GB2041193B - Gas turbine engine combustion apparatus - Google Patents

Gas turbine engine combustion apparatus

Info

Publication number
GB2041193B
GB2041193B GB8003443A GB8003443A GB2041193B GB 2041193 B GB2041193 B GB 2041193B GB 8003443 A GB8003443 A GB 8003443A GB 8003443 A GB8003443 A GB 8003443A GB 2041193 B GB2041193 B GB 2041193B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
combustion apparatus
engine combustion
gas
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
GB8003443A
Other versions
GB2041193A (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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB8003443A priority Critical patent/GB2041193B/en
Publication of GB2041193A publication Critical patent/GB2041193A/en
Application granted granted Critical
Publication of GB2041193B publication Critical patent/GB2041193B/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
    • F23R3/04—Air inlet arrangements
    • 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)
GB8003443A 1979-02-20 1980-02-01 Gas turbine engine combustion apparatus Expired GB2041193B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8003443A GB2041193B (en) 1979-02-20 1980-02-01 Gas turbine engine combustion apparatus

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB7906034 1979-02-20
GB8003443A GB2041193B (en) 1979-02-20 1980-02-01 Gas turbine engine combustion apparatus

Publications (2)

Publication Number Publication Date
GB2041193A GB2041193A (en) 1980-09-03
GB2041193B true GB2041193B (en) 1983-02-09

Family

ID=26270637

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8003443A Expired GB2041193B (en) 1979-02-20 1980-02-01 Gas turbine engine combustion apparatus

Country Status (1)

Country Link
GB (1) GB2041193B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2682802B1 (en) * 1991-10-18 1993-12-03 Sgs Thomson Microelectronics Sa DEVICE FOR GENERATING A PROGRAMMING VOLTAGE FROM A PROGRAMMABLE PERMANENT MEMORY, ESPECIALLY OF THE EPROM TYPE, METHOD AND MEMORY RELATING THERETO.
US5365738A (en) * 1991-12-26 1994-11-22 Solar Turbines Incorporated Low emission combustion nozzle for use with a gas turbine engine
US8281601B2 (en) * 2009-03-20 2012-10-09 General Electric Company Systems and methods for reintroducing gas turbine combustion bypass flow
CN114811652B (en) * 2022-01-27 2023-07-14 南京航空航天大学 Aeroengine combustion chamber adopting MILD combustion

Also Published As

Publication number Publication date
GB2041193A (en) 1980-09-03

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Legal Events

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