TR21832A - Bir soramik elemani bir metal yapiya tesbit etmeye mahsus cihaz - Google Patents

Bir soramik elemani bir metal yapiya tesbit etmeye mahsus cihaz

Info

Publication number
TR21832A
TR21832A TR21832A TR2183282A TR21832A TR 21832 A TR21832 A TR 21832A TR 21832 A TR21832 A TR 21832A TR 2183282 A TR2183282 A TR 2183282A TR 21832 A TR21832 A TR 21832A
Authority
TR
Turkey
Prior art keywords
soramic
determined
metal structure
metal
soramic element
Prior art date
Application number
TR21832A
Other languages
English (en)
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of TR21832A publication Critical patent/TR21832A/tr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous 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
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/04—Mounting of an exhaust cone in the jet pipe
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B13/00—Dowels or other devices fastened in walls or the like by inserting them in holes made therein for that purpose

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
TR21832A 1981-09-11 1982-05-05 Bir soramik elemani bir metal yapiya tesbit etmeye mahsus cihaz TR21832A (tr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/301,172 US4438626A (en) 1981-09-11 1981-09-11 Apparatus for attaching a ceramic member to a metal structure

Publications (1)

Publication Number Publication Date
TR21832A true TR21832A (tr) 1985-08-16

Family

ID=23162256

Family Applications (1)

Application Number Title Priority Date Filing Date
TR21832A TR21832A (tr) 1981-09-11 1982-05-05 Bir soramik elemani bir metal yapiya tesbit etmeye mahsus cihaz

Country Status (6)

Country Link
US (1) US4438626A (tr)
KR (1) KR880001500B1 (tr)
CA (1) CA1187679A (tr)
CH (1) CH660209A5 (tr)
GB (1) GB2107630B (tr)
TR (1) TR21832A (tr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
FR2587455B1 (fr) * 1985-09-18 1987-10-30 Snecma Procede de fabrication d'un anneau bruleur en materiau composite et anneau bruleur realise suivant ledit procede
US5592814A (en) * 1994-12-21 1997-01-14 United Technologies Corporation Attaching brittle composite structures in gas turbine engines for resiliently accommodating thermal expansion
DE19938443A1 (de) 1999-08-13 2001-02-15 Abb Alstom Power Ch Ag Befestigungs- und Fixierungsvorrichtung
US6351941B1 (en) * 2000-02-29 2002-03-05 General Electric Company Methods and apparatus for reducing thermal stresses in an augmentor
US7581399B2 (en) * 2006-01-05 2009-09-01 United Technologies Corporation Damped coil pin for attachment hanger hinge
US7874059B2 (en) * 2006-01-12 2011-01-25 Siemens Energy, Inc. Attachment for ceramic matrix composite component
US7814753B2 (en) * 2006-07-25 2010-10-19 United Technologies Corporation Low profile attachment hanger system for a cooling liner within a gas turbine engine swivel exhaust duct
US7975488B2 (en) * 2006-07-28 2011-07-12 United Technologies Corporation Low profile attachment hanger system for a cooling liner within a gas turbine engine swivel exhaust duct
US8061977B2 (en) 2007-07-03 2011-11-22 Siemens Energy, Inc. Ceramic matrix composite attachment apparatus and method
US8051664B2 (en) * 2007-07-23 2011-11-08 Pratt & Whitney Canada Corp. Pre-loaded internal fuel manifold support
US8211524B1 (en) 2008-04-24 2012-07-03 Siemens Energy, Inc. CMC anchor for attaching a ceramic thermal barrier to metal
WO2013163510A1 (en) 2012-04-27 2013-10-31 General Electric Company Connecting gas turbine engine annular members
US10330011B2 (en) * 2013-03-11 2019-06-25 United Technologies Corporation Bench aft sub-assembly for turbine exhaust case fairing
GB201700100D0 (en) * 2017-01-05 2017-02-22 Rolls Royce Plc A Mount assembly
CN115127126A (zh) * 2021-03-26 2022-09-30 中国航发商用航空发动机有限责任公司 环形燃烧室及分级燃油喷嘴和抑制振荡燃烧的方法

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2625788A (en) * 1948-12-15 1953-01-20 Mcdonnell Aircraft Corp Flame holder and fuel nozzle supporting mechanism for ram jet engines
US2799991A (en) * 1954-03-05 1957-07-23 Earl W Conrad Afterburner flame stabilization means
US3136202A (en) * 1962-06-04 1964-06-09 Arthur C Wagner Sheet metal expansion anchor having eccentric inturned edge
US3269116A (en) * 1965-04-29 1966-08-30 United Aircraft Corp Centrally supported flameholder
US3315468A (en) * 1965-10-01 1967-04-25 Gen Electric Cooled flameholder assembly
US3557402A (en) * 1968-12-04 1971-01-26 Cem Co Inc Coiled fastening pin
US3901622A (en) * 1973-05-31 1975-08-26 Gen Motors Corp Yieldable shroud support
CH632824A5 (de) * 1978-08-31 1982-10-29 Sulzer Ag Thermische isolation fuer rohre und verfahren zum herstellen einer solchen isolation.
DE2845716C2 (de) * 1978-10-20 1985-08-01 Volkswagenwerk Ag, 3180 Wolfsburg Thermisch hoch beanspruchbare Verbindung
US4312599A (en) * 1979-10-22 1982-01-26 General Electric Company High temperature article, article retainer, and cushion

Also Published As

Publication number Publication date
GB2107630B (en) 1985-10-02
GB2107630A (en) 1983-05-05
KR830010283A (ko) 1983-12-30
CA1187679A (en) 1985-05-28
CH660209A5 (de) 1987-03-31
US4438626A (en) 1984-03-27
KR880001500B1 (ko) 1988-08-16

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