FR2251706B1 - - Google Patents

Info

Publication number
FR2251706B1
FR2251706B1 FR7341289A FR7341289A FR2251706B1 FR 2251706 B1 FR2251706 B1 FR 2251706B1 FR 7341289 A FR7341289 A FR 7341289A FR 7341289 A FR7341289 A FR 7341289A FR 2251706 B1 FR2251706 B1 FR 2251706B1
Authority
FR
France
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
FR7341289A
Other languages
French (fr)
Other versions
FR2251706A1 (en
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.)
Avco Corp
Original Assignee
Avco Corp
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
Priority to GB5099673A priority Critical patent/GB1410137A/en
Application filed by Avco Corp filed Critical Avco Corp
Priority to FR7341289A priority patent/FR2251706B1/fr
Publication of FR2251706A1 publication Critical patent/FR2251706A1/fr
Application granted granted Critical
Publication of FR2251706B1 publication Critical patent/FR2251706B1/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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
    • F23R3/002—Wall structures
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54—Reverse-flow combustion chambers
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR7341289A 1973-11-02 1973-11-20 Expired FR2251706B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB5099673A GB1410137A (en) 1973-11-02 1973-11-02 Gas turbine engines
FR7341289A FR2251706B1 (en) 1973-11-02 1973-11-20

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB5099673A GB1410137A (en) 1973-11-02 1973-11-02 Gas turbine engines
FR7341289A FR2251706B1 (en) 1973-11-02 1973-11-20

Publications (2)

Publication Number Publication Date
FR2251706A1 FR2251706A1 (en) 1975-06-13
FR2251706B1 true FR2251706B1 (en) 1976-05-07

Family

ID=26218036

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7341289A Expired FR2251706B1 (en) 1973-11-02 1973-11-20

Country Status (2)

Country Link
FR (1) FR2251706B1 (en)
GB (1) GB1410137A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2219653B (en) * 1987-12-18 1991-12-11 Rolls Royce Plc Improvements in or relating to combustors for gas turbine engines
EP1426558A3 (en) * 2002-11-22 2005-02-09 General Electric Company Gas turbine transition piece with dimpled surface and cooling method for such a transition piece

Also Published As

Publication number Publication date
GB1410137A (en) 1975-10-15
FR2251706A1 (en) 1975-06-13

Similar Documents

Publication Publication Date Title
AR201758A1 (en)
AU476761B2 (en)
AR201235Q (en)
AR201231Q (en)
AU474593B2 (en)
AU474511B2 (en)
AU474838B2 (en)
AU465453B2 (en)
AU471343B2 (en)
AU465434B2 (en)
AU450229B2 (en)
AU476714B2 (en)
AR201229Q (en)
AU466283B2 (en)
AU476696B2 (en)
AU472848B2 (en)
AR199451A1 (en)
FR2251706A1 (en)
AU477823B2 (en)
AU477824B2 (en)
AU471461B2 (en)
AR200256A1 (en)
AR200885A1 (en)
AR201432A1 (en)
AU476873B1 (en)

Legal Events

Date Code Title Description
ST Notification of lapse