IP Library Granted Patent US 8,100,029
Granted Patent B2
US 8,100,029 · App. 12/029,435 · Granted Jan 24, 2012

Control inceptor systems and associated methods

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Quick Facts
Patent No.
US 8,100,029
App. No.
12/029,435
Granted
Jan 24, 2012
Kind
B2
Abstract

Control inceptor systems and associated methods, including inceptors suitable for high-g operations and/or inceptors having a center of rotation located within an operator's grasp region, are disclosed herein. One aspect of the invention is directed toward a control inceptor having a grip coupled to a support. The inceptor is configured so that a center of rotation for movement in at least one plane is located within the grasp region of an operator when an operator grasps the grip. The support is positioned so that when the operator moves the grip (e.g., makes an input movement), the support arcs about the center of rotation.

Claims (54)

1. A control inceptor system for use by an operator having a hand with a grip region, comprising:

a grip configured to be grasped by the operator's hand wherein the grip is located within the grip region of the hand;

a first movement mechanism coupled to and exterior of the grip, the first movement mechanism having a collapsible first linkage arrangement, and at least a portion of the first movement mechanism being rotatable with the grip in a first plane about a first center of rotation that is positioned within the grip region when the operator is grasping the grip; and

a second movement mechanism coupled to and exterior of the grip, the second movement mechanism having a collapsible second linkage arrangement, and at least a portion of the second movement mechanism being rotatable with the grip in a second plane about a second center of rotation that is positioned within the grip region when the operator is grasping the grip,

wherein the second plane is angularly offset from the first plane;

wherein the grip is connected to the first movement mechanism, and wherein the first movement mechanism is connected to the second movement mechanism intermediate the grip and the second movement mechanism.

2. The control inceptor system of claim 1 wherein the first plane is orthogonal to the second plane.

3. The control inceptor system of claim 1 wherein first center of rotation is substantially collocated with the second center of rotation.

4. The control inceptor system of claim 1 wherein the first movement mechanism and the grip are rotatable as a unit about an axis substantially parallel to a line extending between a back of the operator's hand and a palm of the hand as the operator grasps the grip.

5. The control inceptor system of claim 1 wherein the grip and the first movement mechanism are rotatable in the first plane about the first center of rotation in response to an input movement from the operator's hand.

6. The control inceptor system of claim 1 wherein the grip and the first movement mechanism are rotatable in the first plane about the first center of rotation simultaneous with rotation of the grip and the second movement mechanism in the second plane about the second center of rotation.

7. The control inceptor system of claim 1 wherein the first movement mechanism and the grip are moveable as a unit in the second plane about the second center of rotation when the second movement is rotated in the second plane.

8. The control inceptor system of claim 1 wherein the first movement mechanism has a first support member connected to the grip, the first linkage arrangement connected to the first support member with the first support member intermediate the grip and the first linkage arrangement, and a second support member connected to the first linkage arrangement with the first linkage arrangement intermediate the first and second support members, and wherein a portion of the first linkage arrangement is movable relative to the second support member so the first support member and the grip move in an arc in the first plane about the first center of rotation.

9. The control inceptor system of claim 8 wherein the first linkage arrangement includes first and second collapsible assemblies coupled to the first support member and being moveable between collapsed and expanded positions, wherein the first collapsible assembly moves toward the collapsed position and the second collapsible assembly moves toward the expanded position when the first support plate and the grip rotate in the first plane in a first direction, and the first collapsible assembly moves toward the expanded position and the second collapsible assembly moves toward the collapsed position when the first support member and the grip rotate in the first plane in a second direction opposite the first direction.

10. The control inceptor system of claim 8 wherein the second movement mechanism has a third support member connectable to a mounting structure, the second linkage arrangement connected to the third support member and the second support member, wherein the second linkage arrangement is intermediate the second and third support members, and wherein the second linkage arrangement being movable relative to the third support member so the second first support member and the grip move in an arc in the second plane about the second center of rotation.

11. The control inceptor system of claim 8 wherein the second linkage arrangement includes third and fourth collapsible assemblies coupled to the first support member and being moveable between collapsed and expanded positions, wherein the third collapsible assembly moves toward the collapsed position and the fourth collapsible assembly moves toward the expanded position when the second support plate and the grip rotate in the second plane in a first direction, and the third collapsible assembly moves toward the expanded position and the fourth collapsible assembly moves toward the collapsed position when the second support plate and the grip rotate in the second plane in a second direction opposite the first direction.

12. The control inceptor system of claim 1 further comprising a first movement sensor coupled to the first movement mechanism and configured to detect rotational movement of the first movement mechanism in the first plane, and a second movement sensor coupled to the second movement mechanism and configured to detect rotational movement of the second movement mechanism in the second plane.

13. The control inceptor system of claim 1 further comprising a vehicle control system, and the wherein the grip, the first movement mechanism, and the second movement mechanism are coupled to the vehicle control system.

14. A control inceptor system for use by an operator having a hand with a grip region, comprising:

a grip configured to be grasped by the operator's hand so the grip is within the grip region, wherein the grip is moveable in a three-dimensional X-Y-Z frame of reference defined by an XY plane, a YZ plane and a ZX plane all orthogonal to each other;

a first movement mechanism coupled to the grip, at least a portion of the first movement mechanism being rotatable with the grip in the XY plane about a first center of rotation that is positioned within the grip region when the operator is applying a first input force to the grip substantially parallel to the XY plane, the first movement mechanism having a first linkage arrangement movable between collapsed and expanded positions upon movement of the grip; and

a second movement mechanism coupled to the grip, as least a portion of the second movement being rotatable with the grip in the YZ plane about a second center of rotation that is positioned within the grip region when the operator is applying a second input force to the grip substantially parallel to the YZ plane, the second movement mechanism having a second linkage arrangement movable between collapsed and expanded positions upon movement of the grip;

wherein grip is connected to the first movement mechanism, and the first movement mechanism is connected to the second movement mechanism intermediate the grip and the second movement mechanism.

15. The control inceptor system of claim 14 wherein first center of rotation is substantially collocated with the second center of rotation.

16. The control inceptor system of claim 14 wherein the portion of the first movement mechanism and the grip are rotatable as a unit in the YZ plane without rotating in the XY plane.

17. The control inceptor system of claim 14 wherein the grip and the portion of the first movement mechanism are rotatable in the XY plane about the first center of rotation simultaneous with rotation of the grip and the portion of the second movement mechanism in the YZ plane about the second center of rotation.

18. The control inceptor system of claim 14 wherein the first movement mechanism has a first support member connected to the grip, the first linkage arrangement connected to the first support member with the first support member intermediate the grip and the first linkage arrangement, and a second support member connected to the first linkage arrangement with the first linkage arrangement intermediate the first and second support members, and wherein the first support member and at least a portion of the first linkage arrangement being movable relative to the second support member so the first support member and the grip move in an arc in the XY plane about the first center of rotation.

19. The control inceptor system of claim 18 wherein the first linkage arrangement includes first and second collapsible assemblies coupled to the first support member and being moveable between collapsed and expanded positions, wherein the first collapsible assembly moves toward the collapsed position and the second collapsible assembly moves toward the expanded position when the first support plate and the grip rotate in the XY plane in a first direction, and the first collapsible assembly moves toward the expanded position and the second collapsible assembly toward the collapsed position when the first support member and the grip rotate in the XY plane in a second direction opposite the first direction.

20. The control inceptor system of claim 18 wherein the second movement mechanism has a third support member connectable to a mounting structure, the second linkage arrangement connected to the third support member and the second support member, wherein the second linkage arrangement is intermediate the second and third support members, and wherein the second linkage arrangement being movable relative to the third support member so the second first support member and the grip move in an arc in the YZ plane about the second center of rotation.

21. The control inceptor system of claim 18 wherein the second linkage arrangement includes third and fourth collapsible assemblies coupled to the first support member and being moveable between collapsed and expanded positions, wherein the third collapsible assemblies moves toward the collapsed position and the fourth collapsible structure moves toward the expanded position when the second support plate and the grip rotate in the YZ plane in a first direction, and the third collapsible assembly moves toward the expanded position and the fourth collapsible assembly moves toward the collapsed position when the second support plate and the grip rotate in the YZ plane in a second direction opposite the first direction.

22. The control inceptor system of claim 14 further comprising a movement sensor coupled to at least one of the first and second first movement mechanisms and configured to detect rotational movement of the one of the first and second movement mechanism in the respective XY and YZ planes.

23. The control inceptor system of claim 14 further comprising a vehicle control system, and wherein the grip, the first movement mechanism and the second movement mechanism are coupled to the vehicle control system.

24. A control system for a vehicle operated by an operator having a hand with a grip region when the operator grasps a portion of the control system, comprising:

a control devices moveable to provide control of at least a portion of the vehicle;

a control area configured to receive the operator therein;

a control inceptor system mounted in the control area and coupled to the control devices, the control inceptor system having:

a grip configured to be grasped by the operator's hand and located within the grip region;

a first movement mechanism coupled to and exterior of the grip, the first movement mechanism having a collapsible first linkage arrangement and at least a portion of the first movement mechanism being rotatable with the grip in a first plane about a first center of rotation that is positioned within the grip region when the operator is grasping the grip; and

a second movement mechanism coupled to and exterior of the grip, the second movement mechanism having a collapsible second linkage arrangement and at least a portion of the second movement mechanism being rotatable with the grip in a second plane about a second center of rotation that is positioned within the grip region when the operator is grasping the grip, wherein the second plane is angularly offset from the first plane;

wherein the grip is connected to the first movement mechanism, and wherein the first movement mechanism is connected to the second movement mechanism intermediate the grip and the second movement mechanism.

25. The control system of claim 24 wherein the vehicle is one of an aircraft, space craft, and watercraft, and the control devices include at least one control surface for controlling movement of the vehicle.

26. The control system of claim 24 wherein first center of rotation is substantially collocated with the second center of rotation.

27. The control system of claim 24 wherein the first movement mechanism and the grip are rotatable as a unit about an axis substantially parallel to a line extending between a back of the operator's hand and a palm of the hand as the operator grasps the grip.

28. The control system of claim 24 wherein the first and second centers of rotation are located at a position within the grip or substantially adjacent to a surface of the grip.

29. The control system of claim 24 wherein the grip and the first movement mechanism are rotatable in the first plane about the first center of rotation simultaneously with rotation of the grip and the second movement mechanism in the second plane about the second center of rotation.

30. The control system of claim 24 wherein the first movement mechanism and the grip are moveable as a unit about the second center of rotation when the second movement is rotated in the second plane without the grip and the first movement mechanism rotating in the first plane.

31. A method of operating a vehicle by an operator for movement of at least a portion of the vehicle, comprising:

grasping with the operator's hand a grip of a control inceptor system, the control inceptor system comprising the grip configured to be grasped by the operator's hand so the grip is within the grip region of the hand, a first movement mechanism coupled to and exterior of the grip, the first movement mechanism having a collapsible first linkage arrangement and at least a portion of the first movement mechanism being rotatable with the grip in a first plane about a first center of rotation that is positioned within the grip region when the operator is grasping the grip, and a second movement mechanism coupled to and exterior of the grip, the second movement mechanism having a collapsible second linkage arrangement and at least a portion of the second movement mechanism being rotatable with the grip in a second plane about a second center of rotation that is positioned within the grip region when the operator is grasping the grip, wherein the second plane is angularly offset from the first plane, wherein the grip is connected to the first movement mechanism, and wherein the first movement mechanism is connected to the second movement mechanism intermediate the grip and the second movement mechanism;

applying a first input force to the grip and rotating the grip and at least a portion of the first movement mechanism to rotate in the first plane about the first center of rotation;

moving a first portion of the vehicle in response to the first input force and rotation of the grip in the first plane about the first center of rotation;

applying a second input force to the grip and rotating the grip and at least a portion of the second movement mechanism to rotate in the second plane about the second center of rotation; and

moving a second portion of the vehicle in response to the second input force and rotation of the grip in the second plane about the second center of rotation.

32. The method of claim 31 wherein the first and second input forces are applied at lease one of simultaneously and sequentially, and the grip and the portion of the first movement mechanism rotate about the first center of rotation simultaneously or sequentially with rotation of the grip and the portion of the second movement mechanism about the second center of rotation.

33. The method of claim 31 wherein the grip and the first movement mechanism move as a unit in the second plane when the grip and the portion of the second movement mechanism rotate in the second plane about the second center of rotation.

Assignments (11)
RELEASE OF PATENT SECURITY AGREEMENT RECORDED APRIL 3, 2019 AT REEL/FRAME 048788/0581 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 067640/0237 →
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 Apr 3, 2019
From: SOURIAU USA, INC.; LEACH INTERNATIONAL CORPORATION; TA AEROSPACE CO.; ADVANCED INPUT DEVICES, INC.; MASON ELECTRIC CO.; NMC GROUP, INC.; PALOMAR PRODUCTS, INC.; KORRY ELECTRONICS CO.; MEMTRON TECHNOLOGIES CO.; JOSLYN SUNBANK COMPANY, LLC; ARMTEC DEFENSE PRODUCTS CO.; ARMTEC COUNTERMEASURES CO.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 048788/0581 →
SECURITY INTEREST Recorded Apr 3, 2019
From: SOURIAU USA, INC.; LEACH INTERNATIONAL CORPORATION; TA AEROSPACE CO.; ADVANCED INPUT DEVICES, INC.; MASON ELECTRIC CO.; NMC GROUP, INC.; PALOMAR PRODUCTS, INC.; KORRY ELECTRONICS CO.; MEMTRON TECHNOLOGIES CO.; JOSLYN SUNBANK COMPANY, LLC; ARMTEC DEFENSE PRODUCTS CO.; ARMTEC COUNTERMEASURES CO.
To: CREDIT SUISSE AG
Reel/Frame 048788/0719 →
RELEASE OF SECURITY INTEREST Recorded Mar 15, 2019
From: WELLS FARGO BANK, NATIONAL ASSOCIATION AS ADMINISTRATIVE AGENT
To: MASON ELECTRIC CO.
Reel/Frame 048605/0194 →
SECURITY AGREEMENT Recorded Apr 11, 2011
From: MASON ELECTRIC CO.
To: WELLS FARGO BANK, NATIONAL ASSOCIATION, AS ADMINISTRATIVE AGENT
Reel/Frame 026103/0913 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 4, 2011
From: PETERSON, TERRY; ALLEN, KEVIN
To: MASON ELECTRIC CO.
Reel/Frame 025901/0042 →