FR1388342A - Improvements to the combustion systems of aircraft engines comprising a gas turbine - Google Patents

Improvements to the combustion systems of aircraft engines comprising a gas turbine

Info

Publication number
FR1388342A
FR1388342A FR968131A FR968131A FR1388342A FR 1388342 A FR1388342 A FR 1388342A FR 968131 A FR968131 A FR 968131A FR 968131 A FR968131 A FR 968131A FR 1388342 A FR1388342 A FR 1388342A
Authority
FR
France
Prior art keywords
gas turbine
aircraft engines
combustion systems
combustion
systems
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
FR968131A
Other languages
French (fr)
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.)
Bristol Siddeley Engines Ltd
Original Assignee
Bristol Siddeley Engines Ltd
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 claimed from GB1416963A external-priority patent/GB1044674A/en
Application filed by Bristol Siddeley Engines Ltd filed Critical Bristol Siddeley Engines Ltd
Priority to FR968131A priority Critical patent/FR1388342A/en
Application granted granted Critical
Publication of FR1388342A publication Critical patent/FR1388342A/en
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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
FR968131A 1963-04-01 1964-03-20 Improvements to the combustion systems of aircraft engines comprising a gas turbine Expired FR1388342A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR968131A FR1388342A (en) 1963-04-01 1964-03-20 Improvements to the combustion systems of aircraft engines comprising a gas turbine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1416963A GB1044674A (en) 1963-04-01 1963-04-01 Improvements in combustion systems for gas turbine engines
FR968131A FR1388342A (en) 1963-04-01 1964-03-20 Improvements to the combustion systems of aircraft engines comprising a gas turbine

Publications (1)

Publication Number Publication Date
FR1388342A true FR1388342A (en) 1965-02-05

Family

ID=26206568

Family Applications (1)

Application Number Title Priority Date Filing Date
FR968131A Expired FR1388342A (en) 1963-04-01 1964-03-20 Improvements to the combustion systems of aircraft engines comprising a gas turbine

Country Status (1)

Country Link
FR (1) FR1388342A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2319018A1 (en) * 1975-07-21 1977-02-18 United Technologies Corp GAS TURBOMACHINE WITH IMPROVED SUPPORT FOR TRANSITION DUCTS

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2319018A1 (en) * 1975-07-21 1977-02-18 United Technologies Corp GAS TURBOMACHINE WITH IMPROVED SUPPORT FOR TRANSITION DUCTS

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