Retractable cargo hook

Patent metadata

Field	Value
Publication number	US-12404022-B2
Application number	US-202117368218-A
Country	US
Kind code	B2
Filing date	Jul 6, 2021
Priority date	Jul 6, 2021
Publication date	Sep 2, 2025
Grant date	Sep 2, 2025

Abstract

A retractable cargo hook for aircraft is described. The cargo hook including a torsion spring allowing rotatable attachment to an aircraft body. An optional recessed portion of the aircraft body can house and receive the cargo hook. This can protect interior components from crashes which can push the cargo hook into the aircraft fuselage, damaging components.

First claim

What is claimed is:

1. A cargo hook for an aircraft, comprising:
an arm portion configured to be operatively coupled to the aircraft and comprising a first torsion spring, the first torsion spring configured to allow the arm portion to rotate about a first axis;
a load hook configured to be coupled to a cargo load that is outside of the aircraft;
a hook body coupled to the arm portion and to the load hook, wherein the hook body is coupled to the arm portion by a second torsion spring configured to allow the hook body to rotate about a second axis, wherein the arm portion defines a plane that includes the first axis, wherein the second axis is perpendicular to the plane, wherein the first torsion spring is configured to rotatably bias the hook body about the first axis and relative to a surface of the aircraft; and
an attachment plate having a top-most surface which is configured to contact the surface of the aircraft, wherein the attachment plate is configured to support the entirety of the arm portion, wherein the attachment plate includes a first mount and a second mount,
wherein the arm portion includes a first projection and a second projection, wherein the first and second projections are each positioned between the first mount and the second mount of the attachment plate, wherein the first torsion spring is positioned between the first mount and the second mount and between the first projection and the second projection.

2. The cargo hook of claim 1 wherein the arm portion comprises a metal.

3. The cargo hook of claim 1 wherein the first torsion spring is configured to bias the cargo hook in one direction toward the aircraft and away from vertical.

4. The cargo hook of claim 1 wherein the first and second torsion springs are configured to bias the cargo hook to a rest position with an L shape.

5. The cargo hook of claim 1 wherein the torsion spring comprises steel.

6. The cargo hook of claim 1 , wherein the surface of the aircraft is downward facing.

7. The cargo hook of claim 1 wherein the attachment plate is rotatably coupled to the arm portion and the first torsion spring about the first axis and configured to be attached to the aircraft to thereby bias the hook body about the first axis and the aircraft.

8. The cargo hook of claim 7 wherein the attachment plate is configured to be bolted to the aircraft.

Assignees

• Bell Textron Inc
• Textron Innovations Inc

Inventors

• Rodrigue Simon
• Duval Sebastien

Classifications

• B64D1/10

  Stowage arrangements for the devices in aircraft · CPC title

• B64D1/14

  Absorbing landing shocks · CPC title

• B64D2201/00

  Airbags mounted in aircraft for any use · CPC title

• B64D1/12 Primary

  Releasing · CPC title

• B64C27/06

  with single rotor · CPC title