IP Library › Granted Patent US 8,647,039
Granted Patent B2
US 8,647,039 · App. 13/536,413 · Granted Feb 11, 2014

System for loading and unloading loose cargo in a cargo hold, preferably of a plane, and intermediate conveyor means or conveyor unit herefor

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Quick Facts
Patent No.
US 8,647,039
App. No.
13/536,413
Granted
Feb 11, 2014
Kind
B2
Abstract

The present invention concerns a system for loading and unloading loose cargo, such as preferably pieces of luggage or the like, in a cargo hold of a plane, including conveying the loose cargo towards the inner end of the cargo hold during loading, or away from it during unloading, and including transport of the loose cargo between the level of the tarmac and the cargo hold opening. The loose cargo may during loading be conveyed into the fuselage in a direction transversal to the longitudinal axis of the plane and also in the longitudinal direction of the plane, and deposited, in the cargo hold. Loose cargo conveyed back into the plane of the cargo hold opening during unloading may be conveyed off transversely to the longitudinal axis of the plane through the cargo hold opening. Moreover the invention proposes intermediate conveyor means herefor.

Claims (52)

1. A system for loading and unloading loose cargo in a cargo hold of a plane, comprising:

transport means covering the area of the floor of the cargo hold for intermittently conveying the loose cargo towards the inner end of the cargo hold during loading, or away from it during unloading, wherein the front end of said transport means reaches into the range of the cargo hold opening inside the fuselage of the plane, and

a separate tarmac based external conveyor organ connecting to the outside of the plane at the cargo hold opening for transporting the loose cargo between the level of the tarmac and the cargo hold opening,

wherein between the plane-side end of said external conveyor organ and the front end of said transport means in the cargo hold at least one separate intermediate conveyor means is arranged, said intermediate conveyor means includes a first conveyor organ in the form of a conveyor belt, wherein, at one end thereof, said first conveyor organ is followed by a second conveyor organ in the form of a conveyor belt, for bridging the distance from one end of the external conveyor organ into the inside of the cargo hold, whereby the loose cargo is during loading initially conveyed deeper into the fuselage substantially transversely to the longitudinal axis of the plane by the first and second conveyor organs, and wherein an end of the second conveyor organ is followed by a third conveyor organ formed as a roller panel,

whereupon the loose cargo can be rotated manually in the cargo hold and transported further substantially in the longitudinal direction of the plane and deposited on the front end of said transport means in the cargo hold, and

whereby during unloading, loose cargo conveyed beyond the front end of said transport means out into the plane of the cargo hold opening may be transported off substantially transversely to the longitudinal axis of the plane through the cargo hold opening.

2. The system according to claim 1 , wherein said intermediate conveyor means includes a sliding element at its lower side in the overlap range with said external conveyor organ, for slidably supporting said intermediate conveyor means on the upper side of said external conveyor organ in the end range thereof.

3. The system according to claim 2 , wherein said sliding element comprises a wheel.

4. The system according to claim 1 , wherein in the overlap range with said external conveyor organ an outrigger is linked to said intermediate conveyor means, which is supported by its end facing away from said intermediate conveyor means, by means of an articulation linked there, against a sliding rail oriented in parallel with the longitudinal direction of said external conveyor organ and fastened to the latter, for slidably supporting said intermediate conveyor means in the conveying direction of said external conveyor organ.

5. The system according to claim 1 , wherein the end of said intermediate conveyor means facing the front end of said transport means in the cargo hold is adjustable in height relative to the beginning of said intermediate conveyor means facing said external conveyor organ.

6. The system according to claim 1 , wherein an end portion of said intermediate conveyor means is capable of being pivoted about an axis transversely to the conveying direction of said intermediate conveyor means, such that this end portion may be oriented horizontally.

7. The system according to claim 1 , wherein a leading portion of said intermediate conveyor means is oriented at a predetermined angle of inclination with the angle of inclination of said external conveyor organ.

8. The system according to claim 7 , wherein said predetermined angle of inclination of said intermediate conveyor means with the angle of inclination of said external conveyor organ is between approximately 10° and approximately 30°.

9. The system according to claim 1 , wherein said intermediate conveyor means including its conveying direction for conveying loose cargo substantially transversely to the longitudinal axis of the plane may be pivoted about an angular range of about −30° to +30° relative to the conveying direction of said external conveyor organ.

10. The system according to claim 1 , wherein parts of the supporting structure of said intermediate conveyor means are manufactured of lightweight material.

11. The system according to claim 10 , wherein said lightweight materials comprise aluminum.

12. The system according to claim 10 , wherein said lightweight materials comprise fiber composites.

13. The system according to claim 1 , wherein said intermediate conveyor means further comprises at least one frame supported against said external conveyor organ with said first conveyor organ in the form of said first conveyor belt, for receiving the loose cargo during loading in the range in front of the cargo hold opening of the plane, from the end of said external conveyor organ facing the plane, and conveying it on substantially transversely to the longitudinal axis of the plane,

wherein the second conveyor organ receives loose cargo during loading, in the range of the cargo hold opening of the plane from the end of said first conveyor organ and conveys it on substantially transversely to the longitudinal axis of the plane.

14. The system according to claim 13 , wherein during unloading, loose cargo may be applied manually on said third conveyor organ from the front end of said transport means present in the cargo hold substantially in the longitudinal direction of the plane, rotatably placed there, and supported suitably for handover to said second conveyor organ, wherein said second conveyor organ conveys the loose cargo substantially transversely to the longitudinal axis of the plane to the cargo hold opening and/or through the latter and hands it over to said first conveyor organ, which conveys the loose cargo on substantially transversely to the longitudinal axis of the plane to said external conveyor organ and hands it over to the latter for further transport.

15. The system according to claim 13 , wherein said frame of said first conveyor organ comprises a sliding element its lower side for a slidable support of said first conveyor organ substantially in the conveying direction of said external conveyor organ on the upper side of said external conveyor organ in the range of the end portion thereof facing the plane walls.

16. The system according to claim 15 , wherein said sliding element comprises a wheel.

17. The system according to claim 13 , wherein on said frame of said first conveyor organ an outrigger is linked with and is supported by its end facing away from said frame, via an articulation linked there, against a sliding rail which is oriented in parallel with the longitudinal direction of said external conveyor organ and fastened to the latter, for slidable support of said external conveyor organ of said first conveyor organ substantially in the conveying direction on said external conveyor organ.

18. The system according to claim 13 , wherein said second conveyor organ is linked to said frame of said first conveyor organ such that it may be pivoted about an axis transversely to the conveying direction for modifying the height of the end of said second conveyor organ relative to its beginning.

19. The system according to claim 18 , wherein said first conveyor organ may be pivoted about an angular range of between approximately −15° and approximately +45°.

20. The system according claim 13 , wherein said third conveyor organ is linked to the end of said second conveyor organ such that it may be pivoted about an axis transversely to the conveying direction of said second conveyor organ, so that it may be oriented horizontally.

21. The system according to claim 13 , wherein said first conveyor organ with its frame is pivotally supported on said external conveyor organ such that a degree of pivoting said intermediate conveyor means about an angular range of about −30° to +30° relative to the conveying direction of said external conveyor organ may be selected.

22. The system according to claim 13 , wherein said second and/or third conveyor organ is associated with a parallelogram linkage arranged on either side of the edges of a conveyor organ, for supporting a lifting, lowering, or pivoting movement, so that such movements may be predetermined by a person working in the cargo hold approximately free of effort.

23. The system according to claim 13 , wherein in the range of said third conveyor organ a multi-function operating element is provided, whereby the horizontal orientation of said third conveyor organ, the inclination of said second conveyor organ, the position of said first conveyor organ on said external conveyor organ, the conveying direction, the conveying velocity, or further functions may be controlled.

24. The system according to claim 13 , wherein said third conveyor organ comprises a movable sliding organ.

25. The system according to claim 13 , wherein said third conveyor organ comprises an obliquely inclinable sliding surface.

26. The system according to claim 13 , wherein said third conveyor organ comprises a gripping organ for grasping loose cargo for unloading.

27. The system according to claim 13 , wherein said third conveyor organ comprises a conveyor belt running over a rigid slide panel arranged underneath it, wherein said slide panel may be inserted between two cargo items jointly with the conveyor belt, and wherein the upper loose cargo may be transported off by said conveyor belt.

28. The system according to claim 13 , wherein sensors, cameras, or control circuits communicating with said intermediate conveyor means are provided.

29. The system according to claim 13 , wherein said outrigger includes two arms.

30. A system for loading and unloading loose cargo in a cargo hold a plane, comprising:

transport means covering the area of the floor of the cargo hold for intermittently conveying the loose cargo towards the inner end of the cargo hold during loading, or away from it during unloading, wherein the front end of said transport means reaches into the range of the cargo hold opening inside the fuselage of the plane, and

an external conveyor organ connecting to the outside of the plane at the cargo hold opening for transporting the loose cargo between the level of the tarmac and the cargo hold opening,

wherein between the plane-side end of said external conveyor organ and the front end of said transport means in the cargo hold at least one intermediate conveyor means is arranged, whereby the loose cargo may during loading initially be conveyed deeper into the fuselage substantially transversely to the longitudinal axis of the plane,

said intermediate conveyor means comprising at least one frame supported against the external conveyor organ with a first conveyor organ including a first conveyor belt for receiving the loose cargo during loading, in the range in front of the cargo hold opening of the plane, from the end of said external conveyor organ facing the plane, and conveying it on substantially transversely to the longitudinal axis of the plane, wherein the end of said first conveyor organ is followed by a second conveyor organ including a second conveyor belt for bridging the distance from the end of said external conveyor organ to the inside of the cargo hold, for receiving loose cargo during loading, in the range of the cargo hold opening of the plane, from the end of said first conveyor organ, and conveying it on substantially transversely to the longitudinal axis of the plane,

wherein the end thereof is followed by a third conveyor organ including a roller panel for receiving loose cargo during loading from the end of said second conveyor organ and permitting manual rotation of the loose cargo located thereon, such that the loose cargo may be conveyed on substantially in the longitudinal direction of the plane to the front end of transport means present in the cargo hold.

31. The system according to claim 30 , wherein during unloading, loose cargo may be applied manually on said third conveyor organ from the front end of said transport means present in the cargo hold substantially in the longitudinal direction of the plane, rotatably placed there, and supported suitably for handover to said second conveyor organ, wherein said second conveyor organ conveys the loose cargo substantially transversely to the longitudinal axis of the plane to the cargo hold opening and/or through the latter and hands it over to said first conveyor organ, which conveys the loose cargo on substantially transversely to the longitudinal axis of the plane to said external conveyor organ and hands it over to the latter for further transport.

32. The system according to 30 , wherein said frame of said first conveyor organ comprises a sliding element at its lower side for a slidable support of said first conveyor organ substantially in the conveying direction of said external conveyor organ on the upper side of said external conveyor organ in the range of the end portion thereof facing the plane walls.

33. The system according to claim 32 , wherein said sliding element comprises a wheel.

34. The system according to claim 30 , wherein on said frame of said first conveyor organ an outrigger is linked with and is supported by its end facing away from said frame, via an articulation linked there, against a sliding rail which is oriented in parallel with the longitudinal direction of said external conveyor organ and fastened to the latter, for slidable support of said external conveyor organ of said first conveyor organ substantially in the conveying direction on said external conveyor organ.

35. The system according to claim 34 , wherein said outrigger includes two arms.

36. The system according to claim 30 , wherein said second conveyor organ is linked to said frame of said first conveyor organ such that it may be pivoted about an axis transversely to the conveying direction, for modifying the height of the end of said second conveyor organ relative to its beginning.

37. The system according to claim 36 , wherein said second conveyor organ may be pivoted about an angular range of between approximately −15° and approximately +45°.

38. The system according to claim 30 , wherein said third conveyor organ is linked to the end of said second conveyor organ such that it may be pivoted about an axis transversely to the conveying direction of said second conveyor organ, so that it may be oriented horizontally.

39. The system according to claim 30 , wherein said first conveyor organ with its frame is pivotally supported on said external conveyor organ such that a degree of pivoting said intermediate conveyor means about an angular range of about −30° to +30° relative to the conveying direction of said external conveyor organ may be selected.

40. The system according to claim 30 , wherein said second and/or third conveyor organ is associated with a parallelogram linkage arranged on either side of the edges of a conveyor organ, for supporting a lifting, lowering, or pivoting movement, so that such movements may be predetermined by a person working in the cargo hold approximately free of effort.

41. The system according to claim 30 , wherein in the range of said third conveyor organ a multi-function operating element is provided, whereby the horizontal orientation of said third conveyor organ, the inclination of said second conveyor organ, the position of said first conveyor organ on said external conveyor organ, the conveying direction, the conveying velocity, or further functions may be controlled.

Assignments (7)
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 →
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; TRANSDIGM UK HOLDINGS PLC; 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.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ 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 ERIE AVIATION; 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.
To: GOLDMAN SACHS BANK USA, AS ADMINISTRATIVE AGENT AND COLLATERAL AGENT
Reel/Frame 062880/0580 →
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 →
CHANGE OF NAME Recorded May 23, 2022
From: TELAIR INTERNATIONAL AB
To: TURNTIME TECHNOLOGIES AB
Reel/Frame 060160/0792 →
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 →