GB791917A - Improvements in and relating to gas turbine plants - Google Patents

Improvements in and relating to gas turbine plants

Info

Publication number
GB791917A
GB791917A GB3500854A GB3500854A GB791917A GB 791917 A GB791917 A GB 791917A GB 3500854 A GB3500854 A GB 3500854A GB 3500854 A GB3500854 A GB 3500854A GB 791917 A GB791917 A GB 791917A
Authority
GB
United Kingdom
Prior art keywords
air
rotor
gas turbine
combustion
compressor
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
GB3500854A
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
Priority to GB3500854A priority Critical patent/GB791917A/en
Publication of GB791917A publication Critical patent/GB791917A/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
    • 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

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)

Abstract

791,917. Gas turbine plant. HOSSACK, N. Dec. 5, 1955 [Dec. 3, 1954], No. 35008/54. Class 110 (3). In a gas turbine plant, the rotor of an air compressor supplying air to the combustion chamber constitutes also the turbine rotor and the rotor blades constitute a regenerative heat exchanger by which heat is transferred from the combustion gases to the air being compressed. The plant shown comprises a double-sided centrifugal type compressor 27, air being supplied thereto through inlets 17. The rotor vanes are formed with extensions 13 which constitute turbine blades. The air issues from the volute 18 into the combustion equipment 11 and the combustion gases issue through outlet 23 on to the extensions 13, thereby driving the rotor and finally discharge at 24. The air issuing from the compressor vanes 13a passes across the turbine blades 13 and becomes heated before discharging to the combustion equipment.
GB3500854A 1954-12-03 1954-12-03 Improvements in and relating to gas turbine plants Expired GB791917A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3500854A GB791917A (en) 1954-12-03 1954-12-03 Improvements in and relating to gas turbine plants

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3500854A GB791917A (en) 1954-12-03 1954-12-03 Improvements in and relating to gas turbine plants

Publications (1)

Publication Number Publication Date
GB791917A true GB791917A (en) 1958-03-12

Family

ID=10372700

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3500854A Expired GB791917A (en) 1954-12-03 1954-12-03 Improvements in and relating to gas turbine plants

Country Status (1)

Country Link
GB (1) GB791917A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3013387A (en) * 1959-12-14 1961-12-19 James N Preston Internal combustion exhaust reaction engine
DE3544184A1 (en) * 1984-01-20 1986-05-28 Franz-Josef 3500 Kassel Weber Radial gas turbine
FR2904367A1 (en) * 2006-07-27 2008-02-01 Bruno Richard Nicol Fauconnier Gas turbine for e.g. helicopter, has casing including air inlet for receiving air, and turbo-compressor including upper part that transforms gas coming out from combustion chamber into mechanical energy and evacuating energy in exhaust

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3013387A (en) * 1959-12-14 1961-12-19 James N Preston Internal combustion exhaust reaction engine
DE3544184A1 (en) * 1984-01-20 1986-05-28 Franz-Josef 3500 Kassel Weber Radial gas turbine
FR2904367A1 (en) * 2006-07-27 2008-02-01 Bruno Richard Nicol Fauconnier Gas turbine for e.g. helicopter, has casing including air inlet for receiving air, and turbo-compressor including upper part that transforms gas coming out from combustion chamber into mechanical energy and evacuating energy in exhaust
WO2008029269A1 (en) * 2006-07-27 2008-03-13 Bruno Fauconnier Gas turbine engine

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