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

Resilient annular mounting member for a transition duct of a combustion chamber

Patent 5572863 Issued on November 12, 1996. Estimated Expiration Date: Icon_subject June 21, 2015. 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

2578481

2592060

2608057

2615300

2709338

Gas turbine engine having an improved transition duct support
Patent #: 4016718
Issued on: 04/12/1977
Inventor: Lauck

Combustor liner joints
Patent #: 4232527
Issued on: 11/11/1980
Inventor: Reider

Gas turbine engine
Patent #: 5085038
Issued on: 02/04/1992
Inventor: Todman, et al.

Combustion chamber assembly with hollow support strut for carrying cooling air
Patent #: 5353586
Issued on: 10/11/1994
Inventor: Taylor, et al.

Thermoelastic connection of the injector tube and the flame tube of a gas turbine
Patent #: 5419114
Issued on: 05/30/1995
Inventor: Bauermeister, et al.

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Inventors

Assignee

Application

No. 493141 filed on 06/21/1995

US Classes:

60/39.37, Plural combustion products generators in ring coaxial with turbine60/799Having expansible connection

Examiners

Primary: Thorpe, Timothy S.
Assistant: Kim, Ted

Attorney, Agent or Firm

Foreign Patent References

  • 2531328 DE 01/21/1977
  • 579416 GB 08/21/2013
  • 2087536 GB. 05/21/1982
  • 2247521 GB. 03/21/1992

International Class

F02C 003/00

Foreign Application Priority Data

1994-09-15 GB

Abstract

A combustion chamber assembly comprises a plurality of tubular combustion chambers which have their axes arranged generally radially. A transition duct is provided for each of the tubular combustion chambers. Each transition duct has a circular upstream end arranged coaxially with the downstream end of the respective tubular combustion chamber. An annular resilient member mounts the upstream end of the respective transition duct on a tubular portion of a respective support structure. The inner end of the annular member is formed integrally with the upstream end of the transition duct and the outer end of the annular member is secured to a flange on the tubular portion of the support structure by a bolted connection. The annular member has a plurality of circumferentially extending slots to allow thermally induced articulation and to maintain the upstream end of the transition duct coaxial with the support member.

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