System for latching and locking a folding wing

Patent metadata

Field	Value
Publication number	US-9580166-B2
Application number	US-201414165561-A
Country	US
Kind code	B2
Filing date	Jan 27, 2014
Priority date	Jan 27, 2014
Publication date	Feb 28, 2017
Grant date	Feb 28, 2017

Abstract

A folding wing comprises a fixed section, a folding section, and a latch system for latching the folding section to the fixed section. The latch system includes a plurality of latch pins, and a corresponding plurality of non-backdriveable mechanical actuators for extending the latch pins to engage the folding section.

First claim

The invention claimed is:

1. A folding wing comprising:
a fixed section;
a folding section, the folding section hinged to the fixed section at a hinge line; and
a latch system for latching the folding section to the fixed section, the latch system including a plurality of non-backdriveable mechanical latch pin actuators, each non-backdriveable mechanical latch pin actuator comprising a long axis extending through a first end and a second end, each non-backdriveable mechanical latch pin actuator oriented so that the long axis is parallel with the hinge line, each non-backdriveable mechanical latch pin actuator comprising a latch pin, each latch pin configured to move along the long axis between a retracted position and an extended position, each latch pin in the extended position configured to engage the folding section, each non-backdriveable mechanical latch pin actuator further comprising a lock, each lock comprising a lock axis extending through a first side and a second side, each lock oriented so that the lock axis is orthogonal to the long axis, each lock rotatable about the lock axis between an unlocked position and a locked position, each lock configured to create physical interference with its corresponding latch pin in the locked position.

2. The wing of claim 1 , further comprising a drive line for transmitting mechanical power to the plurality of non-backdriveable mechanical latch pin actuators.

3. The wing of claim 2 , further comprising a brake for the drive line.

4. The wing of claim 1 , wherein the latch system is configured to extend one of the latch pins into the folding section before extending another latch pin into the folding section.

5. The wing of claim 1 , wherein each non-backdriveable mechanical latch pin actuator further comprises a housing for its corresponding latch pin, and a roller screw configured to move the latch pin between the retracted position and the extended position, the roller screw further configured to be non-backdriveable.

6. The wing of claim 5 , wherein each roller screw includes a threaded shaft, multiple threaded helical rollers assembled in a planetary arrangement around the threaded shaft, and a threaded nut containing the rollers.

7. The wing of claim 6 , wherein the roller screw has a pitch that allows one end of the threaded shaft to be turned, but does not allow an opposite end of the threaded shaft to be turned by forces acting along an axis of the latch pin.

8. The wing of claim 5 , wherein each lock is a cam lock.

9. The wing of claim 1 , wherein the folding section is a wing tip.

10. An aircraft comprising the folding wing of claim 1 .

11. A latch system for a wing having a fixed section and a folding section, the folding section hinged to the fixed section at a hinge line, the system comprising:
a latch pin configured to move between a retracted position and an extended position
along a long axis, the long axis parallel with the hinge line;
a non-backdriveable mechanical latch pin actuator configured to move the latch pin between the retracted position and the extended position and maintaining the latch pin in the extended position; and
a spring-biased mechanical lock, the spring-biased mechanical lock comprising a lock axis extending through a first side and a second side, the spring-biased mechanical lock oriented so that the lock axis is orthogonal to the long axis, the spring-biased mechanical lock rotatable about the lock axis between an unlocked position and a locked position, the spring-biased mechanical lock configured to create physical interference behind the latch pin after the latch pin has been moved to the extended position.

12. The system of claim 11 , further comprising a drive line for transmitting mechanical power to the non-backdriveable mechanical latch pin actuator.

13. The system of claim 12 , further comprising a brake for the drive line.

14. The system of claim 11 , wherein the non-backdriveable mechanical latch pin actuator further comprises a housing for the latch pin, and a roller screw configured to move the latch pin between the retracted position and the extended position, the roller screw further configured to be non-backdriveable.

Assignees

• Boeing Co

Inventors

• Good Mark S
• Walker Steven Paul
• Lassen Matthew A
• Pietersen Quentin T

Classifications

• Y10T403/32254

  Lockable at fixed position · CPC title

• Y02T50/145

  Cross-Sectional Technologies · mapped topic

• B64C3/56 Primary

  Folding or collapsing to reduce overall dimensions of aircraft · CPC title

• Y02T50/10

  Drag reduction · CPC title