IP Library Granted Patent US 6,902,137
Granted Patent B2
US 6,902,137 · App. 10/241,283 · Granted Jun 7, 2005

Aircraft door latch/lock mechanism with pneumatic decompression override

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Quick Facts
Patent No.
US 6,902,137
App. No.
10/241,283
Granted
Jun 7, 2005
Kind
B2
Abstract

A door latch mechanism mounted in a door frame cooperates with a door bolt separating the cockpit compartment on an aircraft from the passenger compartment. The mechanism prevents a hijacker from entering the cockpit compartment and allows the door to open rapidly when a catastrophic decompression event occurs in the airplane.

Claims (41)

1. A door strike mechanism to be mounted in a door frame to cooperate with a door latch on a door, said mechanism comprising:

a support;

a catch moveably mounted on the support in position to engage the door latch to hold the door closed;

a biasing element urging the catch into position to hold the door closed;

a pin having a locking position in which it prevents the catch from moving out of the door closed position;

a pressure responsive sensor initiating action to move the pin into an unlocked position permitting the catch to move when a sudden change in air pressure on one side of the door occurs, thus allowing the door to open;

a first roller mounted on said catch to engage one side of the pin when an opening force is applied to the door; and

a second roller rotatably mounted on said support and engaging an opposite side of the pin to receive a load applied to the catch, said first and second rollers being mounted to be in rolling engagement with said pin to aid in movement of said pin when it is being moved to the unlocked position.

2. The mechanism of claim 1 wherein the pin is axially moveable and each roller is mounted on an axis that is substantially perpendicular to the pin axis.

3. The mechanism of claim 1 wherein said first and second rollers engage a tip of the pin and the tip is tapered to facilitate the withdrawal of said pin from engagement with said first and second rollers.

4. The mechanism of claim 3 wherein the taper on the pin tip is no more than about 12°.

5. The mechanism of claim 3 wherein the taper of said tip is in the range of about 4° 6°.

6. The mechanism of claim 5 wherein the taper of said tip is about 5°.

7. The mechanism of claim 1 including an actuator for moving the pin between the locking position and the unlocked position, and wherein said sensor provides a signal to energize the actuator.

8. The mechanism of claim 7 wherein said actuator is a solenoid.

9. The mechanism of claim 8 wherein the solenoid provides mechanical force urging said pin into retracted position so as to obtain fast action.

10. The mechanism of claim 1 wherein said biasing element is a spring.

11. A door strike mechanism to be mounted in a door frame to cooperate with a door latch on a door, said mechanism comprising:

a support;

a catch pivotally mounted on the support in position to engage the door latch to hold the door closed;

a spring urging the catch into position to hold the door closed;

a pin having a locking position in which a tip of the pin prevents the catch from moving out of the door closed position, the pin being positioned so that a force applied to the pin by the catch is transferred to said support;

a solenoid for axially moving the pin between the locking position and an unlocked position in which the tip of the pin is retracted to permit the catch to move against the urging of said spring; and

a pressure responsive sensor providing a signal to the solenoid to move the pin into the unlocked position when a sudden change in air pressure on one side of the door occurs.

12. The mechanism of claim 11 , including a first roller mounted on said catch to engage the pin when an opening force is applied to the door, and a second roller rotatably mounted on said support and engaging an opposite side of the pin to provide lateral support to the pin when a large force is applied to said door, said first and second rollers being mounted to guide said pin in rolling engagement to facilitate retraction of said pin.

13. The mechanism of claim 12 wherein the tip of the pin is tapered to facilitate the withdrawal of said pin from engagement with said first and second rollers.

14. The mechanism of claim 13 wherein the taper on the pin tip is no more than about 12°.

15. The mechanism of claim 13 wherein the taper on the pin tip is in the range of about 4°-6°.

16. The mechanism of claim 15 wherein the taper of said tip is about 5°.

17. The mechanism of claim 11 wherein the solenoid is configured to provide mechanical force and electrical force to urge said pin into retracted position so as to obtain fast action.

18. A door strike mechanism to be mounted in a door frame to cooperate with a door latch on a door, said mechanism comprising:

a pivotally mounted catch;

a spring urging the catch into position to hold the door closed;

an axially moveable pin; and

a pair of rollers positioned to guide the movement of the pin, one of the rollers being mounted on the catch to transmit load from the catch to the pin, and the other being mounted on a support to transmit the load to the support, said pin being moveable between a locking position preventing pivoting of the catch and an unlocked position in which the pin is withdrawn from the rollers to permit the catch to pivot in response to a predetermined force applied to the door.

19. A method of preventing a door being manually forced open while permitting the door to open in response to sudden air pressure drop on one side of the door, said method comprising the steps of:

providing a door catch which is urged into position to engage a door latch to hold the door closed;

providing a pin to block movement of the catch that would release the door latch;

engaging one side of a tip of the pin with a first roller mounted on the catch;

engaging an opposite side of the pin tip with a second roller mounted to a support to receive a door opening force;

providing an actuator to retract the pin in response to a sudden air pressure drop so as to allow the catch to move to a door open position in response to a door opening force large enough to cause the catch to move to release the latch, said first and second rollers being configured to facilitate retraction of said pin.

Assignments (4)
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 →
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 →