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GB603283A - Improvements in or relating to internal combustion turbine power plants - Google Patents

Improvements in or relating to internal combustion turbine power plants

Info

Publication number
GB603283A
GB603283A GB1855447A GB1855447A GB603283A GB 603283 A GB603283 A GB 603283A GB 1855447 A GB1855447 A GB 1855447A GB 1855447 A GB1855447 A GB 1855447A GB 603283 A GB603283 A GB 603283A
Authority
GB
United Kingdom
Prior art keywords
turbine
relating
internal combustion
power plants
turbine power
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
GB1855447A
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB1855447A priority Critical patent/GB603283A/en
Publication of GB603283A publication Critical patent/GB603283A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20Adaptations of gas-turbine plants for driving vehicles
    • F02C6/206Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10Gas-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

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)

Abstract

603,283. Gas turbine plant for aircraft. POWER JETS (RESEARCH & DEVELOPMENT), Ltd., and HAWTHORNE, W. R. June 27, 1946, No. 18554/47. Drawings to Specification. [Class 110 (iii)] A gas turbine plant comprising a h.p. compressor driven by a h.p. turbine and a l.p. compressor driven by a l.p. turbine differs from that described in Specification 602,584 in that the air-screw shaft is directly connected to the l.p. turbine shaft and speed-reduction gear, if any, for the airscrew is located forwardly of the h.p. turbine. The turbine exhaust may be led to a propulsion jet.
GB1855447A 1946-06-27 1946-06-27 Improvements in or relating to internal combustion turbine power plants Expired GB603283A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1855447A GB603283A (en) 1946-06-27 1946-06-27 Improvements in or relating to internal combustion turbine power plants

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1855447A GB603283A (en) 1946-06-27 1946-06-27 Improvements in or relating to internal combustion turbine power plants

Publications (1)

Publication Number Publication Date
GB603283A true GB603283A (en) 1948-06-11

Family

ID=10114436

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1855447A Expired GB603283A (en) 1946-06-27 1946-06-27 Improvements in or relating to internal combustion turbine power plants

Country Status (1)

Country Link
GB (1) GB603283A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0395497A1 (en) * 1989-04-26 1990-10-31 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Counter rotating prop-fan engine
US9644537B2 (en) 2013-03-14 2017-05-09 United Technologies Corporation Free stream intake with particle separator for reverse core engine
FR3061241A1 (en) * 2016-12-23 2018-06-29 Safran Aircraft Engines REVERSE FLOW TURBOPROPULSER
EP3572638B1 (en) * 2016-07-19 2020-12-23 Pratt & Whitney Canada Corp. Turboprop engine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0395497A1 (en) * 1989-04-26 1990-10-31 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Counter rotating prop-fan engine
FR2646473A1 (en) * 1989-04-26 1990-11-02 Snecma ENGINE WITH TRACTRIC CONTROTOTATIVE BLOWERS
US5105618A (en) * 1989-04-26 1992-04-21 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Counterrotating fan engine
US9644537B2 (en) 2013-03-14 2017-05-09 United Technologies Corporation Free stream intake with particle separator for reverse core engine
EP3572638B1 (en) * 2016-07-19 2020-12-23 Pratt & Whitney Canada Corp. Turboprop engine
FR3061241A1 (en) * 2016-12-23 2018-06-29 Safran Aircraft Engines REVERSE FLOW TURBOPROPULSER

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