GB1487064A - Wall structure for hot fluid streams - Google Patents

Wall structure for hot fluid streams

Info

Publication number
GB1487064A
GB1487064A GB1901177A GB1901177A GB1487064A GB 1487064 A GB1487064 A GB 1487064A GB 1901177 A GB1901177 A GB 1901177A GB 1901177 A GB1901177 A GB 1901177A GB 1487064 A GB1487064 A GB 1487064A
Authority
GB
United Kingdom
Prior art keywords
hot fluid
wall structure
wall
fluid streams
gas turbine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB1901177A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB1901177A priority Critical patent/GB1487064A/en
Publication of GB1487064A publication Critical patent/GB1487064A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components

Abstract

1487064 Gas turbine combustion chambers ROLLS-ROYCE Ltd 23 Aug 1974 [17 Oct 1973] 19011/77 Divided out of 1487063 Heading F1L A wall structure for a hot fluid stream, e.g. for a gas turbine combustion chamber, comprises a metallic outer wall 110 lined with cube-shaped silicon nitride blocks 114 secured to the wall by projections 117 and spring clips 122. The latter define gaps (123), Fig. 3 (Not shown) for cooling air which then flows through holes 120 to grooves 124, 126 in the blocks. Clips 122 may be formed individually or in strips.
GB1901177A 1974-08-23 1974-08-23 Wall structure for hot fluid streams Expired GB1487064A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1901177A GB1487064A (en) 1974-08-23 1974-08-23 Wall structure for hot fluid streams

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1901177A GB1487064A (en) 1974-08-23 1974-08-23 Wall structure for hot fluid streams

Publications (1)

Publication Number Publication Date
GB1487064A true GB1487064A (en) 1977-09-28

Family

ID=10122273

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1901177A Expired GB1487064A (en) 1974-08-23 1974-08-23 Wall structure for hot fluid streams

Country Status (1)

Country Link
GB (1) GB1487064A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4471623A (en) * 1982-10-15 1984-09-18 The United States Of America As Represented By The Secretary Of The Air Force Combustion chamber floatwall panel attachment arrangement
US4512159A (en) * 1984-04-02 1985-04-23 United Technologies Corporation Clip attachment
EP0224817A1 (en) * 1985-12-02 1987-06-10 Siemens Aktiengesellschaft Heat shield arrangement, especially for the structural components of a gas turbine plant
US4748806A (en) * 1985-07-03 1988-06-07 United Technologies Corporation Attachment means
US4848089A (en) * 1988-02-18 1989-07-18 Avco Corporation Combustor attachment device
US5113660A (en) * 1990-06-27 1992-05-19 The United States Of America As Represented By The Secretary Of The Air Force High temperature combustor liner
US5331816A (en) * 1992-10-13 1994-07-26 United Technologies Corporation Gas turbine engine combustor fiber reinforced glass ceramic matrix liner with embedded refractory ceramic tiles
FR2714152A1 (en) * 1993-12-22 1995-06-23 Snecma Device for fixing a thermal protection tile in a combustion chamber.
WO2014163674A1 (en) * 2013-03-13 2014-10-09 Freeman Ted J Dovetail retention system for blade tracks
US9759082B2 (en) 2013-03-12 2017-09-12 Rolls-Royce Corporation Turbine blade track assembly

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4471623A (en) * 1982-10-15 1984-09-18 The United States Of America As Represented By The Secretary Of The Air Force Combustion chamber floatwall panel attachment arrangement
US4512159A (en) * 1984-04-02 1985-04-23 United Technologies Corporation Clip attachment
US4748806A (en) * 1985-07-03 1988-06-07 United Technologies Corporation Attachment means
EP0224817A1 (en) * 1985-12-02 1987-06-10 Siemens Aktiengesellschaft Heat shield arrangement, especially for the structural components of a gas turbine plant
US4749029A (en) * 1985-12-02 1988-06-07 Kraftwerk Union Aktiengesellschaft Heat sheild assembly, especially for structural parts of gas turbine systems
US4848089A (en) * 1988-02-18 1989-07-18 Avco Corporation Combustor attachment device
US5113660A (en) * 1990-06-27 1992-05-19 The United States Of America As Represented By The Secretary Of The Air Force High temperature combustor liner
US5331816A (en) * 1992-10-13 1994-07-26 United Technologies Corporation Gas turbine engine combustor fiber reinforced glass ceramic matrix liner with embedded refractory ceramic tiles
FR2714152A1 (en) * 1993-12-22 1995-06-23 Snecma Device for fixing a thermal protection tile in a combustion chamber.
US5501071A (en) * 1993-12-22 1996-03-26 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Fixing arrangement for a thermal protection tile in a combustion chamber
US9759082B2 (en) 2013-03-12 2017-09-12 Rolls-Royce Corporation Turbine blade track assembly
US10364693B2 (en) 2013-03-12 2019-07-30 Rolls-Royce Corporation Turbine blade track assembly
WO2014163674A1 (en) * 2013-03-13 2014-10-09 Freeman Ted J Dovetail retention system for blade tracks
US9458726B2 (en) 2013-03-13 2016-10-04 Rolls-Royce Corporation Dovetail retention system for blade tracks

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee