IP Library Granted Patent US 7,665,761
Granted Patent B1
US 7,665,761 · App. 12/057,295 · Granted Feb 23, 2010

Inflatable personal restraint systems and associated methods of use and manufacture

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Quick Facts
Patent No.
US 7,665,761
App. No.
12/057,295
Granted
Feb 23, 2010
Kind
B1
Abstract

Inflatable restraint systems for restraining an occupant in a vehicle are disclosed herein. A personal restraint system configured in accordance with one embodiment of the disclosure includes an airbag carried by a web. The web has an end portion operably coupled to the vehicle and is configured to extend around a portion of the occupant. The airbag includes a first inflatable chamber in fluid communication with a second inflatable chamber. The first inflatable chamber extends adjacent to a portion of the web when inflated, and the second inflatable chamber extends outwardly from the first inflatable chamber adjacent to a portion of the occupant when inflated.

Claims (52)

1. A personal restraint system for use with an occupant seated in a vehicle, the personal restraint system comprising:

a web configured to extend around a portion of the occupant when the occupant is seated in the vehicle; and

an airbag that includes:

a first inflatable chamber attached to the web, the first inflatable chamber having a generally tubular shape extending adjacent to a portion of the web when inflated; and

a second inflatable chamber in fluid communication with the first inflatable chamber, the second inflatable chamber extending outwardly from the first inflatable chamber adjacent to a portion of the occupant when inflated, wherein the second inflatable chamber has an inverted “L” shape when inflated.

2. The personal restraint system of claim 1 wherein the first inflatable chamber has a first exterior surface portion attached to the web and a second exterior surface portion facing away from the web when the first inflatable chamber is inflated, and wherein the second inflatable chamber has a third exterior surface portion attached to the second exterior surface portion of the first inflatable chamber.

3. The personal restraint system of claim 2 wherein the first inflatable chamber is oriented along a centerline when inflated, and wherein third exterior surface portion of the second inflatable chamber is attached to the second exterior surface portion of the first inflatable chamber at a location that is offset from the centerline of the first inflatable chamber.

4. The personal restraint system of claim 1 , further comprising:

a gas source;

a conduit operably coupling the gas source to the first inflatable chamber; and

a sensor operably coupled to the gas source, wherein the sensor is configured to

transmit a signal to the gas source in response to a rapid deceleration of the vehicle above a preset magnitude, and wherein the gas source is configured to dispense gas into the first inflatable chamber in response to the signal.

5. The personal restraint system of claim 1 wherein the first inflatable chamber tensions the web when inflated.

6. The personal restraint system of claim 1 wherein the second inflatable chamber inflates in front of the occupant when inflated.

7. The personal restraint system of claim 1 wherein the first inflatable chamber is at least partially inflated before the second inflatable chamber is inflated.

8. The personal restraint system of claim 7 , further comprising a gas source operably coupled to the first inflatable chamber, wherein the gas source dispenses gas into the first inflatable chamber to inflate the first inflatable chamber, and wherein the gas flows through an opening in the first inflatable chamber into the second inflatable chamber to inflate the second inflatable chamber.

9. The personal restraint system of claim 7 wherein the gas flows from the second inflatable chamber into the first inflatable chamber when the second inflatable chamber is deflated.

10. The personal restraint system of claim 1 :

wherein the web is a shoulder web; and

wherein the second inflatable chamber forms an impact barrier chamber extending from the first inflatable chamber in a generally lateral direction in front of an upper portion of the occupant when inflated.

11. The personal restraint system of claim 1 wherein the web is a first web and the airbag is a first airbag, and wherein the personal restraint system further comprises:

a second web configured to extend around a portion of the occupant when the occupant is seated in the vehicle;

a second airbag carried by the second web, wherein the second airbag includes:

a third inflatable chamber attached to the second web, the third inflatable chamber having a generally tubular shape extending adjacent to a portion of the second web when inflated; and

a fourth inflatable chamber in fluid communication with the third inflatable chamber, the fourth inflatable chamber extending outwardly from the third inflatable chamber adjacent to a portion of the occupant when inflated.

12. A personal restraint system for use in a vehicle, the personal restraint system comprising:

a web operably coupled to the vehicle;

an airbag having a tensioning chamber in fluid communication with an impact barrier chamber, wherein the tensioning chamber is attached to the web and the impact barrier chamber is attached to the tensioning chamber, and wherein the tensioning chamber has a generally tubular shape that tensions the web when inflated, and wherein the impact barrier chamber has a generally inverted “L” shape when inflated that forms a deformable impact cushion for an occupant of the vehicle;

an inflator operably coupled to the tensioning chamber; and

a sensor operably coupled to the inflator, wherein the sensor is configured to activate the inflator in response to a rapid deceleration of the vehicle, whereby the inflator inflates the tensioning chamber and the impact barrier chamber.

13. The personal restraint system of claim 12 wherein the tensioning chamber has a first exterior surface portion attached to the web and a second exterior surface portion attached to a third exterior surface portion of the impact barrier.

14. The personal restraint system of claim 12 wherein the web is a shoulder web and the tensioning chamber has a generally tubular shape extending adjacent to the shoulder web when inflated, and wherein the impact barrier chamber extends outwardly from the tensioning chamber in a lateral direction when inflated.

15. The personal restraint system of claim 12 , further comprising a gas transfer passage between the tensioning chamber and the impact barrier chamber, wherein the tensioning chamber receives gas from the inflator, and the impact barrier chamber receives gas from the tensioning chamber.

16. The personal restraint system of claim 15 wherein the impact barrier chamber vents into the tensioning chamber through an opening in the tensioning chamber when the impact barrier deflates.

17. The personal restraint system of claim 12 wherein the web is a first web, the airbag is a first airbag, and the tensioning chamber is a first tensioning chamber, and wherein the restraint system further includes a second web operably coupled to the vehicle and a second airbag having a second tensioning chamber attached to the second web.

18. The personal restraint system of claim 17 wherein the impact barrier chamber is a first impact barrier chamber, the first web is a shoulder web and the second web is a lap web, and wherein the personal restraint system further comprises a second impact barrier chamber attached to the second tensioning chamber, wherein the first impact barrier chamber extends toward a first portion of the occupant and the second impact barrier chamber extends toward a second portion of the occupant.

19. A personal restraint system for use with an occupant in a vehicle, the personal restraint system comprising:

strap means for restraining the occupant in the vehicle, wherein the strap means extend at least partially around a portion of the occupant;

an airbag carried by the strap means, wherein the airbag includes a first chamber in fluid communication with a second chamber, the first chamber having a first surface portion attached to the strap means and a second surface portion attached to the second chamber, wherein the second chamber has a third surface portion that extends laterally from the first chamber when the first and second chambers are inflated, and wherein the second chamber has an inverted “L” shape when inflated; and

means for automatically inflating the first and second chambers of the airbag in response to a rapid deceleration of the vehicle.

20. The personal restraint system of claim 19 wherein the first chamber has a generally tubular shape that tensions the strap means when inflated, and wherein the second chamber extends laterally outward in front of the occupant when inflated.

21. The personal restraint system of claim 19 wherein the first chamber is inflated with gas flowing directly from the inflating means, and wherein the second chamber is inflated with the gas flowing indirectly from the inflating means through the first chamber into the second chamber.

22. The personal restraint system of claim 19 wherein the first and second chambers are inflated with gas from the inflating means, and wherein the second chamber vents into the first chamber when the second chamber deflates.

23. A method of restraining an occupant in a vehicle, the method comprising:

detecting a rapid deceleration of the vehicle;

inflating a first chamber of an airbag in response to detecting the deceleration, wherein the first chamber has a generally tubular shape extending adjacent to a web when inflated; and

inflating a second chamber of the airbag from the first chamber after the first chamber is at least partially inflated, wherein the second chamber extends outwardly from the first chamber adjacent to a portion of the occupant, and wherein the second chamber has a generally inverted “L” shape when inflated.

24. The method of claim 23 wherein inflating the first chamber of the airbag further includes tensioning the web with the first chamber when the first chamber is inflated.

25. The method of claim 23 , further comprising venting the second chamber into the first chamber in response to an impact from the occupant against the second chamber.

26. The method of claim 23 wherein the airbag is a first airbag and the web is a first web, and wherein the method further comprises:

inflating a third chamber of a second airbag in response to detecting the deceleration, wherein the third chamber has a generally tubular shape extending adjacent to a second web when inflated; and

inflating a fourth chamber of the second airbag from the third chamber after the third chamber is at least partially inflated, wherein the fourth chamber extends outwardly from the third chamber adjacent to a portion of the occupant.

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 →
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 5, 2008
From: GREEN, THOMAS J.; KEESLAR, KEVIN
To: AMSAFE, INC.
Reel/Frame 021054/0487 →