Aircraft component coupling assembly and coupler for aircraft components

Patent metadata

Field	Value
Publication number	US-12305690-B2
Application number	US-202117531808-A
Country	US
Kind code	B2
Filing date	Nov 22, 2021
Priority date	May 23, 2019
Publication date	May 20, 2025
Grant date	May 20, 2025

Abstract

An aircraft component coupling assembly includes first and second plate structures placed and a coupler coupling the first and second plate structures. The first plate structure includes a first insertion hole and a first serration located on a first outer surface of the first plate structure and surrounding the first insertion hole. The second plate structure includes a second insertion hole differing in inner diameter from the first insertion hole. The coupler includes: a contact structure including a second serration and a third insertion hole; a shaft structure being fixedly engaged with one of a second outer surface the second plate structure and a third outer surface of the contact structure; and a pressing structure engaged with the shaft structure and pressing an other of the second outer surface of the second plate structure and the third outer surface of the contact structure.

First claim

The invention claimed is:

1. A coupling assembly, comprising:
a first plate structure;
a second plate structure; and
a coupler coupling the first plate structure and the second plate structure, wherein
the first plate structure includes a first insertion hole and a first serration located on a first outer surface of the first plate structure and surrounding the first insertion hole, the first outer surface facing away from the second plate structure,
the second plate structure includes a second insertion hole in having an inner diameter smaller than an inner diameter of the first insertion hole, and
the coupler includes:
a contact structure including a second serration and a third insertion hole, the second serration contacting the first outer surface of the first plate structure and meshing with the first serration of the first plate structure,
a shaft structure which contacts an inner circumferential surface of the second insertion hole and an inner circumferential surface of the third insertion hole and does not contact an inner circumferential surface of the first insertion hole when inserted through the first, second and third insertion holes, the shaft structure including a fixed engagement portion fixedly engaged with one of a second outer surface of the second plate structure and a third outer surface of the contact structure, and
a pressing structure engaged with the shaft structure and pressing an other of the second outer surface of the second plate structure and the third outer surface of the contact structure.

2. The coupling assembly according to claim 1 , wherein
the shaft structure has an outer diameter equal to inner diameters of the second insertion hole of the second plate structure and the third insertion hole of the contact structure, and
the inner diameters of the second and third insertion holes are smaller than the inner diameter of the first insertion hole.

3. The coupling assembly according to claim 1 , wherein
the fixed engagement portion is located at an end of the shaft structure opposite a distal insertion part of the shaft structure, the distal insertion part being inserted into and through the first, second, and third insertion holes, and
the second serration is placed to mesh with the first serration in a direction from the distal insertion part to the opposite end of the shaft structure.

4. The coupling assembly according to claim 1 , wherein
the shaft structure includes a shaft portion including an external thread on a circumferential surface of the shaft portion,
the pressing structure is a nut including an internal thread engageable with the external thread, and
the external thread and internal thread are engaged to press the second serration against the first serration.

5. The coupling assembly according to claim 4 , wherein
the shaft structure includes a bolt including a head,
the shaft portion is a shaft of the bolt,
the fixed engagement portion is the head of the bolt, and
the contact structure is a plate fitted around the shaft of the bolt.

6. The coupling assembly according to claim 1 , wherein facing surfaces of the first and second plate structures are flat.

7. The coupling assembly according to claim 1 , wherein the contact structure includes the third insertion hole, a contact plate, and a coupler serrated element placed on and secured to the contact plate, the coupler serrated element including the second serration.

8. The coupling assembly according to claim 1 , wherein the first plate structure includes the first insertion hole, a base plate, and a plate serrated element placed on and secured to the base plate, the plate serrated element including the first serration.

9. A coupler for aircraft components that couples a first plate structure and a second plate structure, the first plate structure including a first insertion hole and a first serration located on a first outer surface of the first plate structure and surrounding the first insertion hole, the second plate structure including a second insertion hole having an inner diameter smaller than an inner diameter of the first insertion hole, the coupler comprising:
a contact structure including a second serration and a third insertion hole, the second serration being contacted with the first outer surface of the first plate structure to mesh with the first serration of the first plate structure;
a shaft structure which contacts an inner circumferential surface of the second insertion hole and an inner circumferential surface of the third insertion hole and does not contact an inner circumferential surface of the first insertion hole when inserted through the first, second and third insertion holes, the shaft structure including a fixed engagement portion that is fixedly engaged with one of a second outer surface of the second plate structure and a third outer surface of the contact structure; and
a pressing structure that is engaged with the shaft structure to press an other of the second outer surface of the second plate structure and the third outer surface of the contact structure.

10. The coupler according to claim 9 , wherein the shaft structure has an outer diameter equal to inner diameters of the second insertion hole of the second plate structure and the third insertion hole of the contact structure.

11. The coupler according to claim 10 , wherein the inner diameters of the second and third insertion holes are smaller than the inner diameter of the first insertion hole.

12. The coupler according to claim 9 , wherein the contact structure includes the third insertion hole, a contact plate, and a coupler serrated element placed on and secured to the contact plate, the coupler serrated element including the second serration.

13. A coupling assembly, comprising:
a frame including a first insertion hole and a first serration, the first insertion hole having a first diameter, and the first serration being located on a first outer surface of the frame and surrounding the first insertion hole;
a beam including a second insertion hole having a second diameter smaller than the first diameter; and
a coupler that couples the frame to the beam, the coupler including:
a contact plate including a second serration and a third insertion hole, the second serration contacting the first outer surface of the frame and meshing with the first serration of the frame,
a shaft which contacts an inner circumferential surface of the second insertion hole and an inner circumferential surface of the third insertion hole and does not contact an inner circumferential surface of the first insertion hole when inserted through the first insertion hole, the second insertion hole and the third insertion hole, the shaft including a fixed engagement portion fixedly engaged with one of a second outer surface of the beam and a third outer surface of the contact plate, and
a pressing nut engaged with the shaft and pressing an other of the second outer surface of the beam and the third outer surface of the contact plate, wherein

the first outer surface of the frame faces away from the beam.

14. The coupling assembly according to claim 13 , wherein
the shaft has an outer diameter equal to inner diameters of the second insertion hole of the beam and the third insertion hole of the contact plate, and
the inner diameters of the second and third insertion holes are smaller than the first diameter of the first insertion hole.

15. The coupling assembly according to claim 13 , wherein
the fixed engagement portion is located at an end of the shaft opposite a distal insertion part of the shaft, the distal insertion p

Assignees

• Kawasaki Heavy Ind Ltd

Inventors

• Tanaka Kentaro
• Nawata Kunio
• Ishimoto Sachinori
• Nakaya Kota
• Akasaka Tatsuro

Classifications

• F16B5/02

  by means of fastening members using screw-thread ({F16B5/0004 takes precedence}; construction of screw-threaded connections F16B25/00 - F16B39/00) · CPC title

• B64C1/069

  Joining arrangements therefor · CPC title

• F16B35/045

  for retention or rotation by a tool (specially shaped heads of bolts or screws for rotation by a tool F16B23/00) · CPC title

• F16B5/0225

  allowing for adjustment parallel to the plane of the plates · CPC title

• F16B43/00 Primary

  Washers or equivalent devices; Other devices for supporting bolt-heads or nuts (circlips F16B21/18; {for indicating tensile load F16B31/02; forming a whole with the bolt or nut F16B33/00; locking bolts or nuts by means of a fixed plate or ring, or washer-like resilient plates F16B39/10, F16B39/24}) · CPC title