GB585344A - Internal-combustion turbine plant - Google Patents

Internal-combustion turbine plant

Info

Publication number
GB585344A
GB585344A GB1566042A GB1566042A GB585344A GB 585344 A GB585344 A GB 585344A GB 1566042 A GB1566042 A GB 1566042A GB 1566042 A GB1566042 A GB 1566042A GB 585344 A GB585344 A GB 585344A
Authority
GB
United Kingdom
Prior art keywords
turbine plant
internal
combustion turbine
jet
heppner
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
GB1566042A
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 GB1566042A priority Critical patent/GB585344A/en
Publication of GB585344A publication Critical patent/GB585344A/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
    • 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
    • F02K3/04—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 the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • 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
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/073—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor and turbine stages being concentric

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Tires In General (AREA)
  • Air Bags (AREA)
  • Looms (AREA)

Abstract

585,344. Gas turbines. ARMSTRONG SIDDELEY MOTORS, Ltd., and HEPPNER, F. A. M. Nov. 5, 1942, No. 15660. Drawings to Specification. [Class 110 (iii)] A continuous combustion gas turbine plant for jet propulsion of aircraft, is arranged with the combustion chamber in front of, or behind, a rotating shell carries jet augmenter blades. Specifications 561,246, [Group XXXIV],585,340, 585,342, 585;346 and 585,349 are referred to.
GB1566042A 1942-11-05 1942-11-05 Internal-combustion turbine plant Expired GB585344A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1566042A GB585344A (en) 1942-11-05 1942-11-05 Internal-combustion turbine plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1566042A GB585344A (en) 1942-11-05 1942-11-05 Internal-combustion turbine plant

Publications (1)

Publication Number Publication Date
GB585344A true GB585344A (en) 1947-02-05

Family

ID=10063140

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1566042A Expired GB585344A (en) 1942-11-05 1942-11-05 Internal-combustion turbine plant

Country Status (1)

Country Link
GB (1) GB585344A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2989843A (en) * 1953-07-24 1961-06-27 Curtiss Wright Corp Engine for supersonic flight

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2989843A (en) * 1953-07-24 1961-06-27 Curtiss Wright Corp Engine for supersonic flight

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