Hybrid composite-metal energy absorbing seat

• US 7,083,230 B2
• Filed: 03/03/2005
• Issued: 08/01/2006
• Est. Priority Date: 04/19/2002
• Status: Expired due to Fees

• Current Assignee: Triton Aerospace, LLC
• Original Assignee: Adam Aircraft Industries
• Inventors: Wilson, Sharon M., Kull, Matthew H., Olcott, Dennis D.
• Primary Examiner(s): WHITE, RODNEY BARNETT
• Application Number:
  US11/072,904
• Publication Number:
  US 20050145597A1
• Time in Patent Office: 516 Days
• Field of Search: 297/216.1, 297/216.13, 297/452.18, 297/452.19, 297/452.2, 297/452.55
• US Class Current: 297/216.1
• CPC Class Codes: B60N 2/4242 vertical
• CPC Class Codes: B60N 2/42709 involving residual deformation or fracture of the structure
• CPC Class Codes: B64D 11/0689 specially adapted for pilots
• CPC Class Codes: B64D 25/04 Seat modifications
• CPC Class Codes: B64D 25/10 Ejector seats
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

A hybrid composite-metal energy absorbing seat is described. According to one embodiment, an aircraft seat includes a seat base assembly and a seat back assembly. The seat base assembly includes multiple rigid metal seat base side frame elements joined by a lower seat pan, an energy absorbing element placed on the lower seat pan to deform and absorb downward energy in a crash, and a contoured seat pan whose sides extend past the seat base side frame elements and deform to absorb downward energy in a crash. The seat back assembly is attached to the seat base assembly and includes multiple rigid metal seat back side frame elements joined by a contoured composite seat back. The rigid metal seat back side frame elements absorb forward crash load energy by permanently deforming during a severe forward crash load. The contoured composite seat back provides design/aesthetic flexibility.

Claims

1. An energy absorbent seat comprising:

a seat base assembly, wherein the seat base assembly includes a plurality of rigid seat base side frame elements joined by a seat pan assembly, wherein at least one of the plurality of seat base side frame elements is designed to absorb forward crash energy through inelastic deformation, and wherein the seat pan assembly is designed to absorb downward crash energy through inelastic deformation; and

a seat back assembly attached to the seat base assembly, wherein the seat back assembly includes a plurality of rigid seat back side frame elements joined by a seat back, wherein at least one of the plurality of rigid seat back side frame elements is designed to absorb forward crash energy through inelastic deformation.

2. The seat of claim 1, wherein the seat pan assembly includes a block of honeycombed material, and wherein the block of honeycombed material is capable of absorbing energy by inelastic deformation.

3. The seat of claim 2, wherein the block of honeycombed material is aluminum.

4. The seat of claim 3, wherein at least one side of the block of aluminum honeycombed material is bonded to a sidewall.

5. The seat of claim 2, wherein the honeycomb openings of the block of honeycomb material are aligned such that they form a plane approximately parallel to a seating surface.

6. An aircraft seat, wherein the aircraft seat comprises:

a seat base assembly designed to absorb both forward energy and downward energy of the magnitude exhibited in an aircraft crash; and

a seat back assembly attached to the seat base assembly, wherein the seat back assembly is designed to absorb forward energy of the magnitude exhibited in an aircraft crash.

7. The aircraft seat of claim 6, wherein the seat base assembly is designed to permanently deform when exposed to at least one of the forward energy and the downward energy, and wherein the deformation absorbs energy.

8. The aircraft seat of claim 7, wherein the seat base assembly includes a block of honeycomb aluminum material.

9. The aircraft seat of claim 6, wherein the seat back assembly is designed to permanently deform when exposed to the forward energy, and wherein the deformation absorbs energy.

10. The aircraft seat of claim 6, wherein a first sidewall is attached to a first side of the block of honeycomb aluminum material, and wherein a second sidewall is attached to an opposing side of the honeycomb aluminum material.

11. The aircraft seat of claim 6, wherein the first sidewall covers honeycomb openings in the aluminum honeycombed material.

12. A hybrid composite-metal energy absorbing seat comprising:

a seat base assembly, wherein the seat base assembly includes a plurality of rigid metal seat base side frame elements joined by a seat pan assembly, and wherein the plurality of rigid metal seat base side frame elements are designed to absorb forward crash energy by permanently deforming and; and

a seat back assembly attached to the seat base assembly, wherein the seat back assembly includes a plurality of rigid metal seat back side frame elements jointed by a contoured composite seat back, the plurality of rigid metal seat back side frame elements to absorb forward crash load energy by permanently deforming during a severe forward crash load, the contoured composite seat back providing design/aesthetic flexibility.

13. The seat of claim 12, wherein the seat pan assembly is designed to permanently deform when exposed to a downward crash energy.

14. The seat of claim 13, wherein the seat pan assembly includes a seat pan and a block of energy absorbing material.

15. The seat of claim 14, wherein the block of energy absorbing material is a block of honeycombed material.

16. The seat of claim 15, wherein the block of honeycombed material is selected from a group consisting of:

aluminum, paper, carbon, Nomex™

, and Kevlar™

.

17. The seat of claim 12, wherein the rigid metal seat base side frame elements comprise trusses or webbed trusses having formed therein a plurality of recesses having stable shapes to reduce the weight of the rigid metal seat base side frame elements while maintaining strength of the rigid metal seat base side frame elements.

18. The seat of claim 12, wherein the rigid metal seat back side frame elements comprise webbed trusses having formed therein a plurality of recesses having stable shapes to reduce the weight of the rigid metal seat back side frame elements while maintaining strength of the rigid metal seat back side frame elements.

19. The seat of claim 12, wherein the seat pan assembly includes a molded composite seat cover having sides extending across the plurality of rigid metal seat base side frame elements to provide energy absorption capability in a download by deforming up and over the plurality of rigid metal seat base side frame elements and allowing a center portion of the molded composite seat cover to deflect downwards.

20. The seat of claim 19, wherein the molded composite seat cover is lightly fastened by fasteners to the plurality of rigid metal seat base side frame elements with the fasteners shearing out when exposed to a downward crash energy.

21. The seat of claim 19, wherein the molded composite seat cover is not fastened to the plurality of rigid metal seat base side frame elements.

22. An aircraft seat comprising:

a seat base assembly including at least two rigid metal seat base side frame elements joined by a seat pan assembly, wherein the seat base assembly is designed to permanently deform in a severe aircraft crash; and

a seat back assembly attached to the seat base assembly.

23. The aircraft seat of claim 22, wherein the seat pan assembly includes a molded composite seat cover having sides extending across the plurality of rigid metal seat base side frame elements to provide energy absorption capability in a download by deforming up and over the plurality of rigid metal seat base side frame elements and allowing a center portion of the molded composite seat cover to deflect downwards.

24. The aircraft seat of claim 22, wherein the seat pan assembly includes a block of honeycombed material, wherein the block of honeycombed material is capable of absorbing energy by inelastic deformation.

25. The aircraft seat of claim 24, wherein the block of honeycombed material is aluminum.

26. The aircraft seat of claim 25, wherein at least one side of the block of aluminum honeycombed material is bonded to a sidewall.

27. The aircraft seat of claim 24, wherein the honeycomb openings of the block of honeycomb material are aligned such that they form a plane approximately parallel to a seating surface.

28. The aircraft seat of claim 22, wherein the seat pan assembly includes a download energy absorber comprising a block of honeycomb comprising one or more of Nomex™

material, carbon, Kevlar™

material, and paper.

29. The aircraft seat of claim 22, wherein the seat base assembly is further designed to permanently deform to absorb a forward crash load energy associated with an aircraft crash.

30. The aircraft seat of claim 22, wherein the seat back assembly comprises a plurality of rigid metal seat back side frame elements joined by a contoured composite seat back, the plurality of rigid metal seat back side frame elements to absorb forward crash load energy by permanently deforming during an aircraft crash.

31. A seat assembly comprising:

a seat base energy absorber, wherein the seat base energy absorber includes a block of honeycombed material, wherein the block of honeycombed material is designed to inelastically deform in an aircraft crash; and

wherein a sidewall is attached to a side of the block of honeycombed material.