GB713783A - Gas turbine propulsion units - Google Patents

Gas turbine propulsion units

Info

Publication number
GB713783A
GB713783A GB12852A GB12852A GB713783A GB 713783 A GB713783 A GB 713783A GB 12852 A GB12852 A GB 12852A GB 12852 A GB12852 A GB 12852A GB 713783 A GB713783 A GB 713783A
Authority
GB
United Kingdom
Prior art keywords
compressor
gas turbine
fan
duct
intake
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
GB12852A
Inventor
Gilbert William Beesley
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.)
Armstrong Siddeley Motors Ltd
Original Assignee
Armstrong Siddeley Motors Ltd
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 Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Priority to GB12852A priority Critical patent/GB713783A/en
Publication of GB713783A publication Critical patent/GB713783A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/022—Blade-carrying members, e.g. rotors with concentric rows of axial blades

Abstract

713,783. Jet propulsion plant. ARMSTRONG SIDDELEY MOTORS, Ltd. Dec. 24, 1952 [Jan. 2, 1952], No. 128/52 Class 110(3) In a ducted fan gas turbine en gine comprising a fan 16 and a compressor 11 which are arranged in separate ducts and are driven by a gas turbine providing a propulsion thrust, means, such as arcuate flaps 26. are provided for diverting when desired, the whole of the out out from the fan into the intake 18 of the compressor. Arcuate flaps 29 32 are also provided to control the duct 30 leading from the fan outlet to the compressor intake and the inlet 25 of the compressor respect ively. Burners may be provided ir the outer duct and in the turbine exhaust duct. The engine may incorporate a variable area jet propulsion nozzle.
GB12852A 1952-01-02 1952-01-02 Gas turbine propulsion units Expired GB713783A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB12852A GB713783A (en) 1952-01-02 1952-01-02 Gas turbine propulsion units

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB12852A GB713783A (en) 1952-01-02 1952-01-02 Gas turbine propulsion units

Publications (1)

Publication Number Publication Date
GB713783A true GB713783A (en) 1954-08-18

Family

ID=9698906

Family Applications (1)

Application Number Title Priority Date Filing Date
GB12852A Expired GB713783A (en) 1952-01-02 1952-01-02 Gas turbine propulsion units

Country Status (1)

Country Link
GB (1) GB713783A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1058315B (en) * 1955-09-30 1959-05-27 Power Jets Res & Dev Ltd Jet engine with air inlet connected to a combustion chamber via a connecting duct and device arranged within this connecting duct for increasing the pressure of the air flowing from the air inlet to the combustion chamber
US3016698A (en) * 1959-07-02 1962-01-16 Gen Motors Corp Bypass engine
DE1134555B (en) * 1958-06-05 1962-08-09 Gen Electric Recoil engine for supersonic flight speed
US3176463A (en) * 1960-09-27 1965-04-06 Snecma Flight control and stabilization by hot jets, applicable in particular to aircraft taking off vertically without change of attitude
DE1277638B (en) * 1961-02-06 1968-09-12 Snecma Combination jet engine
DE1289364B (en) * 1964-08-04 1969-02-13 Rolls Royce Compound engine for propulsion of aircraft
US3548597A (en) * 1968-09-16 1970-12-22 Alexander Hossen Etessam Turbine engine for aircraft having a supplementary compressor driven by a supplementary turbine
US4038818A (en) * 1972-05-25 1977-08-02 Rolls-Royce (1971) Limited Gas turbine power plant having series-parallel valve arrangement
US4085583A (en) * 1975-03-31 1978-04-25 The Boeing Company Method for selectively switching motive fluid supply to an aft turbine of a multicycle engine
US4569199A (en) * 1982-09-29 1986-02-11 The Boeing Company Turboprop engine and method of operating the same
GB2301402A (en) * 1988-12-02 1996-12-04 Rolls Royce Plc Valve for diverting fluid flows in gas turbine engines
EP1918551A2 (en) * 2006-10-24 2008-05-07 Rolls-Royce plc Gas turbine engine

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1058315B (en) * 1955-09-30 1959-05-27 Power Jets Res & Dev Ltd Jet engine with air inlet connected to a combustion chamber via a connecting duct and device arranged within this connecting duct for increasing the pressure of the air flowing from the air inlet to the combustion chamber
DE1134555B (en) * 1958-06-05 1962-08-09 Gen Electric Recoil engine for supersonic flight speed
US3016698A (en) * 1959-07-02 1962-01-16 Gen Motors Corp Bypass engine
US3176463A (en) * 1960-09-27 1965-04-06 Snecma Flight control and stabilization by hot jets, applicable in particular to aircraft taking off vertically without change of attitude
DE1277638B (en) * 1961-02-06 1968-09-12 Snecma Combination jet engine
DE1289364B (en) * 1964-08-04 1969-02-13 Rolls Royce Compound engine for propulsion of aircraft
US3548597A (en) * 1968-09-16 1970-12-22 Alexander Hossen Etessam Turbine engine for aircraft having a supplementary compressor driven by a supplementary turbine
US4038818A (en) * 1972-05-25 1977-08-02 Rolls-Royce (1971) Limited Gas turbine power plant having series-parallel valve arrangement
US4085583A (en) * 1975-03-31 1978-04-25 The Boeing Company Method for selectively switching motive fluid supply to an aft turbine of a multicycle engine
US4569199A (en) * 1982-09-29 1986-02-11 The Boeing Company Turboprop engine and method of operating the same
GB2301402A (en) * 1988-12-02 1996-12-04 Rolls Royce Plc Valve for diverting fluid flows in gas turbine engines
GB2301402B (en) * 1988-12-02 1997-09-03 Rolls Royce Plc Valve for diverting fluid flows in gas turbine engines
EP1918551A2 (en) * 2006-10-24 2008-05-07 Rolls-Royce plc Gas turbine engine
EP1918551A3 (en) * 2006-10-24 2014-04-09 Rolls-Royce plc Gas turbine engine

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