DE69102548D1 - Befestigungsvorrichtung. - Google Patents

Befestigungsvorrichtung.

Info

Publication number
DE69102548D1
DE69102548D1 DE69102548T DE69102548T DE69102548D1 DE 69102548 D1 DE69102548 D1 DE 69102548D1 DE 69102548 T DE69102548 T DE 69102548T DE 69102548 T DE69102548 T DE 69102548T DE 69102548 D1 DE69102548 D1 DE 69102548D1
Authority
DE
Germany
Prior art keywords
fastening device
fastening
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 - Fee Related
Application number
DE69102548T
Other languages
English (en)
Other versions
DE69102548T2 (de
Inventor
Martyn Grigson Roberts
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
Application granted granted Critical
Publication of DE69102548D1 publication Critical patent/DE69102548D1/de
Publication of DE69102548T2 publication Critical patent/DE69102548T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Connection Of Plates (AREA)
DE69102548T 1990-01-29 1991-01-23 Befestigungsvorrichtung. Expired - Fee Related DE69102548T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/471,634 US5103638A (en) 1990-01-29 1990-01-29 Mounting arrangement

Publications (2)

Publication Number Publication Date
DE69102548D1 true DE69102548D1 (de) 1994-07-28
DE69102548T2 DE69102548T2 (de) 1995-02-09

Family

ID=23872415

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69102548T Expired - Fee Related DE69102548T2 (de) 1990-01-29 1991-01-23 Befestigungsvorrichtung.

Country Status (3)

Country Link
US (1) US5103638A (de)
EP (1) EP0440366B1 (de)
DE (1) DE69102548T2 (de)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5313780A (en) * 1992-12-07 1994-05-24 General Electric Company Free-riding oil tube damper
US5265409A (en) * 1992-12-18 1993-11-30 United Technologies Corporation Uniform cooling film replenishment thermal liner assembly
FR2865502B1 (fr) * 2004-01-23 2006-03-03 Snecma Moteurs Bras monobloc accroche-flammes pour un dispositif de post combustion d'un turboreacteur a double flux
US7584621B2 (en) * 2005-08-05 2009-09-08 Siemens Energy, Inc. Radially expanding turbine engine exhaust cylinder interface
US8572986B2 (en) * 2009-07-27 2013-11-05 United Technologies Corporation Retainer for suspended thermal protection elements in a gas turbine engine
US10563868B2 (en) * 2017-05-08 2020-02-18 General Electric Company Coupling method and structure for a propulsion system hot section

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2876891A (en) * 1953-01-26 1959-03-10 Gen Mills Inc Vibratory apparatus
GB980372A (en) * 1962-03-20 1965-01-13 Daimler Benz Ag Improvements relating to spring arrangements
US3295325A (en) * 1965-04-29 1967-01-03 United Aircraft Corp Jet engine afterburner flameholder
US3646763A (en) * 1970-05-25 1972-03-07 Gen Electric Gas turbine engine with improved afterburner
US4064691A (en) * 1975-11-04 1977-12-27 General Electric Company Cooling of fastener means for a removable flameholder
FR2551500B1 (fr) * 1983-09-07 1985-11-08 Snecma Anneau-bruleur pour postcombustion de moteur a reaction
FR2586792B1 (fr) * 1985-09-03 1989-06-16 Snecma Dispositif de liaison entre un anneau bruleur ou accroche-flammes en materiau composite et un canal de chambre de post-combustion d'un turboreacteur
FR2623249A1 (fr) * 1987-11-12 1989-05-19 Snecma Ensemble constitue de deux pieces en materiaux ayant des coefficients de dilatation differents, reliees entre elles et methode d'assemblage
FR2626044A1 (fr) * 1988-01-14 1989-07-21 Snecma Melangeur de flux a section variable avec stabilisateur de rechauffe integre pour turboreacteur double flux
US4901527A (en) * 1988-02-18 1990-02-20 General Electric Company Low turbulence flame holder mount

Also Published As

Publication number Publication date
US5103638A (en) 1992-04-14
EP0440366A1 (de) 1991-08-07
EP0440366B1 (de) 1994-06-22
DE69102548T2 (de) 1995-02-09

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee