IP Library Granted Patent US 7,918,001
Granted Patent B2
US 7,918,001 · App. 12/060,095 · Granted Apr 5, 2011

Multi-pivot latch assemblies

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 7,918,001
App. No.
12/060,095
Granted
Apr 5, 2011
Kind
B2
Abstract

Multi pivot latch assemblies for releasably engaging anchors and other attach points in vehicles are disclosed herein. A latch assembly configured in accordance with one embodiment of the disclosure includes a latch and an actuator, each of which is movably coupled to a frame. In operation, movement of the actuator from a locked position toward an unlocked position causes the latch to rotate from a first position to a second position about a first pivot point, and from the second position toward the third position about a second pivot point to open the latch assembly and release the anchor.

Claims (54)

1. A latch assembly for releasably engaging an anchor in a vehicle, the latch assembly comprising:

a frame including a first engagement surface;

a latch movably coupled to the frame, the latch including a second engagement surface configured to cooperate with the first engagement surface to releasably engage the anchor in a space therebetween, wherein the latch is rotatable from a first latch position to a second latch position about a first pivot point located in the space between the first and second engagement surfaces, and wherein the latch is further rotatable from the second latch position to a third latch position about a second pivot point different from the first pivot point; and

an actuator movably coupled to the frame, wherein movement of the actuator from a first actuator position toward a second actuator position rotates the latch from the first latch position to the second latch position about the first pivot point, and from the second latch position to the third latch position about the second pivot point.

2. The latch assembly of claim 1 :

wherein the frame includes a first opening and a second opening; and

wherein the latch includes a first guide feature and a second guide feature, wherein the first guide feature is movably received in the first opening of the frame, and wherein the second guide feature is movably received in the second opening of the frame.

3. The latch assembly of claim 2 wherein the first opening has a generally “V” shape and the second opening has a generally linear shape.

4. The latch assembly of claim 1 :

wherein the frame includes a first opening and a second opening, wherein the first opening has a generally “V” shape and the second opening has a generally linear shape; and

wherein the latch includes a first guide pin and a second guide pin fixedly attached to the latch, wherein the first guide pin moves through the first opening and the second guide pin moves through the second opening during movement of the actuator.

5. The latch assembly of claim 1 wherein the frame includes a first jaw and the latch includes a second jaw, and wherein the anchor is retained between the first and second jaws when the latch is in the first latch position.

6. The latch assembly of claim 5 wherein the anchor is retained between the first and second jaws when the latch is in the second latch position, and wherein the second jaw is spaced apart from the first jaw to release the anchor when the latch is in the third latch position.

7. The latch assembly of claim 1 wherein the latch includes at least one guide feature projecting therefrom, and wherein the second pivot point is positioned at least proximate to the guide feature.

8. The latch assembly of claim 1 :

wherein the latch includes a guide feature projecting therefrom; and

wherein the actuator includes an end portion having an abutment surface that cooperates with the guide feature during movement of the actuator.

9. A latch assembly for releasably engaging an anchor in a vehicle, the latch assembly comprising:

a frame;

a latch movably coupled to the frame, wherein the latch is rotatable from a first latch position to a second latch position about a first pivot point, and wherein the latch is further rotatable from the second latch position to a third latch position about a second pivot point different from the first pivot point; and

an actuator movably coupled to the frame, wherein the actuator includes:

a proximal end portion having a channel extending therethrough;

a medial portion extending from the proximal end portion, wherein the medial end portion has a biasing member cavity extending therethrough and intersecting the channel; and

a distal end portion extending from the medial portion, wherein the distal end portion has a generally hook shape, and wherein movement of the actuator from a first actuator position toward a second actuator position rotates the latch from the first latch position to the second latch position about the first pivot point, and from the second latch position to the third latch position about the second pivot point.

10. A latch assembly for releasably engaging an anchor in a vehicle, the latch assembly comprising:

a frame having a first opening and a second opening;

a latch having a jaw portion that receives the anchor, wherein the latch further includes a first guide feature movably received in the first opening of the frame and a second guide feature moveably received in the second opening of the frame; and

an actuator movable relative to the frame, wherein movement of the actuator from a locked position toward an intermediate position pivots the latch about a pivot point positioned within a cross section of the anchor, and wherein continued movement of the actuator from the intermediate position toward an unlocked position pivots the latch about the second guide feature and releases the anchor from the jaw portion of the latch.

11. The latch assembly of claim 10 wherein the first opening is a first slot having a generally “V” shape, and wherein the second opening is a second slot having a generally linear shape.

12. The latch assembly of claim 11 wherein the second opening has a pivot surface, and wherein the second guide feature contacts the pivot surface when the latch pivots about the second guide feature.

13. The latch assembly of claim 10 wherein the first guide feature moves in a first direction in the first opening and the second guide feature moves in a second direction in the second opening when the latch pivots about the anchor, and wherein the first guide feature moves in a third direction in the first opening when the latch pivots about the second guide feature.

14. The latch assembly of claim 10 :

wherein the first opening has a generally “V” shape and the second opening has a generally linear shape;

wherein the first guide feature is a first pin fixedly attached to the latch, wherein the first pin cooperates with an abutment surface of the actuator; and

wherein the second guide feature is a second pin fixedly attached to the latch, wherein the second pin contacts a pivot surface of the frame during at least a portion of movement of the actuator.

15. A latch assembly for releasably engaging an anchor in a vehicle, the latch assembly comprising:

a frame having a first opening and a second opening;

a latch having a jaw portion that receives the anchor, wherein the latch further includes a first guide feature movably received in the first opening of the frame and a second guide feature moveably received in the second opening of the frame; and

an actuator movable relative to the frame, wherein movement of the actuator from a locked position toward an intermediate position pivots the latch about the anchor, and wherein continued movement of the actuator from the intermediate position toward an unlocked position pivots the latch about the second guide feature and releases the anchor from the jaw portion of the latch, wherein the frame includes a stop member and the actuator includes a cavity, and wherein the latch assembly further comprises a biasing member positioned in the cavity of the actuator, wherein the biasing member urges the actuator away from the stop member toward the locked position.

16. A latch assembly for releasably engaging an anchor in a vehicle, the latch assembly comprising:

a frame having a first opening and a second opening;

a latch having a jaw portion that receives the anchor, wherein the latch further includes a first guide feature movably received in the first opening of the frame and a second guide feature moveably received in the second opening of the frame; and

an actuator movable relative to the frame, wherein movement of the actuator from a locked position toward an intermediate position pivots the latch about the anchor, and wherein continued movement of the actuator from the intermediate position toward an unlocked position pivots the latch about the second guide feature and releases the anchor from the law portion of the latch, wherein the actuator includes a channel extending longitudinally through a proximal end portion of the actuator, and wherein the frame is at least partially received within the channel.

17. A latch system for releasably engaging an anchor in a vehicle, the latch system comprising:

a frame having an end portion for coupling to a web;

a latch movably coupled to the frame;

first means for pivoting the latch relative to the frame and about a first pivot point positioned within a cross section of the anchor; and

second means for pivoting the latch relative to the frame and about a second pivot point, different from the first pivot point, to release the latch from the anchor.

18. The latch system of claim 17 wherein the first means includes a guide feature projecting from the latch that cooperates with an abutment surface of an actuator.

19. The latch system of claim 17 wherein the second means includes a guide feature projecting from the latch that cooperates with a pivot surface of the frame.

20. The latch assembly of claim 17 :

wherein the first means includes a first guide feature projecting from the latch and movably received in a first opening in the frame;

wherein the second means includes a second guide feature projecting from the latch and movably received in a second opening in the frame; and

wherein the first pivot point is positioned at least proximate to the anchor and the second pivot point is position at least proximate to the second guide feature.

Assignments (11)
RELEASE OF PATENT SECURITY AGREEMENT RECORDED FEBRUARY 19, 2019 AT REEL/FRAME 048365/0499 Recorded Jun 6, 2024
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
To: TRANSDIGM INC.; TRANSDIGM GROUP INCORPORATED; AEROSONIC LLC; MOUNTAINTOP TECHNOLOGIES, INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; SHIELD RESTRAINT SYSTEMS, INC.; AMSAFE, INC.; ARKWIN INDUSTRIES, INC.; AVIONIC INSTRUMENTS, INC.; AEROSONIC CORPORATION; AVTECHTYEE, INC.; BREEZE-EASTERN LLC; BRUCE AEROSPACE INC.; CEF INDUSTRIES, LLC; CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; PURE TECHNOLOGIES LTD.; HARCO LABORATORIES, INC.; HARCO LLC; HARCO TECHNOLOGIES CORPORATION; CORRPRO COMPANIES, INC.; HARCO CORPORATION; HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PNEUDRAULICS, INC.; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; TACTAIR FLUID CONTROLS, INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR INTERNATIONAL GMBH; TELAIR INTERNATIONAL AB; NORDISK AVIATION PRODUCTS AS; TURNTIME TECHNOLOGIES AB; AEROCONTROLEX GROUP, INC.; TRANSICOIL INC.; SOUTHCO, INC.; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC COUNTERMEASURES CO.; ADVANCED INPUT DEVICES, INC.; ARMTEC DEFENSE PRODUCTS COMPANY; JOSLYN SUNBANK COMPANY LLC; LEACH INTERNATIONAL CORPORATION; SOURIAU USA, INC.; NMC GROUP, INC.; TA AEROSPACE CO.; MASON ELECTRIC CO.; KORRY ELECTRONICS CO.; PALOMAR PRODUCTS, INC.; ROLLS-ROYCE PLC; MEMTRON TECHNOLOGIES CO.; CHELTON, INC. (N/K/A CHELTON AVIONICS, INC.); SIMPLEX MANUFACTURING CO.; APICAL INDUSTRIES, INC.; AERO-INSTRUMENTS CO., LLC; AIRBORNE SYSTEMS NA, INC.; HARCOSEMCO LLC; HARCO, LLC (N/K/A HARCOSEMCO LLC); PEXCO AEROSPACE, INC.; TELAIR US LLC; CALSPAN AERO SYSTEMS ENGINEERING, INC.; CALSPAN SYSTEMS, LLC; ADAMS RITE AEROSPACE, INC.; ACME AEROSPACE, INC.; SCHNELLER, INC.; CEF INDUSTRIES, INC.
Reel/Frame 067640/0147 →
CORRECTIVE ASSIGNMENT TO CORRECT THE NATURE OF CONVEYANCE PREVIOUSLY RECORDED AT REEL: 064961 FRAME: 0671. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT OF PATENT AND TRADEMARK SECURITY INTEREST. Recorded Oct 5, 2023
From: CREDIT SUISSE AG, CAYMAN ISLANDS BRANCH, AS PREDECESSOR COLLATERAL AGENT
To: GOLDMAN SACHS BANK USA, AS SUCCESSOR COLLATERAL AGENT
Reel/Frame 065132/0644 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 20, 2023
From: CREDIT SUISSE AG, CAYMAN ISLANDS BRANCH, AS PREDECESSOR COLLATERAL AGENT
To: GOLDMAN SACHS BANK USA, AS SUCCESSOR COLLATERAL AGENT
Reel/Frame 064961/0671 →
RELEASE OF SECURITY INTEREST Recorded Apr 19, 2023
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
To: TA AEROSPACE CO.; TRANSDIGM, INC.; TRANSDIGM GROUP INCORPORATED; ACME AEROSPACE, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC CORPORATION; AIRBORNE HOLDINGS, INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; AMSAFE COMMERCIAL PRODUCTS INC.; AMSAFE, INC.; ARKWIN INDUSTRIES, INC.; AVIONIC INSTRUMENTS LLC; AVIONICS SPECIALTIES, INC.; AVTECH TYEE, INC.; BEAM'S INDUSTRIES; BREEZE EASTERN CORPORATION; BRUCE AEROSPACE, INC.; CEF INDUSTRIES, INC.; CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; ELECTROMECH TECHNOLOGIES LLC; HARCO LABORATORIES, INC.; HARCO LLC; HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PEXCO AEROSPACE, INC.; PNEUDRAULICS, INC.; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SHIELD RESTRAINT SYSTEMS, INC.; TACTAIR FLUID CONTROLS INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR INTERNATIONAL LLC; TRANSCOIL LLC; WESTERN SKY INDUSTRIES, LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC COUNTERMEASURES CO.; ARMTEC DEFENSE PRODUCTS COMPANY; LEACH INTERNATIONAL CORPORATION; NMC GROUP INC.; MASON ELECTRIC CO.; KORRY ELECTRONICS CO.; PALOMAR PRODUCTS, INC.; CHELTON, INC. (N/K/A CHELTON AVIONICS, INC.); SIMPLEX MANUFACTURING CO.; APICAL INDUSTRIES, INC.
Reel/Frame 063363/0753 →
SECURITY INTEREST Recorded Feb 27, 2023
From: TRANSDIGM INC.; TRANSDIGM GROUP INCORPORATED; 17111 WATERVIEW PKWY LLC; ACME AEROSPACE, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC LLC; AIRBORNE ACQUISITION, INC.; AIRBORNE GLOBAL, INC.; AIRBORNE HOLDINGS, INC.; AIRBORNE SYSTEMS NA INC.; AIRBORNE SYSTEMS NORTH AMERICA INC.; AIRBORNE SYSTEMS NORTH AMERICA OF CA INC.; AMSAFE GLOBAL HOLDINGS, INC.; AMSAFE, INC.; ANGUS ELECTRONICS CO.; APICAL INDUSTRIES, INC.; ARKWIN INDUSTRIES, INC.; ARMTEC COUNTERMEASURES CO.; ARMTEC COUNTERMEASURES TNO CO.; ARMTEC DEFENSE PRODUCTS CO.; AUXITROL WESTON USA, INC.; AVIATION TECHNOLOGIES, INC.; AVIONIC INSTRUMENTS LLC; AVIONICS SPECIALTIES, INC.; AVTECHTYEE, INC.; BETA TRANSFORMER TECHNOLOGY LLC; BREEZE-EASTERN LLC; BRIDPORT HOLDINGS, INC.; BRIDPORT-AIR CARRIER, INC.; BRUCE AEROSPACE INC.; CDA INTERCORP LLC; CEF INDUSTRIES, LLC; CENTURY HELICOPTERS, INC.; CHAMPION AEROSPACE LLC; CHELTON AVIONICS HOLDINGS, INC.; CHELTON AVIONICS, INC.; CHELTON DEFENSE PRODUCTS, INC.; CMC ELECTRONICS AURORA LLC; DART AEROSPACE USA, INC.; DART BUYER, INC.; DART HELICOPTER SERVICES, INC.; DART INTERMEDIATE, INC.; DART TOPCO, INC.; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; ELECTROMECH TECHNOLOGIES LLC; ESTERLINE EUROPE COMPANY LLC; ESTERLINE INTERNATIONAL COMPANY; ESTERLINE TECHNOLOGIES CORPORATION; ESTERLINE TECHNOLOGIES SGIP LLC; HARCOSEMCO LLC; HARTWELL CORPORATION; HELI TECH, INC.; HYTEK FINISHES CO.; ILC HOLDINGS, INC.; JANCO CORPORATION; JOHNSON LIVERPOOL LLC; KIRKHILL INC.; KORRY ELECTRONICS CO.; LEACH HOLDING CORPORATION; LEACH INTERNATIONAL CORPORATION; LEACH MEXICO HOLDING LLC; LEACH TECHNOLOGY GROUP, INC.; MARATHONNORCO AEROSPACE, INC.; MASON ELECTRIC CO.; MCKECHNIE AEROSPACE DE, INC.; MCKECHNIE AEROSPACE HOLDINGS, INC.; MCKECHNIE AEROSPACE US LLC; NAT SEATTLE INC.; NMC GROUP, INC.; NORDISK AVIATION PRODUCTS LLC; NORTH HILLS SIGNAL PROCESSING CORP.; NORTH HILLS SIGNAL PROCESSING OVERSEAS LLC; NORWICH AERO PRODUCTS, INC.; OFFSHORE HELICOPTER SUPPORT SERVICES, INC.; PALOMAR PRODUCTS, INC.; PARAVION TECHNOLOGY, INC.; PEXCO AEROSPACE, INC.; PNEUDRAULICS, INC.; POWER DEVICE CORPORATION; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SHIELD RESTRAINT SYSTEMS, INC.; SIMPLEX MANUFACTURING CO.; SKANDIA, INC.; SKURKA AEROSPACE INC.; SYMETRICS INDUSTRIES, LLC; TA AEROSPACE CO.; TACTAIR FLUID CONTROLS, INC.; TDG ESL HOLDINGS INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR US LLC; TEXAS ROTRONICS, INC.; TRANSICOIL LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; BRIDPORT ERIE AVIATION, INC.; TRANSDIGM UK HOLDINGS PLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
Reel/Frame 063012/0788 →
PATENT SECURITY AGREEMENT Recorded Apr 9, 2020
From: AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; ACME AEROSPACE, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC CORPORATION/LLC; AIRBORNE HOLDINGS, INC.; AMSAFE COMMERCIAL PRODUCTS INC.; AMSAFE, INC.; ARKWIN INDUSTRIES, INC.; AVIONIC INSTRUMENTS LLC; AVIONICS SPECIALTIES, INC.; AVTECHTYEE, INC.; BEAM’S INDUSTRIES; BREEZE-EASTERN CORPORATION; BRUCE AEROSPACE, INC.; CEF INDUSTRIES, INC.; CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; ELECTROMECH TECHNOLOGIES LLC; HARCO LABORATORIES, INCORPORATED; HARCO LLC; HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PEXCO AEROSPACE, INC.; PNEUDRAULICS, INC.; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SHIELD RESTRAINT SYSTEMS, INC.; TACTAIR FLUID CONTROLS, INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR INTERNATIONAL LLC; TRANSDIGM, INC.; TRANSCOIL LLC; WESTERN SKY INDUSTRIES, LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC COUNTERMEASURES CO.; ARMTEC DEFENSE PRODUCTS COMPANY; ARMTEC DEFENSE PRODUCTS CO.; LEACH INTERNATIONAL CORPORATION; NMC GROUP, INC.; TA AEROSPACE CO.; MASON ELECTRIC COMPANY; KORRY ELECTRONICS CO.; PALOMAR PRODUCTS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE AND NOTES COLLATERAL AGENT
Reel/Frame 052352/0704 →
SECURITY INTEREST Recorded Feb 19, 2019
From: TRANSDIGM, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC LLC (F/K/A AEROSONIC CORPORATION); AIRBORNE HOLDINGS, INC.; AIRBORNE SYSTEMS OF NORTH AMERICA OF NJ INC.; AMSAFE, INC.; ARKWIN INDUSTRIES, INC.; AVIONIC INSTRUMENTS LLC; AVIONICS SPECIALTIES, INC.; AVTECHTYEE, INC.; BREEZE-EASTERN LLC (F/K/A BREEZE-EASTERN CORPORATION); BRUCE AEROSPACE, INC.; CEF INDUSTRIES, LLC (F/K/A CEF INDUSTRIES, INC.); CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; ELECTROMECH TECHNOLOGIES LLC (F/K/A WESTERN SKY, INDUSTRIES, LLC); HARCOSEMCO LLC (F/K/A HARCO LABORATORIES, INCORPORATED) (F/K/A HARCO LLC); HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PEXCO AEROSPACE, INC.; PNEUDRAULICS, INC.; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SHIELD RESTRAINT SYSTEMS, INC. (F/K/A AMSAFE COMMERCIAL PRODUCTS INC.) (F/K/A BEAM'S INDUSTRIES, INC.); TACTAIR FLUID CONTROLS, INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR INTERNATIONAL LLC; TRANSICOIL LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ACME AEROSPACE, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.,
Reel/Frame 048365/0499 →
CHANGE OF NAME Recorded Oct 10, 2014
From: AMSAFE COMMERCIAL PRODUCTS, INC.
To: SHIELD RESTRAINT SYSTEMS, INC.
Reel/Frame 033961/0758 →
SECURITY AGREEMENT Recorded Mar 9, 2012
From: AMSAFE, INC.; AMSAFE COMMERCIAL PRODUCTS, INC.; AMSAFE AVIATION, INC.
To: CREDIT SUISSE AG
Reel/Frame 027830/0183 →
TERMINATION AND SECURITY RELEASE Recorded Mar 8, 2012
From: ARES CAPITAL CORPORATION
To: AMSAFE, INC.; AMSAFE COMMERCIAL PRODUCTS, INC.; AMSAFE AVIATION, INC.
Reel/Frame 027830/0048 →
SECURITY AGREEMENT Recorded Jul 22, 2011
From: AMSAFE, INC.; AMSAFE COMMERCIAL PRODUCTS. INC.; AMSAFE AVIATION, INC.
To: ARES CAPITAL CORPORATION, AS ADMINISTRATIVE AGENT
Reel/Frame 026637/0591 →