Title:
【発明の名称】エネルギ吸収リンク部材及びこれを具えた航空機用シート
Document Type and Number:
Japanese Patent JP3014963
Kind Code:
B2
Abstract:
An energy-absorbing bolt specially designed for an aircraft seat. It comprises an outer sleeve terminated at a first end by fastening means for fastening to a first structural element; an inner sleeve terminated at an opposite, second end by a rod suitable for being rigidly associated with a second structural element; the two sleeves being fitted one in the other in such a manner as to enable one to slide axially relative to the other in the event of the bolt being subjected to energy exceeding a certain threshold; a first pin constituting a fuse relative to the trigger threshold being mounted transversely in holes and being held in position by a locking member; a second pin also being mounted transversely so as to project at at least one of its ends from the inner sleeve in a complementary housing, and having, during axial sliding in the moving-apart direction, a first function of deforming the outer sleeve to absorb energy, and a second function of providing an end-of-stroke stop by co-operating with an inside projection of the outer sleeve.
Inventors:
Fabry Sheep Pinole
Application Number:
JP13915196A
Publication Date:
February 28, 2000
Filing Date:
May 31, 1996
Export Citation:
Assignee:
Societe Andre Striere Commercial de Materiel Aeronotique (Societe Anonymous)
International Classes:
B64D25/04; B64D11/06; F16F7/12; (IPC1-7): B64D25/04
Domestic Patent References:
| JP444903Y2 | ||||
| JP4628332Y1 |
Other References:
【文献】米国特許3538785(US,A)
【文献】米国特許5454622(US,A)
【文献】米国特許5454622(US,A)
Attorney, Agent or Firm:
Takashi Ishida (3 others)