be received in the groove of the lock cylinder. The groove of the lock cylinder may be configured to limit rotation of the lock cylinder relative to the block.
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.
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 the best mode 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 foregoing terms as well as other terms 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.
An engine assembly 10 for attachment with an aircraft is shown in
A latch mechanism 30 is coupled between panels 13, 15 to secure panels 13, 15 in the closed position at the selection of a user as suggested in
As such, latch mechanism 30 includes a hook-handle assembly 32 coupled to one of panels 13, 15 and a clevis 34 coupled to the other of panels 13, 15 as suggested in
A key 80 is inserted into clevis-sensing lock 50 to unlock latch mechanism 30 as suggested in
Hook-handle assembly 32 includes a handle 42 used to operate latch mechanism 30, a hook member 40, and a linkage arrangement 44 coupled between handle 42 and hook member 40 as suggested in
Clevis 34 includes a hook-end receiver 62 for engaging with a hook end 60 of hook member 40 and a coupler portion 140 coupled to a clevis retainer 38 as suggested in
Clevis-sensing lock 50 includes a block 64 coupled to an underside surface 116 of handle 42 and a coupler shaft 68 configured to couple interference member 56 with block 64 as suggested in
To assemble clevis-sensing lock 50, coupler shaft 68 is positioned within bore 92 of lock cylinder 102, and a pin 100 is engaged with holes 103, 105 of coupler lock cylinder 102 and coupler shaft 68, respectively, as suggested in
Tumbler pins 122 are inserted into corresponding bores within lock cylinder 102 and lock cylinder 102 is inserted into bore 154 of block 64 as suggested in
Guide pins 110 are received in cavities 76 of block 64 as suggested in
Interference member 56 includes protruding portions 150 and flats 142 extending between protruding portions 150 as shown in
Clevis-sensing lock 50, as assembled, is shown in
Key 80 includes head 84 and shaft 98 coupled to head 84 as shown in
In the locked orientation, an interface between tumbler pins 122 and detent pins 130 is misaligned from a bottom plane P of lock cylinder 102 such that detent pins 30 engage with lock cylinder 102 and block 64 to prevent rotation of lock cylinder 102 as suggested in
As key 80 is rotated to unlock clevis-sensing lock 50, protrusion 94 extends under handle 42 and becomes misaligned from aperture 82 as suggested in
Lock cylinder 102 is formed to include a groove 170 as shown in
Once clevis-sensing lock 50 is unlocked by key 80, latch mechanism 30 can be opened as suggested in
Fins 72 of clevis 34 are engage with guide pins 110 to allow rotation and removal of key 80 as suggested in
A hook-handle assembly 32a incorporating an alternative clevis-sensing lock 50a in accordance with the present disclosure is shown in
Clevis-sensing lock 50a includes a block 64a and a lock cylinder 102a configured to couple an interference member 56a with block 64a as suggested in
Lock cylinder 102a is formed to include a bore 92a aligned with an aperture 82a of handle 42a and configured to receive a shaft 98a of a key 80a for rotation of lock cylinder 102a and interference member 56a as suggested in
To assemble clevis-sensing lock 50a, a tamper guard 186a, key interface 68a, a spring 136a, and a spacer 188a are inserted into lock cylinder 102a and retained therein by a retainer ring 189a as suggested in
Guide pins 110a are received in cavities 76a of block 64a as suggested in
A ball detent assembly 172a is positioned within a ball detent receiver 178a as suggested in
Similar to interference member 56, interference member 56a includes protruding portions 150a and flats 142a extending between protruding portions 150a as shown in
Clevis-sensing lock 50a, as assembled, is shown in
Key 80a is inserted into clevis-sensing lock 50a to move pin assembly 104a out of notch 184a as suggested in
Shaft 98a of key 80a is formed to include a groove 95a as suggested in
Clevis-sensing lock 50a includes anti-tamper features as suggested in
In illustrative embodiments, the clevis-sensing locks described herein can be configured for use with a specific latch design or configured to be used as a retrofit on a remanufactured latch. An existing latch assembly can reuse most of the parts with perhaps a modification to the handle to remove a pre-existing handle release and to accommodate a clevis-sensing lock. Additionally, the clevis can be replaced merely by disengaging the threaded portion of the old clevis and attaching a new clevis which will include the fins and other corresponding structures detailed above. This design is easy to operate, difficult to defeat, and provides a nearly fail-proof method of ensuring the latch has properly secured the latch cowl.
In illustrative embodiments, a clevis-sensing lock can be retained on a latch mechanism for preventing the latch mechanism from opening inadvertently. The clevis-sensing lock includes a tool, key, or other device which must be used to unlock the clevis-sensing lock to permit movement of the handle to disengage the latch mechanism. The key cannot be removed from the lock when the latch is open. Furthermore, the key includes a visual indicator such as a flag, streamer, or other device which provides a clear visual indicator that the key is retained in the lock. This visual indicator extends away from the aircraft to provide a clear visual indication of the unlatched condition. Since the key can only be removed from the lock when the latch is, in fact, in a proper closed position, the presence of such a visual indicator indicates that the latches are not secure for flight operations.
Engine cowls may sometimes appear to be in a latched closed position when they are not due to the low profile of the latches and low height from the ground of the engines of the aircraft. It is often times that technicians will clip the latches up tight against the cowling without latching them to prevent snags with clothing during operations on the engine. These situations can be problematic if an aircraft takes off while the latches are open, and may cause damage to the cowlings or engines while in flight.
In illustrative embodiments, a clevis sensing lock can be attached to any hook latch that engages with a clevis. The clevis sensing lock attaches to the handle of the hook latch, and passes through the clevis when the latch is closed. It requires a key or tool to unlock the latch and allow the latch to open. When the latch is open, the key cannot be removed from the handle. They key has a long flag or streamer attached to it so that anybody standing around the aircraft, not necessarily near the engine, can see that the cowls are not closed and latched. To unlatch the cowls, the operator inserts the key, with the long flag or streamer attached, into the latch, turns the key, then opens the latch.
In illustrative embodiments, the lock includes a block which holds all of the lock's internal parts to the handle of the hook latch. The block has a large hole for a lock cylinder, and some slots and holes for some pins, guides, and springs. Another pair of slots on the block allows fins that are attached to the clevis to fit into the block. The T-shaped lock cylinder, which fits into the block, has two large flats on one end, which allows it to fit through the clevis during handle opening and closing.
In illustrative embodiments, at the other end of the lock, there is a hole for a key to fit into. Near the open end of the hole, the lock cylinder has a retaining groove that protrudes into the hole, but only part way around the lock cylinder. This groove on the lock cylinder engages with a rivet that passes through the handle and through the block in such a way that the lock cylinder cannot come out of the lock, and in such a way that the lock cylinder can only turn a predetermined amount. The rivet protrudes into the hole of the lock such that the key has a corresponding flat on it that allows the key to pass by the rivet when the latch is closed. When the key is inserted into the lock, a groove on the key matches the groove on the lock cylinder that engages with the rivet that holds the lock cylinder in place. When the key is turned, the groove on the key engages with the rivet, which prevents the key from being removed.
In illustrative embodiments, the end of the key has a feature which grabs onto a mating component, sometimes called a plug, down in the bottom of the hole of the lock cylinder. The shape at the end of the key can be any shape that allows the key to grab the plug and turn it. The plug has a spring behind it, and a hole for a cross pin, which fits into a through slot on the lock cylinder. The cross pin limits the amount of axial movement in the lock cylinder and also ensures that the key, plug, and lock cylinder turn together. When the key is not inserted into the lock, the cross pin is pushed by the spring, via the plug, into a V-groove on the block, thereby preventing accidental rotation of the lock cylinder when the latch is closed. When the key is inserted into the lock, the cross pin is pushed out of the V-groove on the block, and the cylinder is allowed to turn. With this arrangement of the key, lock cylinder, and plug, they cannot be turned unless the key is fully inserted into the lock cylinder and engaged with the plug.
In illustrative embodiments, the lock cylinder also has a circular groove and two intersecting straight slots, which are parallel to the axis of the lock cylinder, that allow the ends of two locking pins to travel in them. The locking pins ride in a guide, inside the block. Each guide is pushed by a spring toward the clevis. The clevis has two fins which, in the latch closed position, engage with the guides, and push the guides and locking pins into the circular groove. When the locking pins are in the circular groove, the lock may be turned toward the unlock position. Once the lock cylinder is turned completely to the unlock position, the handle may be moved in the direction that opens the latch, and the engaging portion of the lock may pass through the clevis. The clevis has two fins which fit into some blind slots on the block, and push the guides and locking pins when the latch is closed. As the latch opens, and the handle moves away from the clevis, the fins on the clevis disengage from the guides and locking pins. The locking pins are then pushed down into the straight slots on the lock cylinder, which prevents the lock cylinder from turning toward the lock position and prevents the key from being removed.
In illustrative embodiments, there could be one or two flats on opposing sides of the lock cylinder. The locking pins would be longer and offset from the axis of the cylinder, such that they would fit tangentially into the circular groove on lock cylinder when the latch is in the closed position. When the latch is open, the locking pins would slide down onto the flats of the lock cylinder and prevent the lock cylinder from turning.
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 so as to encompass all such modifications and equivalent structures and functions.
This application is a Continuation of copending U.S. patent application Ser. No. 16/393,646, filed Apr. 24, 2019, which is a Divisional of U.S. patent application Ser. No. 15/510,139, filed Mar. 9, 2017 (Now U.S. Pat. No. 10,392,830), which is a U.S. nationalization under 35 U.S.C. § 371 of International Application No. PCT/US2015/049216, filed Sep. 9, 2015, which claims priority under 35 U.S.C. § 119(e) to U.S. Provisional Application No. 62/048,247, filed Sep. 9, 2014. The disclosures set forth in the referenced applications are incorporated herein by reference in their entireties.
Number | Name | Date | Kind |
---|---|---|---|
2592647 | Black | Apr 1952 | A |
2601577 | Whitmore | Jun 1952 | A |
2677261 | Jacobi | May 1954 | A |
2710214 | Summers | Jun 1955 | A |
2722445 | Cudney | Nov 1955 | A |
2904141 | Henrichs | Sep 1959 | A |
2982121 | George | May 1961 | A |
3070395 | Morrison et al. | Dec 1962 | A |
3194595 | Wheeler et al. | Jul 1965 | A |
3209563 | Pelcin | Oct 1965 | A |
3261188 | Kerr | Jul 1966 | A |
3279836 | Swanson | Oct 1966 | A |
3320783 | Kerr | May 1967 | A |
3420077 | Drazin | Jan 1969 | A |
3509748 | Trainor | May 1970 | A |
3541819 | Kerr | Nov 1970 | A |
3797289 | Mercurio | Mar 1974 | A |
3958821 | Scalera | May 1976 | A |
3961507 | Falk | Jun 1976 | A |
4053177 | Stammreich | Oct 1977 | A |
D246761 | Kelley | Dec 1977 | S |
4069696 | Steinbach | Jan 1978 | A |
4083211 | Scherbing | Apr 1978 | A |
4111020 | Scherbing | Sep 1978 | A |
4116479 | Poe | Sep 1978 | A |
4134281 | Pelcin | Jan 1979 | A |
4191036 | Steinbach | Mar 1980 | A |
4233828 | Dauenbaugh | Nov 1980 | A |
4268077 | Bohleen et al. | May 1981 | A |
4307905 | Poe et al. | Dec 1981 | A |
4413849 | Davis et al. | Nov 1983 | A |
4446709 | Steinbach | May 1984 | A |
4510779 | Ahad | Apr 1985 | A |
4613099 | Smith et al. | Sep 1986 | A |
4638649 | Chao | Jan 1987 | A |
4704884 | Sugimoto | Nov 1987 | A |
4735069 | Steinbach | Apr 1988 | A |
4736174 | Castonguay et al. | Apr 1988 | A |
4743052 | Stammreich et al. | May 1988 | A |
4899565 | Steinbach | Feb 1990 | A |
4911485 | Wasilewski | Mar 1990 | A |
4925221 | Carmody et al. | May 1990 | A |
4934164 | Shew | Jun 1990 | A |
4977768 | Embry | Dec 1990 | A |
5018376 | Lee | May 1991 | A |
5024072 | Lee | Jun 1991 | A |
5097686 | Plumer | Mar 1992 | A |
5201557 | Schlack | Apr 1993 | A |
5257839 | Nielsen | Nov 1993 | A |
5267762 | Gromotka | Dec 1993 | A |
5321962 | Ferchau et al. | Jun 1994 | A |
5400629 | Myers | Mar 1995 | A |
5402660 | Osada | Apr 1995 | A |
5435160 | Linsalato | Jul 1995 | A |
5454239 | Esaki | Oct 1995 | A |
5469725 | Yamada | Nov 1995 | A |
5518206 | Arnold et al. | May 1996 | A |
5595080 | Whinton | Jan 1997 | A |
5620212 | Bourne | Apr 1997 | A |
5638709 | Clavin | Jun 1997 | A |
5664813 | Gromotka | Sep 1997 | A |
5713482 | Bordner | Feb 1998 | A |
5765883 | Dessenberger et al. | Jun 1998 | A |
5819563 | Bianco | Oct 1998 | A |
5870917 | Mahot | Feb 1999 | A |
5984382 | Bourne | Nov 1999 | A |
6095567 | Buell | Aug 2000 | A |
6174007 | Schlack | Jan 2001 | B1 |
6196593 | Petrick | Mar 2001 | B1 |
6250556 | Schneider | Jun 2001 | B1 |
6255957 | Sonderegger | Jul 2001 | B1 |
6279971 | Dessenberger, Jr. | Aug 2001 | B1 |
6325428 | Do | Dec 2001 | B1 |
6343815 | Poe | Feb 2002 | B1 |
6513841 | Jackson | Feb 2003 | B1 |
6575005 | Hunter | Jun 2003 | B1 |
6644078 | Hung | Nov 2003 | B1 |
7017955 | Chiang | Mar 2006 | B1 |
7150168 | Kuo | Dec 2006 | B1 |
7162900 | Lu | Jan 2007 | B1 |
7185926 | Helsley et al. | Mar 2007 | B2 |
D548047 | Kearns | Aug 2007 | S |
D570196 | McKinnon | Jun 2008 | S |
7454934 | Lin | Nov 2008 | B2 |
7461871 | Vauchel | Dec 2008 | B2 |
7503600 | Hautala et al. | Mar 2009 | B2 |
8113551 | Baic et al. | Feb 2012 | B2 |
8186728 | Kopylov | May 2012 | B2 |
8356844 | Baic | Jan 2013 | B2 |
8419088 | Baic et al. | Apr 2013 | B2 |
8544900 | Elbrecht et al. | Oct 2013 | B2 |
8720237 | Williams | May 2014 | B2 |
8764072 | Gonidec | Jul 2014 | B2 |
8864185 | Do | Oct 2014 | B2 |
8864189 | Fournie | Oct 2014 | B2 |
9004548 | Joret et al. | Apr 2015 | B2 |
9140041 | Wollacott | Sep 2015 | B2 |
9169669 | Clary | Oct 2015 | B2 |
9169678 | Rozema | Oct 2015 | B2 |
9353559 | Fabre et al. | May 2016 | B2 |
9567784 | Defrance | Feb 2017 | B2 |
9587516 | Fabre et al. | Mar 2017 | B2 |
9650807 | Helsley | May 2017 | B2 |
9771739 | Wells | Sep 2017 | B1 |
10119299 | Wu | Nov 2018 | B1 |
10392830 | Helsley | Aug 2019 | B2 |
11193305 | Helsley | Dec 2021 | B2 |
20020195827 | Jackson et al. | Dec 2002 | A1 |
20030226385 | Chin-Shen | Dec 2003 | A1 |
20040104583 | Porte | Jun 2004 | A1 |
20040231379 | Yu | Nov 2004 | A1 |
20060214431 | Helsley et al. | Sep 2006 | A1 |
20070186601 | Lin | Aug 2007 | A1 |
20080129056 | Hernandez et al. | Jun 2008 | A1 |
20090134637 | Baic | May 2009 | A1 |
20110101710 | Elbrecht et al. | May 2011 | A1 |
20130238326 | DeFrance | Dec 2013 | A1 |
20140030079 | Provost et al. | Jan 2014 | A1 |
20140225380 | Gonidec | Aug 2014 | A1 |
20150184543 | Fabre et al. | Jul 2015 | A1 |
20150184544 | Fabre et al. | Jul 2015 | A1 |
20170356223 | Do | Dec 2017 | A1 |
Number | Date | Country |
---|---|---|
102011000443 | Jun 2012 | DE |
WO 2015126950 | Aug 2015 | WO |
Entry |
---|
U.S. Appl. No. 15/510,139, filed Mar. 9, 2017. |
U.S. Appl. No. 16/393,646, filed Apr. 24, 2019 |
Extended Search Report issued in Appl. No. EP19177555.0 (dated Sep. 25, 2019). Copy available in related U.S. Appl. No. 16/393,646 as noted in IDS filed in this application filed May 20, 2021. |
Office Action issued in Appl. No. CA2960880 (dated Dec. 2, 2021). |
Safety First—The Airbus Safety Magazine, Issue 14 (Jul. 2012). |
Number | Date | Country | |
---|---|---|---|
20210270057 A1 | Sep 2021 | US |
Number | Date | Country | |
---|---|---|---|
62048247 | Sep 2014 | US |
Number | Date | Country | |
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Parent | 15510139 | US | |
Child | 16393646 | US |
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Parent | 16393646 | Apr 2019 | US |
Child | 17326120 | US |