Home | Links | Contact Us | More About Intellectual Property | Bookmark
Search patents:
Home Telecommunications Energy-absorbing-seat-arrangement

 Spread spectrum communications system
Accordingly, it is a general object of the present invention to provide an improved spread spectrum ...


 Spread spectrum pulse position modulation system
Accordingly, the present invention has been made in consideration of the above problems in the ...


 Sequential detection system and method with adaptive bias
This invention relates generally to cellular telephone communications, and more particularly to a ...


 Control systems for radar receivers
What is claimed is: 1. In a return echo ranging system, comprising: means for transmitting a ...


 Power factor correction system
Briefly, a power factor correction (PFC) system in accordance with the present invention is coupled ...


 Concentric ring antenna
To overcome the limitations of the prior art, a method and apparatus is provided to permit exciting ...


 Doppler frequency impulse radar system with displaced pulse sequence
I claim: 1. A doppler frequency impulse radar system, comprising a transmitting circuit for ...


 Method of screening infra-red radiation
I claim: 1. A method of screening infra-red radiation which comprises forming between the source of ...


 Electrical noise detector for detecting power line gap defects
In accordance with the present invention, a device for identifying a defect in power line equipment ...


 Test bench for wideband radio link
What we claim is: 1. A radio link test bench system, comprising: (1) transmission station means, ...


 Energy-absorbing seat arrangement

Details
Inventors: Martin, John S.;
Assignee: Engineering Patents and Equipment Limited (St. Peter, GB1)
Primary Examiner:
Assistant Examiner:
Attorney, Agent or Firm:

An energy absorbing seat arrangement, particularly for a helicopter, in which a seat pan is carried by a frame slidably mounted on parallel upwardly extending pillars secured to the helicopter. In normal conditions, downward sliding of the frame on the pillars is prevented, in one embodiment, by metal rods fixed with respect to the pillars, and extending through drawing dies fixed with respect to the seat frame. In a variant the rods and dies are replaced by a deformable metal tube and a mandrel extending through the tube. In the event of a crash in which rapid downward movement of the helicopter and the pillars is halted suddenly, the seat and seat frame continue to move downwardly, sliding along the pillars, while drawing of the rods through the dies, or drawing of the mandrel through the deformable tube, to dissipate the kinetic energy of the seat and its occupant relatively gradually.

DETAILED DESCRIPTION It is an object of the present invention to provide such an energy-absorbing seat arrangement which is simple and reliable in operation and which will not present a hazard in normal use.
According to the present invention there is provided an energy-absorbing seat arrangement including a first structure, including a seat pan, and a second structure adapted for fixing to an aircraft, vehicle or the like, said first structure being connected with said second structure by means including at least one deformable metal member arranged to undergo controlled, predetermined plastic deformation, in the event of the force acting between said first and second structure in at least one predetermined direction exceeding a predetermined value, in such a way as to allow controlled, energy-absorbing movement to take place between said structure under the action of said force.
In one embodiment of the invention, deformable metal members are provided in the form of elongate bolts which are drawn through dies under tension arising from impact or inertial forces in a crash situation, the drawing of said bolts through the dies serving to absorb the energy of the impact relatively gradually.
In another embodiment of the invention the bolts and dies are replaced by mandrels which are drawn through respective deformable tubular members to expand the same in the event of a crash.



Related patents
  Thin profile integrated suspension and seat trim cover
The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows: 1. A seat assembly, such as a vehicle seat assembly, ...
  Railway car retarder system
The invention provides for a railway car retarder mechanism that employs linear electromagnetic induction to precisely accelerate or decelerate a railcar. The retarder ...
  Homocopter
The Homocopter looks like a combination between a monocycle and a helicopter, being a small and very light vehicle, enableing one to fly, rotating its rotary wing (a ...
  Servo control system for a co-axial rotary winged aircraft
We claim: 1. A servo control system for a co-axial rotary winged aircraft having an upper and lower rotor comprising: command means for providing electronic command ...
  Coaxial transmission/center hub subassembly for a rotor assembly having ducted, coaxial counter-rotating rotors
One object of the present invention is to provide a coaxial transmission/center hub subassembly for a rotor assembly having ducted, coaxial counter-rotating rotors that ...
  Gas bag inflators
An object of the invention is to provide a simple and effective solution to the foregoing problem. Another object of the invention is to provide an improvement for a ...
  Arrangement for an airbag gas generator
The invention relates to an arrangement for a gas generator of a motor vehicle occupant protection system, the primary charge of which is arranged in a housing which has ...
  Vented gas passenger side air bag inflator
An object of the invention is to provide an improved solid fuel inflator assembly for air bag restraint systems used on the passenger side of automotive vehicles. A...
  Sensor for vehicle seat belt systems
What is claimed is: 1. A sensor for vehicle seat belt systems comprising a casing, an inertia body having at least a portion received in the casing for displacement ...
  Plastic air bag cover having an integrated light source
An object of the present invention is to provide an air bag cover having a light source module incorporated therein to project an information-bearing image within a ...

0.014

Archive: All patents - Links

Copyright (c)2006 Eipa-patents.org - All rights reserved