GB2253657B - Improvements in or relating to gas turbines - Google Patents

Improvements in or relating to gas turbines

Info

Publication number
GB2253657B
GB2253657B GB9125805A GB9125805A GB2253657B GB 2253657 B GB2253657 B GB 2253657B GB 9125805 A GB9125805 A GB 9125805A GB 9125805 A GB9125805 A GB 9125805A GB 2253657 B GB2253657 B GB 2253657B
Authority
GB
United Kingdom
Prior art keywords
relating
gas turbines
turbines
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 - Fee Related
Application number
GB9125805A
Other versions
GB2253657A (en
GB9125805D0 (en
Inventor
Colin Andrew Millar Tayler
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB9125805D0 publication Critical patent/GB9125805D0/en
Publication of GB2253657A publication Critical patent/GB2253657A/en
Application granted granted Critical
Publication of GB2253657B publication Critical patent/GB2253657B/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
    • 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
    • F02C7/125—Cooling of plants by partial arc admission of the working fluid or by intermittent admission of working and cooling fluid
    • 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
    • F02C3/045—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB9125805A 1990-12-08 1991-12-04 Improvements in or relating to gas turbines Expired - Fee Related GB2253657B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB909026748A GB9026748D0 (en) 1990-12-08 1990-12-08 Improvements in or relating to gas turbines

Publications (3)

Publication Number Publication Date
GB9125805D0 GB9125805D0 (en) 1992-02-05
GB2253657A GB2253657A (en) 1992-09-16
GB2253657B true GB2253657B (en) 1995-01-18

Family

ID=10686727

Family Applications (2)

Application Number Title Priority Date Filing Date
GB909026748A Pending GB9026748D0 (en) 1990-12-08 1990-12-08 Improvements in or relating to gas turbines
GB9125805A Expired - Fee Related GB2253657B (en) 1990-12-08 1991-12-04 Improvements in or relating to gas turbines

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB909026748A Pending GB9026748D0 (en) 1990-12-08 1990-12-08 Improvements in or relating to gas turbines

Country Status (1)

Country Link
GB (2) GB9026748D0 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2376163C (en) * 1999-07-19 2005-04-26 Michael A. Wilson Efficiency enhanced turbine engine

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1059876A (en) * 1965-01-13 1967-02-22 Rolls Royce Combustion equipment
GB1104529A (en) * 1966-10-14 1968-02-28 Rolls Royce Gas turbine engine
GB1110302A (en) * 1966-06-17 1968-04-18 Rolls Royce Pressure exchanger
GB1411123A (en) * 1971-10-21 1975-10-22 Gen Power Corp Integral turbo-compressor shock wave engine
GB1420600A (en) * 1972-02-23 1976-01-07 Secr Defence Rotary bladed compressors
US4070824A (en) * 1970-05-26 1978-01-31 Traut Earl W Integrated flow turbine engine
US4757682A (en) * 1985-05-20 1988-07-19 Eugene Bahniuk Axial flow turbine

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1059876A (en) * 1965-01-13 1967-02-22 Rolls Royce Combustion equipment
GB1110302A (en) * 1966-06-17 1968-04-18 Rolls Royce Pressure exchanger
GB1104529A (en) * 1966-10-14 1968-02-28 Rolls Royce Gas turbine engine
US4070824A (en) * 1970-05-26 1978-01-31 Traut Earl W Integrated flow turbine engine
GB1411123A (en) * 1971-10-21 1975-10-22 Gen Power Corp Integral turbo-compressor shock wave engine
GB1420600A (en) * 1972-02-23 1976-01-07 Secr Defence Rotary bladed compressors
US4757682A (en) * 1985-05-20 1988-07-19 Eugene Bahniuk Axial flow turbine

Also Published As

Publication number Publication date
GB9026748D0 (en) 1991-01-30
GB2253657A (en) 1992-09-16
GB9125805D0 (en) 1992-02-05

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Legal Events

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

Effective date: 20071204