Hybrid composite-metal energy absorbing seat

• US 6,896,324 B1
• Filed: 04/21/2003
• Issued: 05/24/2005
• Est. Priority Date: 04/19/2002
• Status: Expired due to Fees

• Current Assignee: Triton Aerospace, LLC
• Original Assignee: Adam Aircraft Industries
• Inventors: Olcott, Dennis D., Wilson, Sharon M., Kull, Matthew H.
• Primary Examiner(s): WHITE, RODNEY BARNETT
• Application Number:
  US10/420,566
• Time in Patent Office: 764 Days
• Field of Search: 297/452.18, 297/452.19, 297/452.55, 297/216.1, 297/216.13
• 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. A hybrid composite-metal energy absorbing aircraft seat comprising:

a seat base assembly comprising a plurality of rigid metal seat base side frame elements joined by a seat pan formed of sheet metal and a molded composite seat cover, the plurality of rigid metal seat base side frame elements to absorb forward crash load energy by permanently deforming during a severe forward crash load, the seat pan configured to hold a lightweight energy absorber for absorbing downloads, the molded composite seat cover having sides extending across the plurality of seat base side frame elements to also provide energy absorption capability in a download;

a seat back assembly attached to the seat base assembly, the seat back assembly comprising a plurality of rigid metal seat back side frame elements joined together with a plurality of composite molded shells, including an outer shell and an inner shell between which a shoulder belt harness system is housed and anchored to the plurality of rigid metal seat back side frame elements to transfer shoulder belt crash loads to the plurality of rigid metal seat back side fame elements and down into the plurality of rigid metal seat base side frame elements causing the plurality of rigid metal seat base side frame elements and the plurality of seat back side frame elements to deform and dissipate a portion of forces acting upon the seat; and

wherein the molded composite seat cover sides 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.

2. The seat of claim 1, 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.

3. The seat of claim 1, wherein the rigid metal seat back 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 back side frame elements while maintaining strength of the rigid metal seat back side frame elements.

4. The seat of claim 1, wherein the lightweight energy absorber comprises a block of aluminum honeycomb.

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

6. The seat of claim 4, wherein the honeycomb openings of the block of aluminum honeycomb are aligned such that they form a plane approximately parallel to a seating surface.

7. The seat of claim 5, wherein the sidewall is a first sidewall attached to a, and wherein the first sidewall is attached to a first side of the block of aluminum honeycomb, and wherein a second sidewall is attached to an opposing side of the aluminum honeycombed material.

8. The seat of claim 4, wherein the block of aluminum honeycomb is designed for inelastic deformation upon application of a particular force.

9. The seat of claim 1, wherein the lightweight energy absorber comprises a block of energy absorbing aluminum honeycomb.

10. The seat of claim 9, wherein the block of energy absorbing aluminum honeycomb is designed for inelastic deformation upon application of a particular force.

11. The seat of claim 1, wherein the lightweight energy absorber comprises a block of honeycomb comprising one or more of Nomex™

material, carbon, Kevlar™

material, and paper.

12. The seat of claim 1, wherein the lightweight energy absorber comprises a block of open or closed-cell foam.

13. The seat of claim 1, wherein the lightweight energy absorber comprises a block of viscoelastic materials.

14. The seat of claim 1, 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 in a download.

15. The seat of claim 1, wherein the molded composite seat cover is not fastened to the plurality of rigid metal seat base side frame elements.

16. The seat of claim 1, wherein the plurality of rigid metal seat base side frame elements, the seat pan, and the molded composite seat cover are combined into a single integrated composite component manufactured using a process selected from a group consisting of:

wet layup, prepreg, RTM, and VARTM.

17. The seat of claim 1, wherein the rigid metal seat back side frame elements and the plurality of composite molded shells are combined into a single integrated composite component manufactured using a process selected from a group consisting of:

wet layup, prepreg, RTM, and VARTM.

18. The seat of claim 1, wherein the plurality of rigid metal seat back side frame elements are joined by a contoured composite seat back, and wherein 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.

19. The seat of claim 18, wherein the contoured composite seat back provides design/aesthetic flexibility.

20. The seat of claim 1, wherein the rigid metal seat back side frame elements absorb forward crash load energy by permanently deforming during a crash.

21. The seat of claim 1, wherein the molded composite seat cover sides are designed to inelastically deform upon application of a particular force.