IP Library Granted Patent US 8,646,158
Granted Patent B2
US 8,646,158 · App. 12/775,268 · Granted Feb 11, 2014

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 8,646,158
App. No.
12/775,268
Granted
Feb 11, 2014
Kind
B2
Abstract

Latch assemblies for releasably engaging anchor members and other attachment points in vehicles are disclosed herein. A latch assembly configured in accordance with one embodiment of the disclosure includes a latch and an ejector movably coupled to a frame. In some embodiments, a biasing member urges the ejector toward a position that holds the latch in a first or open position prior to attachment to an anchor member. When the anchor member presses against the ejector, the biasing member causes the ejector to rotate latch from the first or open position to a second position about a first pivot point, and then from the second position to a third or fully closed position about a second pivot point.

Claims (42)

1. A latch assembly for engaging an anchor member, the latch assembly comprising:

a frame having a first jaw portion and first and second openings proximate the first jaw portion;

a pivotable latch having a second jaw portion, wherein the latch is operably coupled to the frame by a first guide feature movably received in the first opening and a second guide feature movably received in the second opening;

an ejector operably coupled between the frame and the latch; and

a biasing member urging the ejector against the first guide feature to selectively move the latch from an open position to a closed position by pivoting the latch about a first pivot point and then a second pivot point spaced apart from the first pivot point.

2. The latch assembly of claim 1 wherein the frame includes a proximal end portion having a web aperture and a distal end portion proximate the first jaw portion, and wherein moving the ejector toward the proximal end portion causes the ejector to drive the latch to the closed position by pivoting the latch about the first pivot point and then the second pivot point.

3. The latch assembly of claim 1 wherein the frame includes a proximal end portion having a web aperture and a distal end portion proximate the first jaw portion, wherein the ejector includes a base portion having a bearing surface and an upper portion having a recess configured to receive the first guide feature, and wherein pressing the bearing surface toward the proximal end portion of the frame causes the recess to move the first guide feature toward the distal end portion of the frame and pivot the latch about the first pivot point and then the second pivot point.

4. The latch assembly of claim 1 wherein the first opening is a slot having a generally “V” shape.

5. The latch assembly of claim 1 wherein the first opening is a slot having a generally “V” shape with first and second upper end portions and a bottom mid portion, wherein the first guide feature is positioned against the first upper end portion of the “V” when the latch is in the open position, wherein pushing the ejector back against the biasing member causes the ejector to drive the first guide feature toward the bottom mid portion of the “V” and then toward the second upper end portion of the “V” to close the latch.

6. The latch assembly of claim 1 wherein the ejector includes a notch configured to receive the first guide feature, wherein pushing the ejector back against the biasing member causes the first guide feature to move into the notch.

7. The latch assembly of claim 1 wherein the ejector includes a blocking surface adjacent to a notch configured to receive the first guide feature, wherein the blocking surface holds the first guide feature in the open latch position, and wherein pushing the ejector back against the biasing member causes the first guide feature to move off of the blocking surface and into the notch.

8. A latch assembly for releasably securing a child seat to an anchor in a vehicle, the latch assembly comprising:

a frame having a proximal end portion and a distal end portion, the frame further having a first opening, a second opening, and a first jaw proximate the distal end portion;

a latch movably coupled to the frame proximate the distal end portion by a first guide feature movably received in the first opening and a second guide feature movably received in the second opening, wherein the latch includes a second jaw spaced apart from the first jaw to define a latch mouth therebetween;

an anchor ejector operably coupled to the frame between the first and second jaws, wherein movement of the ejector toward the proximal end portion of the frame causes the second jaw to move toward the first jaw as the latch pivots about a first pivot point and then a second pivot point spaced apart from the first pivot point; and

a biasing member urging a first portion of the ejector against the first guide feature, wherein movement of a second portion of the ejector toward the proximal end portion of the frame causes the first portion of the ejector to drive the first guide feature toward the distal end of the frame.

9. A latch assembly for releasably securing a child seat to an anchor in a vehicle, the latch assembly comprising:

a frame having a proximal end portion and a distal end portion, the frame further having a first opening, a second opening, and a first jaw proximate the distal end portion;

a latch movably coupled to the frame proximate the distal end portion by a first guide feature movably received in the first opening and a second guide feature movably received in the second opening, wherein the latch includes a second jaw spaced apart from the first jaw to define a latch mouth therebetween; and

an anchor ejector operably coupled to the frame between the first and second jaws, wherein movement of the ejector toward the proximal end portion of the frame causes the second jaw to move toward the first jaw as the latch pivots about a first pivot point and then a second pivot point spaced apart from the first pivot point, wherein the ejector includes a blocking surface, and wherein the blocking surface bears against the first guide feature to hold the latch in an open position.

10. The latch assembly of claim 9 wherein the first and second jaws at least partially define a mouth, and wherein the anchor ejector is slidably coupled to the frame within the mouth.

11. The latch assembly of claim 9 wherein movement of the ejector toward the proximal end portion of the frame causes the latch to pivot from an open position toward a closed position.

12. The latch assembly of claim 9 wherein the first and second guide features are fixedly attached to the latch.

13. The latch assembly of claim 9 wherein the first opening in the frame is a slot having a generally “V” shape, and wherein the ejector rotates over-center as the first guide feature moves from a first end portion of the slot to a second end portion of the slot.

14. The latch assembly of claim 9 wherein movement of the ejector toward the proximal end portion of the frame causes the latch to pivot in a first direction from an open position toward a closed position, and wherein the latch assembly further comprises a release actuator operably coupled to the latch, wherein movement of the release actuator from a first actuator position toward a second actuator position rotates the latch in a second direction about the second pivot point, and wherein continued movement of the release actuator from the second actuator position toward a third actuator position rotates the latch in the second direction about the first pivot point to return the latch to the open position.

15. A latch system for releasably coupling a web to an anchor in a vehicle, the latch system comprising:

a frame having a proximal end portion for engaging the web and a distal end portion for engaging the anchor;

a latch movably coupled to the frame toward the distal end portion via a first guide feature and a second guide feature; and

an ejector operable to hold the latch in an open position via the first guide feature, wherein the latch is movable from the open position to a closed position via a first rotation about a first axis and a second rotation about a second axis spaced apart from the first axis.

16. The latch system of claim 15 wherein the frame includes an elongate slot, wherein the first guide feature extends through the elongate slot, and wherein the ejector is operable to hold the latch in the open position by holding the first guide feature against an end portion of the elongate slot.

17. The latch system of claim 15 , further comprising means for releasing the latch system from the anchor by:

pivoting the latch about the second axis; and

pivoting the latch about the first axis to move the latch to the open position.

18. The latch system of claim 17 wherein the means for releasing the latch system includes a flexible strap operably coupled to the latch.

19. The latch system of claim 15 wherein rotation of the latch includes the ejector contacting the anchor and driving the latch about the first axis and the second axis.

20. A latch assembly for releasably securing a child seat to an anchor in a vehicle, the latch assembly comprising:

a frame having a proximal end portion, a distal end portion, and a first jaw proximate the distal end portion;

a latch movably coupled to the frame via a guide feature and proximate the distal end portion, wherein the latch includes a second jaw configured to move toward the first jaw to engage the anchor in a closed position as the latch rotates in a first direction about a first pivot point and then a second pivot point spaced apart from the first pivot point;

an elector positionable to engage the guide feature to hold the latch in an open position; and

a release actuator operably coupled to the latch, wherein pulling the release actuator away from the distal end portion of the frame rotates the latch in a second direction about the second pivot point and then the first pivot point to move the second jaw away from the first jaw to release the anchor and return the latch to an open position.

21. The latch assembly of claim 20 wherein the release actuator includes a flexible strap.

22. The latch assembly of claim 20 wherein the guide feature is a first guide feature, wherein the frame includes a first elongate opening and a second elongate opening, and wherein the latch is movably coupled to the frame by the first guide feature movably received in the first elongate opening and a second guide feature movably received in the second elongate opening.

Assignments (12)
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 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 15, 2010
From: BUCKINGHAM, FRED; MAIN, MARK E.
To: AMSAFE COMMERCIAL PRODUCTS, INC.
Reel/Frame 024537/0593 →