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GB0411943D0 - Gas turbine engine - Google Patents

Gas turbine engine

Info

Publication number
GB0411943D0
GB0411943D0 GBGB0411943.4A GB0411943A GB0411943D0 GB 0411943 D0 GB0411943 D0 GB 0411943D0 GB 0411943 A GB0411943 A GB 0411943A GB 0411943 D0 GB0411943 D0 GB 0411943D0
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
engine
gas
turbine
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.)
Ceased
Application number
GBGB0411943.4A
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 GBGB0411943.4A priority Critical patent/GB0411943D0/en
Publication of GB0411943D0 publication Critical patent/GB0411943D0/en
Priority to GB0509813A priority patent/GB2414520B/en
Priority to DE602005013027T priority patent/DE602005013027D1/en
Priority to EP05253147A priority patent/EP1607612B1/en
Priority to US11/134,278 priority patent/US7500352B2/en
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/025—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the by-pass flow being at least partly used to create an independent thrust component
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00—Axial-flow pumps
    • F04D19/002—Axial flow fans
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00—Axial-flow pumps
    • F04D19/007—Axial-flow pumps multistage fans
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00—Axial-flow pumps
    • F04D19/02—Multi-stage pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GBGB0411943.4A 2004-05-28 2004-05-28 Gas turbine engine Ceased GB0411943D0 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GBGB0411943.4A GB0411943D0 (en) 2004-05-28 2004-05-28 Gas turbine engine
GB0509813A GB2414520B (en) 2004-05-28 2005-05-12 Gas turbine engine
DE602005013027T DE602005013027D1 (en) 2004-05-28 2005-05-20 gas turbine
EP05253147A EP1607612B1 (en) 2004-05-28 2005-05-20 Gas turbine engine
US11/134,278 US7500352B2 (en) 2004-05-28 2005-05-23 Gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0411943.4A GB0411943D0 (en) 2004-05-28 2004-05-28 Gas turbine engine

Publications (1)

Publication Number Publication Date
GB0411943D0 true GB0411943D0 (en) 2004-06-30

Family

ID=32671217

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB0411943.4A Ceased GB0411943D0 (en) 2004-05-28 2004-05-28 Gas turbine engine
GB0509813A Expired - Fee Related GB2414520B (en) 2004-05-28 2005-05-12 Gas turbine engine

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB0509813A Expired - Fee Related GB2414520B (en) 2004-05-28 2005-05-12 Gas turbine engine

Country Status (2)

Country Link
DE (1) DE602005013027D1 (en)
GB (2) GB0411943D0 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109424472A (en) * 2017-08-31 2019-03-05 劳斯莱斯有限公司 Gas-turbine unit

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102395851B1 (en) * 2015-04-08 2022-05-10 삼성전자주식회사 Fan assembly and air conditioner having the same

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1003740A (en) * 1964-06-08 1965-09-08 Rolls Royce Helicopter rotor
GB1018538A (en) * 1964-07-06 1966-01-26 Rolls Royce Gas turbine engine
GB1055328A (en) * 1964-07-20 1967-01-18 Rolls Royce Gas turbine engine
US4860537A (en) * 1986-08-29 1989-08-29 Brandt, Inc. High bypass ratio counterrotating gearless front fan engine
US4916894A (en) * 1989-01-03 1990-04-17 General Electric Company High bypass turbofan engine having a partially geared fan drive turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109424472A (en) * 2017-08-31 2019-03-05 劳斯莱斯有限公司 Gas-turbine unit

Also Published As

Publication number Publication date
GB0509813D0 (en) 2005-06-22
GB2414520B (en) 2006-07-05
DE602005013027D1 (en) 2009-04-16
GB2414520A (en) 2005-11-30

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Legal Events

Date Code Title Description
AT Applications terminated before publication under section 16(1)