GB201617638D0 - Gas turbine engine heat exchanger - Google Patents

Gas turbine engine heat exchanger

Info

Publication number
GB201617638D0
GB201617638D0 GBGB1617638.0A GB201617638A GB201617638D0 GB 201617638 D0 GB201617638 D0 GB 201617638D0 GB 201617638 A GB201617638 A GB 201617638A GB 201617638 D0 GB201617638 D0 GB 201617638D0
Authority
GB
United Kingdom
Prior art keywords
heat exchanger
gas turbine
turbine engine
engine heat
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.)
Withdrawn
Application number
GBGB1617638.0A
Other versions
GB2555379A (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 GB1617638.0A priority Critical patent/GB2555379A/en
Publication of GB201617638D0 publication Critical patent/GB201617638D0/en
Publication of GB2555379A publication Critical patent/GB2555379A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/24—Heat or noise insulation
    • F02C7/25—Fire protection or prevention

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB1617638.0A 2016-10-18 2016-10-18 Gas turbine engine heat exchanger Withdrawn GB2555379A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1617638.0A GB2555379A (en) 2016-10-18 2016-10-18 Gas turbine engine heat exchanger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1617638.0A GB2555379A (en) 2016-10-18 2016-10-18 Gas turbine engine heat exchanger

Publications (2)

Publication Number Publication Date
GB201617638D0 true GB201617638D0 (en) 2016-11-30
GB2555379A GB2555379A (en) 2018-05-02

Family

ID=57680825

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1617638.0A Withdrawn GB2555379A (en) 2016-10-18 2016-10-18 Gas turbine engine heat exchanger

Country Status (1)

Country Link
GB (1) GB2555379A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11300053B2 (en) 2019-10-02 2022-04-12 Honeywell International Inc. Passive flame arrestor system

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9109464B2 (en) * 2011-08-31 2015-08-18 United Technologies Corporation Distributed lubrication system
US9151224B2 (en) * 2012-03-14 2015-10-06 United Technologies Corporation Constant-speed pump system for engine thermal management system AOC reduction and environmental control system loss elimination
EP2900965B1 (en) * 2012-09-28 2017-11-22 United Technologies Corporation Gas turbine engine thermal management system for heat exchanger using bypass flow
WO2015138020A2 (en) * 2013-12-18 2015-09-17 United Technologies Corporation Heat exchanger flow control assembly
EP3090163B1 (en) * 2013-12-30 2018-02-21 United Technologies Corporation Compressor rim thermal management

Also Published As

Publication number Publication date
GB2555379A (en) 2018-05-02

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)