Offset flange floor panel connection system

Patent metadata

Field	Value
Publication number	US-11608155-B2
Application number	US-202016933991-A
Country	US
Kind code	B2
Filing date	Jul 20, 2020
Priority date	May 15, 2017
Publication date	Mar 21, 2023
Grant date	Mar 21, 2023

Abstract

A floor panel connection system for attaching a floor panel to an airframe is disclosed. The connection system includes an offset flange insert comprising a base portion, a flange portion, and an interconnect portion. The base portion of the insert is configured to be received in a hole in an edge region of the floor panel and includes an opening that is sized to receive a fastener. The interconnect portion extends laterally from the base portion such that when the edge portion of the floor panel is overlapping a lateral edge portion of the airframe, the flange portion of the insert is beyond the lateral edge portion. The flange portion is also configured to be bonded to a bottom surface of the floor panel beyond the lateral edge portion of the airframe.

First claim

We claim:

1. A floor panel assembly for an aircraft, comprising:
a planar expanse having a top face, a bottom face, an edge region, and a hole in the edge region; and
an insert having a base portion and a flange portion, the base portion being configured to be received in the hole of the edge region and the flange portion being configured to be bonded to the bottom face adjacent the hole but beyond a lateral edge portion of an airframe when the edge region is in overlapping engagement with the lateral edge portion of the airframe.

2. The floor panel assembly of claim 1 , wherein the insert further includes an interconnect portion disposed between the base and flange portions, the edge region includes an elongate recess adjacent to the hole and sized to receive the interconnect portion, and wherein the hole is within an end of the elongate recess of the edge region.

3. The floor panel assembly of claim 2 , wherein the interconnect portion includes at least one bridge that connects the base portion to the flange portion.

4. The floor panel assembly of claim 1 , wherein the flange portion is planar, and the base portion includes a vertical axis, the planar flange portion is within a plane that is perpendicular to the vertical axis, and the base is not within the plane.

5. The floor panel assembly of claim 1 , wherein the base portion of the insert includes an opening sized to receive at least one fastener.

6. The floor panel assembly of claim 5 , further including a fastener configured to be inserted through the opening of the base portion of the insert and an aperture of the airframe.

7. A floor panel connection system, comprising:
an aircraft airframe having a lateral edge portion with a plurality of apertures;
a planar expanse having an edge region configured for overlapping engagement with the lateral edge portion of the airframe, the edge region including a hole; and
an insert having a base portion and a flange portion, the base portion being configured to be received in the hole of the edge region and the flange portion being configured to be bonded to a bottom face of the planar expanse adjacent the hole but beyond a lateral edge portion of the aircraft airframe when the edge region is in overlapping engagement with the lateral edge portion of the airframe.

8. The floor panel connection system of claim 7 , wherein the base portion includes an opening configured to align with an aperture of the plurality of apertures of the aircraft airframe.

9. The floor panel connection system of claim 8 , further including a fastener configured to be inserted through the opening of the base portion when the opening is in alignment with the aperture of the aircraft airframe.

10. The floor panel connection system of claim 7 , wherein the insert further includes an interconnect portion disposed between the base and flange portions, and the edge region includes an elongate recess adjacent to the hole and sized to receive the interconnect portion.

11. The floor panel connection system of claim 10 , wherein the hole is within an end of the elongate recess of the edge region.

12. The floor panel connection system of claim 10 , wherein the interconnect portion includes at least one bridge that connects the base portion to the flange portion.

13. The floor panel connection system of claim 10 , wherein the flange portion is planar, and the base portion includes a vertical axis, the planar flange portion is within a plane that is perpendicular to the vertical axis, and the base portion and interconnect portions are not within the plane.

14. A method of assembling a floor panel of an airplane, comprising:
positioning an insert in a hole of an edge region of a planar expanse, the insert including a base portion and a flange portion;
bonding the flange portion of the insert to a bottom face of the planar expanse, adjacent the hole of the edge region;
overlapping the edge region of the planar expanse with a lateral edge portion of an airframe such that the flange portion of the insert does not contact the lateral edge portion of the airframe.

15. The method of claim 14 , wherein overlapping the edge region of the planar expanse with the lateral edge portion of the airframe includes aligning an opening of the base portion of the insert with an aperture of the airframe.

16. The method of claim 15 , further including:
inserting a fastener through the opening of the base portion of the insert and the aperture of the airframe to attach the planar expanse to the airframe.

17. The method of claim 16 , wherein inserting a fastener includes: (a) inserting an expanding nut through the opening of the base portion and through the aperture of the lateral edge portion, and (b) inserting a screw through an opening of the expanding nut, such that an end portion of the expanding nut engages the lateral edge portion.

18. The floor panel connection system of claim 10 , wherein the flange portion contacts the bottom face when (a) the base portion is received in the hole and (b) the interconnect portion is received in the elongate recess.

19. The floor panel connection system of claim 18 , wherein, when (a) the base portion is received in the hole and (b) the interconnect portion is received in the elongate recess, the flange portion contacts the bottom face and the base portion and the interconnect portion do not extend beyond the bottom face.

20. The floor panel connection system of claim 7 , wherein the lateral edge portion of the airframe is scalloped, and the flange portion of the insert is kidney-shaped to correspond to the scalloped lateral edge portion.

Assignees

• Boeing Co

Inventors

• Mills Christopher J
• Yang Emily
• Durbin Michael Patrick

Classifications

• B64C1/18 Primary

  Floors · CPC title

• B64D11/0696

  Means for fastening seats to floors, e.g. to floor rails · CPC title

• Y02T50/40

  Weight reduction · CPC title