Aircraft pressure deck

Patent metadata

Field	Value
Publication number	US-11358699-B2
Application number	US-202016841947-A
Country	US
Kind code	B2
Filing date	Apr 7, 2020
Priority date	Apr 7, 2020
Publication date	Jun 14, 2022
Grant date	Jun 14, 2022

Abstract

Embodiments for aircraft pressure deck. One embodiment is a pressure deck of an aircraft. The pressure deck includes beams extending longitudinally along a fuselage of the aircraft, and a web attached to an underside of the beams, the web including arches between adjacent beams to allow the pressure deck to flex laterally. The pressure deck also includes a box structure between a middle pair of the beams and configured to transfer load forward to a rear spar of a wing of the aircraft and aft to an aft wheel well bulkhead of the aircraft. The pressure deck further includes a first intercostal outboard from the box structure and configured to stabilize a first outboard pair of the beams, and a second intercostal outboard from the first intercostal and coupled between a second outboard pair of the beams via a swing link to allow the second intercostal to flex laterally.

First claim

What is claimed is:

1. A pressure deck of an aircraft, the pressure deck comprising:
beams extending longitudinally along a fuselage of the aircraft and spaced from one another in a lateral direction, wherein the beams include a middle pair of beams, and outboard beams spaced in the lateral direction from the middle pair of beams on each side of the pressure deck;
a web attached to an underside of the beams, the web including arches between adjacent beams to allow the pressure deck to flex laterally;
a box structure between the middle pair of the beams, and configured to transfer a load forward to a rear spar of a wing of the aircraft and aft to an aft wheel well bulkhead of the aircraft;
each side of the pressure deck comprising:
a tension strap coupled between one of the middle pair of the beams and a first one of the outboard beams in the lateral direction, wherein the tension strap is configured to support lateral forces between the one of the middle pair of beams and the first one of the outboard beams via tension, and to bend in response to compression;
a first intercostal coupled between the first one of the outboard beams and a second one of the outboard beams in the lateral direction, and configured to stabilize the first one of the outboard beams and the second one of the outboard beams with a fixed lateral structure; and
a second intercostal coupled between the second one of the outboard beams and a third one of the outboard beams in the lateral direction, and configured to flex laterally;
wherein the third one of the outboard beams couples with a fuselage frame;
wherein the second intercostal is configured to transfer a vertical load to the second one of the outboard beams and the third one of the outboard beams, and to transfer a lateral load to the fuselage frame.

2. The pressure deck of claim 1 wherein:
the second intercostal is coupled to the second one of the outboard beams via a swing link to flex laterally;
the swing link comprises a structural member having a first pinned connection with the second intercostal and a second pinned connection with the second one of the outboard beams; and
the second intercostal is coupled to the third one of the outboard beams via a pin.

3. The pressure deck of claim 1 wherein:
the first intercostal includes a lower section to fixedly couple between the first one of the outboard beams and the second one of the outboard beams, and an upper section to fixedly couple between the first one of the outboard beams and the second one of the outboard beams separately from the lower section, and
a space between the lower section and the upper section of the first intercostal is configured to accommodate aircraft systems routing.

4. The pressure deck of claim 2 wherein:
the second pinned connection of the swing link attaches directly to the second one of the outboard beams.

5. The pressure deck of claim 2 wherein:
the second pinned connection of the swing link attaches indirectly to the second one of the outboard beams.

6. The pressure deck of claim 1 wherein:
the web is flat underneath the box structure.

7. The pressure deck of claim 1 wherein:
the box structure includes a forward intercostal coupling the middle pair of the beams, an aft intercostal coupling the middle pair of the beams, and an upper truss coupling the forward intercostal and the aft intercostal.

8. The pressure deck of claim 1 wherein:
the pressure deck is vertically disposed between a cabin and a main wheel well of the aircraft.

9. The pressure deck of claim 8 wherein:
the arches of the web are configured to support pressure from the cabin that is disposed above the pressure deck.

10. An aircraft comprising:
a fuselage; and
a pressure deck comprising:
beams extending longitudinally along the fuselage and spaced from one another in a lateral direction, wherein the beams include a middle pair of beams, and outboard beams spaced in the lateral direction from the middle pair of beams on each side of the pressure deck;
a web attached to an underside of the beams, the web including arches between adjacent beams to allow the pressure deck to flex laterally;
a box structure between the middle pair of the beams, and configured to transfer a load forward to a rear spar of a wing of the aircraft and aft to an aft wheel well bulkhead of the aircraft;
each side of the pressure deck comprising:
a tension strap coupled between one of the middle pair of the beams and a first one of the outboard beams in the lateral direction, wherein the tension strap is configured to support lateral forces between the one of the middle pair of beams and the first one of the outboard beams via tension, and to bend in response to compression;
a first intercostal coupled between the first one of the outboard beams and a second one of the outboard beams in the lateral direction, and configured to stabilize the first one of the outboard beams and the second one of the outboard beams with a fixed lateral structure; and
a second intercostal coupled between the second one of the outboard beams and a third one of the outboard beams in the lateral direction, and configured to flex laterally;
wherein the third one of the outboard beams couples with a fuselage frame of the fuselage;
wherein the second intercostal is configured to transfer a vertical load to the second one of the outboard beams and the third one of the outboard beams, and to transfer a lateral load to the fuselage frame.

11. The aircraft of claim 10 wherein:
the second intercostal is coupled to the second one of the outboard beams via a swing link to flex laterally;
the swing link comprises a structural member having a first pinned connection with the second intercostal and a second pinned connection with the second one of the outboard beams; and
the second intercostal is coupled to the third one of the outboard beams via a pin.

12. The aircraft of claim 10 wherein:
the first intercostal includes a lower section to fixedly couple between the first one of the outboard beams and the second one of the outboard beams, and an upper section to fixedly couple between the first one of the outboard beams and the second one of the outboard beams separately from the lower section, and
a space between the lower section and the upper section of the first intercostal is configured to accommodate aircraft systems routing.

13. The aircraft of claim 10 wherein:
the web is flat underneath the box structure.

14. The aircraft of claim 10 wherein:
the pressure deck is vertically disposed between a cabin and a main wheel well of the aircraft, and
the arches of the web are configured to support pressure from the cabin that is disposed above the pressure deck.

15. A pressure deck of an aircraft, the pressure deck comprising:
beams extending longitudinally in the aircraft between a rear spar and an aft wheel well bulkhead of the aircraft, and spaced from one another in a lateral direction, wherein the beams include a middle pair of beams, and outboard beams spaced in the lateral direction from the middle pair of beams on a side of the pressure deck;
a web attached to an underside of the beams, the web including arches between adjacent beams to allow the pressure deck to flex laterally;
a box structure between the middle pair of the beams, and configured to transfer a load forward to the rear spar and aft to the aft wheel well bulkhead;
a tension strap coupled between one of the middle pair of the beams and a first one of the outboard beams in the lateral direction, wherein the tension strap is configured to support lateral force

Assignees

• Boeing Co

Inventors

• Leibov David H
• Ingham Steven D
• Cox Daniel
• Mclaughlin Mark R
• Menanno Alfons
• Paravata Soma Gopala Rao
• Sullivan Kevin L

Classifications

• B64C1/26

  Attaching the wing or tail units or stabilising surfaces · CPC title

• B64C1/061

  Frames · CPC title

• B64C1/20

  specially adapted for freight · CPC title

• B64C1/18 Primary

  Floors · CPC title

• B64C1/00 Primary

  Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like · CPC title