Seat belt arrangement and seat assembly incorporating same

Patent metadata

Field	Value
Publication number	US-10279914-B2
Application number	US-201514685042-A
Country	US
Kind code	B2
Filing date	Apr 13, 2015
Priority date	Apr 15, 2014
Publication date	May 7, 2019
Grant date	May 7, 2019

Abstract

A seat belt arrangement for a seat assembly of an aircraft for securing a passenger in a seat during travel. The seat belt arrangement comprises: a seat belt including at least a first belt portion to extend across a body part of the passenger seated on the seat; and a fastener member provided on the first belt portion, especially at a first end region of the first belt portion, for operation by the passenger to fasten and to release the seat belt across the body part of the passenger. A second end region of the first belt portion is anchored at a footing of the seat assembly or at a floor structure of the aircraft directly.

First claim

The invention claimed is:

1. A seat belt arrangement for a seat assembly of an aircraft for securing a passenger in a seat during travel, the seat assembly including a frame upon which the seat is supported, the frame having leas and one or more footings which are arranged between the legs and a floor structure of the aircraft and which contact and attach to the floor structure, the seat belt arrangement comprising:
a seat belt including at least a first belt portion for extending across a body part of the passenger seated on the seat; and
a fastener member provided on the first belt portion for operation by the passenger to fasten and to release the seat belt across the body part of the passenger;
wherein a second end region of the first belt portion is anchored to a footing of the seat assembly or directly to the floor structure of the aircraft.

2. The seat belt arrangement according to claim 1 , wherein the second end region of the first belt portion extends to the floor structure of the aircraft or to the footing of the seat assembly in contact with the floor structure.

3. The seat belt arrangement according to claim 1 , wherein the second end region of the first belt portion includes an attachment member with which the seat belt is securely fixed or anchored to the footing of the seat assembly or to the floor structure of the aircraft.

4. The seat belt arrangement according to claim 1 , wherein the fastener member provided on the first belt portion is configured to cooperate with a complementary fastener member for fastening and releasing the first belt portion across the body part of the passenger seated on the seat.

5. The seat belt arrangement according to claim 4 , wherein the seat belt includes a second belt portion which cooperates with the first belt portion for extending across a body part of the passenger seated on the seat, the complementary fastener member being provided on the second belt portion, and wherein a second end region of the second belt portion is anchored at a footing of the seat assembly or at a floor structure of the aircraft directly.

6. The seat belt arrangement according to claim 5 , wherein the second end region of the second belt portion extends to the footing of the seat assembly or to the floor structure of the aircraft.

7. The seat belt arrangement according to claim 5 , wherein the second end region of the second belt portion comprises an attachment member with which the seat belt is securely fixed or anchored to the footing of the seat assembly or to the floor structure, especially to a seat rail, of the aircraft.

8. An aircraft seat assembly for mounting on a floor structure of an aircraft, comprising:
at least one seat configured to accommodate and support a passenger during travel;
a frame upon which the at least one seat is mounted and supported, the frame including legs and one or more footings arranged between the frame and a floor structure of the aircraft and configured for engagement with and attachment to the floor structure; and
a seat belt respectively associated with each seat and configured to extend across a body part of the passenger seated on the seat, the seat belt including at least a first belt portion and a fastener member provided on the first belt portion for operation by the passenger to fasten and to release the seat belt across the body part of the passenger,
wherein a second end region of the first belt portion is anchored to the footing or directly to the floor structure of the aircraft.

9. The seat assembly according to claim 8 , wherein the second end region of the first belt portion extends to the floor structure of the aircraft or to the footing of the frame contacting the floor structure.

10. The seat assembly according to claim 9 , wherein the seat belt includes a second belt portion which cooperates with the first belt portion to extend across a body part of the passenger seated on the seat, wherein a complementary fastener member is provided on the second belt portion to cooperate with the fastener member for fastening and releasing the seat belt across the body part of the passenger seated on the seat, and wherein a second end region of the second belt portion is anchored at the footing of the frame or at the floor structure of the aircraft directly.

11. The seat assembly according to claim 10 , wherein the second end region of the second belt portion extends to the footing or the floor structure.

12. An aircraft including at least one aircraft seat assembly for mounting on a floor structure of the aircraft, the aircraft seat assembly comprising:
at least one seat configured to accommodate and support a passenger during travel;
a frame upon which the at least one seat is mounted and supported, the frame including leas and one or more footings arranged between the frame and a floor structure of the aircraft and configured for engagement with and attachment to the floor structure; and
a seat belt respectively associated with each seat and configured to extend across a body part of the passenger seated on the seat, the seat belt including at least a first belt portion and a fastener member provided on the first belt portion, especially at a first end region of the first belt portion, for operation by the passenger to fasten and to release the seat belt across the body part of the passenger,
wherein a second end region of the first belt portion is anchored to the footing or directly to the floor structure of the aircraft.

13. The seat belt arrangement according to claim 1 , wherein the fastener member is provided at a first end region of the first belt portion.

14. The seat assembly according to claim 8 , wherein the fastener member is provided at a first end region of the first belt portion.

15. The seat belt arrangement according to claim 3 , wherein the attachment member securely fixes or anchors the seat belt to a seat rail in the floor structure.

16. The seat assembly according to claim 9 , wherein the attachment member securely fixes or anchors the seat belt to a seat rail in the floor structure.

17. The seat belt arrangement according to claim 7 , wherein the attachment member of the second end region of the second belt portion securely fixes or anchors the seat belt to a seat rail of the aircraft.

18. The seat assembly according to claim 11 , wherein the attachment member of the second end region of the second belt portion securely fixes or anchors the seat belt to a seat rail of the aircraft.

19. The seat assembly according to claim 8 , wherein the second end region of the first belt portion includes an attachment member with which the seat belt is securely fixed or anchored to the footing of the frame or to the floor structure of the aircraft.

20. The seat assembly according to claim 10 , wherein the second end region of the second belt portion comprises an attachment member with which the seat belt is securely fixed or anchored to the footing or to the floor structure.

Assignees

• Airbus Operations Gmbh

Inventors

• Fragnière Benjamin

Classifications

• B64D11/062 Primary

  Belts or other passenger restraint means for passenger seats · CPC title

• B64D11/0649

  Seats characterised by special features for reducing weight · CPC title

• Y02T50/46

  Cross-Sectional Technologies · mapped topic

• Y02T50/40

  Weight reduction · CPC title