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GB906754A - Improvements in or relating to gas turbine engines - Google Patents

Improvements in or relating to gas turbine engines

Info

Publication number
GB906754A
GB906754A GB2061761A GB2061761A GB906754A GB 906754 A GB906754 A GB 906754A GB 2061761 A GB2061761 A GB 2061761A GB 2061761 A GB2061761 A GB 2061761A GB 906754 A GB906754 A GB 906754A
Authority
GB
United Kingdom
Prior art keywords
gases
engine
turbine
gas turbine
fed
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
GB2061761A
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
Priority to DEL34736A priority Critical patent/DE1151985B/en
Application filed by Individual filed Critical Individual
Priority to GB2061761A priority patent/GB906754A/en
Publication of GB906754A publication Critical patent/GB906754A/en
Expired 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/003—Gas-turbine plants with heaters between turbine stages
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Supercharger (AREA)

Abstract

906,754. Gas turbine plant. LUTZ, O. June 7, 1861, No. 20617/61. Class 110 (3). [Also in Groups XXXI and XXXIII] A gas turbine engine feeds gases either from a compressor driven by the engine or the exhaust gases or ram air from the engine intake or a mixture of any of these gases to combustion equipment, where additional fuel may be burnt. The gases from the combustion equipment are fed to a turbine which is drivingly connected to an output shaft mounted so that its rotational axis is pivotable relative to the engines. The exhaust and by-pass air from a by-pass engine 1 are fed to a combustion chamber 11 and then exhausted to atmosphere from a nozzle 17<SP>1</SP> through a turbine 13. The turbine is mounted on an output shaft 16 connected to a propeller 15 by gearing 14. The casing 17 is rotatable about a coupling 12.
GB2061761A 1959-11-18 1961-06-07 Improvements in or relating to gas turbine engines Expired GB906754A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
DEL34736A DE1151985B (en) 1959-11-18 1959-11-18 Gas turbine engine system with a power turbine, with the possibility of a short-term increase in output
GB2061761A GB906754A (en) 1961-06-07 1961-06-07 Improvements in or relating to gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2061761A GB906754A (en) 1961-06-07 1961-06-07 Improvements in or relating to gas turbine engines

Publications (1)

Publication Number Publication Date
GB906754A true GB906754A (en) 1962-09-26

Family

ID=10148892

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2061761A Expired GB906754A (en) 1959-11-18 1961-06-07 Improvements in or relating to gas turbine engines

Country Status (1)

Country Link
GB (1) GB906754A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2923263A1 (en) * 2007-11-07 2009-05-08 Turbomeca Sa TURBOMOTEUR COMPRISING MEANS FOR HEATING THE AIR ENTERING THE FREE TURBINE

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2923263A1 (en) * 2007-11-07 2009-05-08 Turbomeca Sa TURBOMOTEUR COMPRISING MEANS FOR HEATING THE AIR ENTERING THE FREE TURBINE

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