IP Library Granted Patent US 12,263,946
Granted Patent B2
US 12,263,946 · App. 18/056,892 · Granted Apr 1, 2025

Installment system for overhead bins

Inventors: Nathan Earl Esau (Wichita, KS); Jonathan Lynn Headrick (Peck, KS)
Assignee: Textron Innovations Inc.
B64D11/003B64C1/066
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Quick Facts
Patent No.
US 12,263,946
App. No.
18/056,892
Granted
Apr 1, 2025
Kind
B2
Abstract

An overhead bin in an aircraft includes a liner disposed on an underside of a cabin ceiling and a receptacle that protrudes through an opening in the liner. A bin has a top side with at least one attachment point that includes: a stud mechanically coupled to the top side and a screw disposed within the stud. The stud includes a rounded flange configured to insert into the receptacle for removably securing the bin beneath the liner. An installation method for an overhead bin in an aircraft includes raising the overhead bin to engage the stud with the receptacle, sliding the overhead bin outboard for inserting the stud into the receptacle, and turning a screw within the stud for tightening the stud within the receptacle for securing the overhead bin beneath the ceiling.

Claims (29)

1. An installment system for an overhead bin in an aircraft, comprising:

a receptacle mechanically coupled to a structure above a cabin ceiling of the aircraft via a bracket, wherein the receptacle protrudes through an opening in a liner disposed on an underside of the cabin ceiling; and

a bin having a top side with at least one attachment point, the at least one attachment point comprising:

a stud mechanically coupled to the top side; and

a screw disposed within the stud,

wherein the stud comprises a rounded flange configured to insert into the receptacle for removably securing the bin beneath the liner.

2. The system of claim 1 , wherein the receptacle comprises a slot having wide openings at opposing ends and a narrow portion therebetween, wherein the stud is configured for insertion of the rounded flange into the slot via one of the wide openings and for inserting the rounded flange into the narrow portion.

3. The system of claim 2 , wherein the receptacle comprises:

a hole above the slot facing downward at the narrow portion; and

an end of the screw is configured to engage the hole when the bin is installed.

4. The system of claim 1 , wherein the stud comprises internal threads configured to receive the screw.

5. The system of claim 4 , wherein the screw is configured to be turned within the internal threads for engaging of the rounded flange within the receptacle.

6. The system of claim 5 , wherein the screw is configured to be turned via a screwdriver.

7. An installation method for an overhead bin in an aircraft, wherein the overhead bin comprises at least one stud on a top side of the overhead bin and a ceiling of the aircraft comprises at least one receptacle, the installation method comprising:

raising the overhead bin to engage the at least one stud with the at least one receptacle;

sliding the overhead bin in an outboard direction for inserting the at least one stud into a narrow portion of the at least one receptacle; and

turning a screw disposed within the at least one stud in a first direction for engaging within the at least one receptacle, thereby securing the overhead bin beneath the ceiling.

8. The method of claim 7 , comprising turning the screw disposed within the at least one stud in a second direction opposite the first direction for disengaging within the at least one receptacle, thereby releasing the overhead bin for removal from the ceiling.

9. The method of claim 7 , comprising configuring the aircraft for providing storage for an individual trip by installing one or more overhead bins.

10. The method of claim 7 , comprising configuring the aircraft for reducing weight and increasing overhead cabin space for an individual trip by removing one or more overhead bins.

11. A removable bin installment system for use in an aircraft, comprising:

a plurality of brackets mounted to an overhead structure above a ceiling in the aircraft, wherein an underside of the ceiling comprises a liner having a finished surface;

a plurality of receptacles each mechanically coupled to a respective one of the brackets, wherein the liner comprises a plurality of openings configured to each receive a respective one of the receptacles for protruding through the liner; and

a removable bin having a top side with a plurality of attachment points, each of the attachment points comprising:

a stud mechanically coupled to the top side, wherein the stud comprises an exposed end having a larger diameter configured for inserting into a respective one of the receptacles; and

a screw disposed within the stud, wherein the screw is configured for turning thereby tightening the stud within the receptacle for removably securing the removable bin beneath the ceiling.

12. The removable bin installment system of claim 11 , wherein the receptacles each comprise: a slot having a wide opening configured for receiving the exposed end of the stud; and a narrow portion configured for securing the exposed end of the stud thereto.

13. The removable bin installment system of claim 12 , wherein the receptacles each comprise a hole above the slot in the narrow portion such that an end of the screw is configured for engaging the hole when the removable bin is installed.

14. The removable bin installment system of claim 13 , wherein the screw is coupled with the stud via threads such that tightening of the screw is configured to secure the removable bin or loosening of the screw is configured to unsecure the removable bin.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 31, 2023
From: TEXTRON AVIATION INC.
To: TEXTRON AVIATION RHODE ISLAND INC.
Reel/Frame 063815/0658 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 31, 2023
From: TEXTRON AVIATION RHODE ISLAND INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 063815/0689 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 18, 2022
From: ESAU, NATHAN EARL; HEADRICK, JONATHAN LYNN
To: TEXTRON AVIATION INC.
Reel/Frame 061824/0448 →
Continuity (2)
Provisional Application 63281222 · Nov 19, 2021
Related Publication 20230159170A1 · May 25, 2023
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