U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Aircraft with a detachable passenger escape cabin and an aircraft with airbags

Patent 6682017 Issued on January 27, 2004. Estimated Expiration Date: Icon_subject September 9, 2022. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

Aircraft breakaway cabin section
Patent #: 4143841
Issued on: 03/13/1979
Inventor: Roeder

Latch bolt locking mechanism for fire door locksets
Patent #: 4183565
Issued on: 01/15/1980
Inventor: Allemann

Aircraft with jettisonable fuel tank means
Patent #: 4306693
Issued on: 12/22/1981
Inventor: Cooper

Airplane safety body passenger compartment
Patent #: 4699336
Issued on: 10/13/1987
Inventor: Diamond

Segmented safety aircraft
Patent #: 5356097
Issued on: 10/18/1994
Inventor: Chalupa

Plane saddle for a safety airplane
Patent #: 5568903
Issued on: 10/29/1996
Inventor: Pena, et al.

Emergency landing auxiliary apparatus for an aircraft using a parachute Patent #: 5810293
Issued on: 09/22/1998
Inventor: Leeki-Woo

Inventor

Application

No. 10/220977 filed on 09/09/2002

US Classes:

244/140, Passenger compartment244/138R, SAFETY LOWERING DEVICES70/275Using a powered device (e.g., motor)

Examiners

Primary: Dinh, Tan

International Classes

B64C 1/00 (20060101)
B64C 1/32 (20060101)
B64D 17/00 (20060101)
B64D 25/00 (20060101)
B64D 17/80 (20060101)
B64D 25/12 (20060101)

Abstract

An aircraft with a detachable cabin (1) that serves to rescue its passengers as a result of the aircraft's sudden fall either due to its malfunction or fire. The cabin escapes either smoothly or by means of fast ejection and descends slowly to the Earth with the aid of a parachute (13, 14); during a crash on the ground or in the sea external airbags (38a-38f) with which it is equipped and which are located in its lower part are inflated thus absorbing the loads that are developed during the crash. In addition a conventional aircraft (70) of the type being already in use is also described and in which the parachute equipment (71) has already been applied; however, the proposed equipment of the airbag boxes (72a-72c) is adapted to it for the absorption of the energy produced due to its crash on Earth in case of its sudden fall.

PatentsPlus Images
Enhanced PDF formats
loading...
PatentsPlus: add to cart
PatentsPlus: add to cartSearch-enhanced full patent PDF image
$9.95more info
PatentsPlus: add to cart
PatentsPlus: add to cartIntelligent turbocharged patent PDFs with marked up images
$16.95more info
 
Sign InRegister
Username  
Password   
forgot password?