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

Improvements in or relating to gas turbine engines

Patent 4716721 Issued on January 5, 1988. Estimated Expiration Date: Icon_subject November 13, 2005. 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

3620012

3775975

3861139

3908361

Integral infrared radiation suppressor for a turbofan engine
Patent #: 4271666
Issued on: 06/09/1981
Inventor: Hurley ,   et al.

Rotary pressure seal structure and method for reducing thermal stresses therein
Patent #: 4397471
Issued on: 08/09/1983
Inventor: Feldman ,   et al.

Casing structure for a gas turbine engine Patent #: 4502276
Issued on: 03/05/1985
Inventor: Pask

Inventors

Assignee

Application

No. 06/797805 filed on 11/13/1985

US Classes:

60/796, Having mounting or supporting structure415/199.4, Including an axial-flow blade set415/213.1, Casing with mounting means415/220Casing with axial flow runner

Examiners

Primary: Casaregola, Louis J.
Assistant: Stout, Donald E.

Attorney, Agent or Firm

International Classes

F01D 25/26 (20060101)
F01D 25/24 (20060101)
F02C 7/20 (20060101)

Foreign Application Priority Data

1984-12-08 GB

Abstract

The casings of gas turbine engines are subject to loadings which distort the casing and adversely affect the running clearance between rotating and static components contained within the casings. The invention provides an engine having inner and outer housings the inner housing containing one of the engine compressors. The inner casing is mounted on a load transmitting and isolating structure which allows thrust and torque to be transmitted to the outer casing, but isolates the inner casing from distortions of the outer casing. The load transmitting and isolating structure includes a torque reaction and mounting means at the upstream end of the inner casing, a mounting means and a thrust reacting means mounted between the ends of the inner casing. The mounting means are adjacent the bearings of the rotor shaft of the compressor and are not affected to any appreciable extent by outer casing distortion. The thrust reacting means are mounted in a horizontal plane and are not affected by bending of the outer casing in a vertical plane.

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?