GB1454206A - Continuous combustion device - Google Patents

Continuous combustion device

Info

Publication number
GB1454206A
GB1454206A GB3402274A GB3402274A GB1454206A GB 1454206 A GB1454206 A GB 1454206A GB 3402274 A GB3402274 A GB 3402274A GB 3402274 A GB3402274 A GB 3402274A GB 1454206 A GB1454206 A GB 1454206A
Authority
GB
United Kingdom
Prior art keywords
combustion device
continuous combustion
baffle
canada
heading
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
GB3402274A
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.)
Pratt and Whitney Canada Corp
Original Assignee
United Aircraft of Canada 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 US05/429,946 external-priority patent/US3952501A/en
Application filed by United Aircraft of Canada Ltd filed Critical United Aircraft of Canada Ltd
Publication of GB1454206A publication Critical patent/GB1454206A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/26—Controlling the air flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)

Abstract

1454206 Gas turbine engine combustion equipment- UNITED AIRCRAFT OF CANADA Ltd 1 Aug 1974 [2 Jan 1974] 34022/74 Addition to 1385903 Heading F1L In a modification of the primary/secondary airflow control arrangement described in Specification 1385903, the pivoted baffle (243) of that Specification is replaced by a baffle 38 mounted on axially slidable rods 42.
GB3402274A 1974-01-02 1974-08-01 Continuous combustion device Expired GB1454206A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/429,946 US3952501A (en) 1971-04-15 1974-01-02 Gas turbine control

Publications (1)

Publication Number Publication Date
GB1454206A true GB1454206A (en) 1976-11-03

Family

ID=23705393

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3402274A Expired GB1454206A (en) 1974-01-02 1974-08-01 Continuous combustion device

Country Status (3)

Country Link
CA (1) CA1005651A (en)
FR (1) FR2256313B2 (en)
GB (1) GB1454206A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4151713A (en) * 1977-03-15 1979-05-01 United Technologies Corporation Burner for gas turbine engine
DE3209135A1 (en) * 1982-03-12 1983-09-15 Kraftwerk Union AG, 4330 Mülheim GAS TURBINE COMBUSTION CHAMBER

Also Published As

Publication number Publication date
FR2256313B2 (en) 1981-08-07
CA1005651A (en) 1977-02-22
FR2256313A2 (en) 1975-07-25

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee