FR967431A - Improvements to turbo-reactors - Google Patents

Improvements to turbo-reactors

Info

Publication number
FR967431A
FR967431A FR967431DA FR967431A FR 967431 A FR967431 A FR 967431A FR 967431D A FR967431D A FR 967431DA FR 967431 A FR967431 A FR 967431A
Authority
FR
France
Prior art keywords
turbo
reactors
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
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 Aeroplane Co Ltd
Original Assignee
Bristol Aeroplane Co 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
Application filed by Bristol Aeroplane Co Ltd filed Critical Bristol Aeroplane Co Ltd
Application granted granted Critical
Publication of FR967431A publication Critical patent/FR967431A/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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
FR967431D 1947-06-12 1948-06-08 Improvements to turbo-reactors Expired FR967431A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB967431X 1947-06-12

Publications (1)

Publication Number Publication Date
FR967431A true FR967431A (en) 1950-11-03

Family

ID=10805320

Family Applications (1)

Application Number Title Priority Date Filing Date
FR967431D Expired FR967431A (en) 1947-06-12 1948-06-08 Improvements to turbo-reactors

Country Status (1)

Country Link
FR (1) FR967431A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1055884B (en) * 1954-03-02 1959-04-23 Bristol Aero Engines Ltd Flame tube for a combustion chamber of a gas turbine engine
WO2003044329A1 (en) * 2001-11-20 2003-05-30 Alstom Technology Ltd Gas turbo group

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1055884B (en) * 1954-03-02 1959-04-23 Bristol Aero Engines Ltd Flame tube for a combustion chamber of a gas turbine engine
WO2003044329A1 (en) * 2001-11-20 2003-05-30 Alstom Technology Ltd Gas turbo group
US7013652B2 (en) 2001-11-20 2006-03-21 Alstom Technology Ltd Gas turbo set

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