[go: up one dir, main page]

GB2350158B - Gas turbine engine with low exhaust temperature - Google Patents

Gas turbine engine with low exhaust temperature

Info

Publication number
GB2350158B
GB2350158B GB8709735A GB8709735A GB2350158B GB 2350158 B GB2350158 B GB 2350158B GB 8709735 A GB8709735 A GB 8709735A GB 8709735 A GB8709735 A GB 8709735A GB 2350158 B GB2350158 B GB 2350158B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
exhaust temperature
low exhaust
low
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 - Fee Related
Application number
GB8709735A
Other versions
GB8709735D0 (en
GB2350158A (en
Inventor
Graham A Reynolds
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 GB8709735A priority Critical patent/GB2350158B/en
Publication of GB8709735D0 publication Critical patent/GB8709735D0/en
Publication of GB2350158A publication Critical patent/GB2350158A/en
Application granted granted Critical
Publication of GB2350158B publication Critical patent/GB2350158B/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • 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
    • F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • 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
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • 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
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
    • 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
    • F02C7/22—Fuel supply systems
    • F02C7/224—Heating fuel before feeding to the burner
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/60—Application making use of surplus or waste energy

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
GB8709735A 1987-04-24 1987-04-24 Gas turbine engine with low exhaust temperature Expired - Fee Related GB2350158B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8709735A GB2350158B (en) 1987-04-24 1987-04-24 Gas turbine engine with low exhaust temperature

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8709735A GB2350158B (en) 1987-04-24 1987-04-24 Gas turbine engine with low exhaust temperature

Publications (3)

Publication Number Publication Date
GB8709735D0 GB8709735D0 (en) 2000-10-04
GB2350158A GB2350158A (en) 2000-11-22
GB2350158B true GB2350158B (en) 2001-04-04

Family

ID=10616290

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8709735A Expired - Fee Related GB2350158B (en) 1987-04-24 1987-04-24 Gas turbine engine with low exhaust temperature

Country Status (1)

Country Link
GB (1) GB2350158B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2409001B (en) 2003-12-13 2006-04-05 Rolls Royce Plc Transferring thermal energy between gas and a fuel in a gas turbine engine
WO2007023326A1 (en) * 2005-08-23 2007-03-01 Shap Spa Solar Heat And Power Cogeneration plant
EP3978737B1 (en) 2020-09-30 2024-04-17 Rolls-Royce plc Complex cycle gas turbine engine
GB2627310B (en) * 2023-03-28 2025-03-26 Clean Energy Design Systems Ltd Hydrogen fueled gas turbine power system

Also Published As

Publication number Publication date
GB8709735D0 (en) 2000-10-04
GB2350158A (en) 2000-11-22

Similar Documents

Publication Publication Date Title
GB2207191B (en) Gas turbine engine
GB2211596B (en) Gas turbine engine carburetor
GB8708859D0 (en) Gas turbine engine
GB8726985D0 (en) Turbofan gas turbine engine
GB8624163D0 (en) Turbofan gas turbine engine
GB2194553B (en) Gas turbine engine airfoils
GB8700806D0 (en) Turbopropeller/gas turbine engine
GB2190146B (en) Gas turbine engines
GB8616153D0 (en) Turbofan gas turbine engine
GB2254661B (en) Gas turbine engine
GB2206686B (en) Gas turbine engine augmentor
GB8610180D0 (en) Gas turbine engine
EP0241404A3 (en) Gas turbine engine nacelle
GB8624833D0 (en) Intake for turbopropeller gas turbine engine
GB2213525B (en) Engine with exhaust gas sensing
GB2192237B (en) Gas turbine engine power turbine
GB8620199D0 (en) Gas turbine engine
GB8619653D0 (en) Gas turbine engine
GB8610559D0 (en) Gas turbine engines
IL80634A0 (en) Gas turbine engine augmentor
GB8630334D0 (en) Gas turbine engine
GB8830151D0 (en) Gas turbine engine
GB8703101D0 (en) Gas turbine engine combustion chambers
GB8616154D0 (en) Turbofan gas turbine engine
GB2350158B (en) Gas turbine engine with low exhaust temperature

Legal Events

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

Effective date: 20010704