Ceiling retaining assemblies and methods for an internal cabin of a vehicle

Patent metadata

Field	Value
Publication number	US-11472553-B2
Application number	US-202016748952-A
Country	US
Kind code	B2
Filing date	Jan 22, 2020
Priority date	Jan 22, 2020
Publication date	Oct 18, 2022
Grant date	Oct 18, 2022

Abstract

A retaining assembly and method for use within an internal cabin of an aircraft, in which the retaining assembly includes a hinge including a biasing member. The hinge is moveable between a retaining position, in which the biasing member is configured to exert a biasing force into a top surface of a ceiling panel within an internal cabin of a vehicle to prevent the ceiling panel from upward motion, and a release position, in which the hinge is configured to be pivoted away from the ceiling panel and the biasing member is configured to be separated from the ceiling panel.

First claim

What is claimed is:

1. A retaining assembly comprising:
a hinge comprising a biasing member, wherein the hinge is moveable between a retaining position, in which the biasing member is configured to exert a biasing force into a top surface of a ceiling panel within an internal cabin of a vehicle to prevent the ceiling panel from upward motion, and a release position, in which the hinge is configured to be pivoted away from the ceiling panel and the biasing member is configured to be separated from the ceiling panel; and
a plunger that is configured to selectively extend into and retract from a channel of a pivot restraint spur of the hinge, wherein upward pivotal motion of the hinge is restrained when the plunger extends into the channel.

2. The retaining assembly of claim 1 , further comprising:
a base, wherein a portion of the ceiling panel is configured to be sandwiched between the biasing member and the base when the hinge is in the retaining position; and
a wall connected to the base, wherein the hinge is pivotally coupled to the wall, and wherein the wall is configured to secure the retaining assembly to a rail connected to a strongback of an overhead stowage bin assembly.

3. The retaining assembly of claim 2 , wherein the wall comprises one or more fastener through-holes that retain fasteners that are configured to secure the retaining assembly to the rail.

4. The retaining assembly of claim 2 , wherein the hinge is pivotally coupled to the wall through an axle.

5. The retaining assembly of claim 1 , wherein the plunger comprises a shaft having a distal end that is configured to be pushed into the channel and pulled out of the channel.

6. The retaining assembly of claim 1 , wherein the biasing member is coupled to a pivot coupler of the hinge, and wherein the biasing member comprises:
an extension beam extending below the pivot coupler, wherein the extension beam is pivotally coupled to the pivot coupler through an axle; and
a coil spring extending between the pivot coupler and the extension beam, wherein the coil spring is configured to bias at least a portion of the extension beam onto the top surface of the ceiling panel when the hinge is in the retaining position.

7. The retaining assembly of claim 6 , wherein the portion comprises an expanded panel engagement member that is configured to abut against the top surface of the ceiling panel when the hinge is in the retaining position.

8. The retaining assembly of claim 1 , wherein the biasing member comprises a spring steel strap.

9. The retaining assembly of claim 8 , wherein the spring steel strap comprises:
a securing segment secured to the hinge;
an extension segment connected to the securing segment, wherein the extension segment outwardly and downwardly extends from the hinge; and
an engagement member connected to the extension segment, wherein the engagement member is configured to engage the top surface of the ceiling panel.

10. A method comprising:
providing a retaining assembly comprising a hinge that includes a biasing member;
moving the hinge into a retaining position, wherein said moving the hinge into the retaining position causes the biasing member to exert a biasing force into a top surface of a ceiling panel within an internal cabin of a vehicle to prevent the ceiling panel from upward motion;
moving the hinge into a release position, wherein said moving the hinge into the release position pivots the hinge away from the ceiling panel and separates the biasing member from the ceiling panel; and
extending a plunger into a channel of a pivot restraint spur of the hinge when the hinge is in the retaining position, wherein said extending restrains pivotal motion of the hinge; and retracting the plunger from the channel of the pivot restraint spur to allow the hinge to move into the release position.

11. The method of claim 10 , further comprising sandwiching a portion of the ceiling panel between the biasing member and a base of the retaining assembly when the hinge is in the retaining position.

12. The method of claim 10 , further comprising:
pivotally coupling the hinge to a wall of the retaining assembly; and
securing the wall to a rail connected to a strongback of an overhead stowage bin assembly.

13. The method of claim 10 , wherein said moving the hinge into the retaining position comprises biasing, by a coil spring of the biasing member, the portion of the extension beam onto the top surface of the ceiling panel when the hinge is in the retaining position.

14. The method of claim 10 , wherein said moving the hinge into the retaining position comprises biasing a spring steel strap of the biasing member onto the top surface of the ceiling panel when the hinge is in the retaining position.

15. An aircraft comprising:
an internal cabin;
a stowage bin assembly within the internal cabin;
a monument within the internal cabin;
a ceiling panel extending between the stowage bin assembly and the monument; and
a retaining assembly comprising:
a hinge comprising a biasing member, wherein the hinge is moveable between a retaining position, in which the biasing member exerts a biasing force into a top surface of the ceiling panel to prevent the ceiling panel from upward motion, and a release position, in which the hinge is pivoted away from the ceiling panel and the biasing member is separated from the ceiling panel;
a base, wherein a portion of the ceiling panel is sandwiched between the biasing member and the base when the hinge is in the retaining position;
a wall connected to the base, wherein the hinge is pivotally coupled to the wall, and wherein the wall secures the retaining assembly to a rail connected to a strongback of an overhead stowage bin assembly; and
a plunger that is configured to selectively extend into and retract from a channel of a pivot restraint spur of the hinge, wherein upward pivotal motion of the hinge is restrained when the plunger extends into the channel.

16. The aircraft of claim 15 , wherein the biasing member is coupled to a pivot coupler of the hinge, and wherein the biasing member comprises:
an extension beam extending below the pivot coupler, wherein the extension beam is pivotally coupled to the pivot coupler through an axle; and
a coil spring extending between the pivot coupler and the extension beam, wherein the coil spring biases at least a portion of the extension beam onto the top surface of the ceiling panel when the hinge is in the retaining position.

17. The aircraft of claim 15 , wherein the biasing member comprises a spring steel strap.

18. The aircraft of claim 17 , wherein the spring steel strap comprises:
a securing segment secured to the hinge;
an extension segment connected to the securing segment, wherein the extension segment outwardly and downwardly extends from the hinge; and
an engagement member connected to the extension segment, wherein the engagement member is configured to engage the top surface of the ceiling panel.

19. The aircraft of claim 15 , wherein the wall comprises one or more fastener through-holes that retain fasteners that are configured to secure the retaining assembly to the rail.

20. The aircraft of claim 15 , wherein the hinge is pivotally coupled to the wall through an axle.

Assignees

• Boeing Co

Inventors

• Logue Adam Arthur
• Bundy Bryan Charles
• Cartwright Jeffrey Allen

Classifications

• B64D11/00 Primary

  Passenger or crew accommodation; Flight-deck installations not otherwise provided for · CPC title

• B64C1/066 Primary

  Interior liners · CPC title

• B64D11/003

  Stowage devices for passengers' personal luggage · CPC title