GB713839A - Improvements in or relating to internal combustion turbines - Google Patents

Improvements in or relating to internal combustion turbines

Info

Publication number
GB713839A
GB713839A GB196651A GB196651A GB713839A GB 713839 A GB713839 A GB 713839A GB 196651 A GB196651 A GB 196651A GB 196651 A GB196651 A GB 196651A GB 713839 A GB713839 A GB 713839A
Authority
GB
United Kingdom
Prior art keywords
rotor
compressor
pressure
shaft
combustion chamber
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
GB196651A
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 GB196651A priority Critical patent/GB713839A/en
Publication of GB713839A publication Critical patent/GB713839A/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
    • F02C3/10—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
    • F02C3/103—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 the compressor being of the centrifugal type

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

713,839. Gas turbine plant. ENTICKNAP, A. Oct. 27, 1952 [July 25, 1951; June 19, 1952], Nos. 1966/51 and 15512/52. Class 110(3) A gas turbine plant comprises in combination means to deliver air from a compressor rotor 14 to a stationary combustion chamber 28, means to guide the combustion products into a high-pressure rotor 34 and an oppositely-rotating co-axial low-pressure rotor 35 'located within the highpressure rotor so as to receive the gases radially inwards therefrom and to discharge them axially, one of said rotors being mounted on the compressor-rotor shaft and the other on a power output shaft. A row of fixed nozzle blades may be incorporated between the combustion chamber and the high-pressure turbine rotor. In a modification, Fig. 3 (not shown), the compressor is driven by the high-pressure turbine. The com-. pressor rotor 14 is preferably formed in one piece with its shaft 13. Specifications 587,150. 595,286 and 619,650 are referred to.
GB196651A 1951-07-25 1951-07-25 Improvements in or relating to internal combustion turbines Expired GB713839A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB196651A GB713839A (en) 1951-07-25 1951-07-25 Improvements in or relating to internal combustion turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB196651A GB713839A (en) 1951-07-25 1951-07-25 Improvements in or relating to internal combustion turbines

Publications (1)

Publication Number Publication Date
GB713839A true GB713839A (en) 1954-08-18

Family

ID=9731183

Family Applications (1)

Application Number Title Priority Date Filing Date
GB196651A Expired GB713839A (en) 1951-07-25 1951-07-25 Improvements in or relating to internal combustion turbines

Country Status (1)

Country Link
GB (1) GB713839A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0103370A1 (en) * 1982-08-11 1984-03-21 Rolls-Royce Plc Improvements in or relating to gas turbine engines
GB2169967A (en) * 1985-01-22 1986-07-23 Piers Anthony Benedict Lee Radial flow gas turbine engines
EP1251256A1 (en) * 2001-04-17 2002-10-23 Heinz Dipl.-Ing. Fehrs Gas turbine
US10215052B2 (en) 2017-03-14 2019-02-26 Pratt & Whitney Canada Corp. Inter-shaft bearing arrangement
US10393027B2 (en) 2016-07-19 2019-08-27 Pratt & Whitney Canada Corp. Gas turbine engine shaft architecture and associated method of disassembly
US10465611B2 (en) 2016-09-15 2019-11-05 Pratt & Whitney Canada Corp. Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
US10738709B2 (en) 2017-02-09 2020-08-11 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine
US10746188B2 (en) 2017-03-14 2020-08-18 Pratt & Whitney Canada Corp. Inter-shaft bearing connected to a compressor boost system
US10808624B2 (en) 2017-02-09 2020-10-20 Pratt & Whitney Canada Corp. Turbine rotor with low over-speed requirements
US10815899B2 (en) 2016-11-15 2020-10-27 Pratt & Whitney Canada Corp. Gas turbine engine accessories arrangement
US11035293B2 (en) 2016-09-15 2021-06-15 Pratt & Whitney Canada Corp. Reverse flow gas turbine engine with offset RGB
US11408352B2 (en) 2016-09-15 2022-08-09 Pratt & Whitney Canada Corp. Reverse-flow gas turbine engine
US11536153B2 (en) 2018-08-08 2022-12-27 Pratt & Whitney Canada Corp. Turboshaft gas turbine engine

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0103370A1 (en) * 1982-08-11 1984-03-21 Rolls-Royce Plc Improvements in or relating to gas turbine engines
GB2169967A (en) * 1985-01-22 1986-07-23 Piers Anthony Benedict Lee Radial flow gas turbine engines
EP1251256A1 (en) * 2001-04-17 2002-10-23 Heinz Dipl.-Ing. Fehrs Gas turbine
US10767567B2 (en) 2016-07-19 2020-09-08 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine architecture
US10458340B2 (en) 2016-07-19 2019-10-29 Pratt & Whitney Canada Corp. Turbine shaft power take-off
US10690061B2 (en) 2016-07-19 2020-06-23 Pratt & Whitney Canada Corp. Gear train architecture for a multi-spool gas turbine engine
US10393027B2 (en) 2016-07-19 2019-08-27 Pratt & Whitney Canada Corp. Gas turbine engine shaft architecture and associated method of disassembly
US10883424B2 (en) 2016-07-19 2021-01-05 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine architecture
US11035293B2 (en) 2016-09-15 2021-06-15 Pratt & Whitney Canada Corp. Reverse flow gas turbine engine with offset RGB
US10465611B2 (en) 2016-09-15 2019-11-05 Pratt & Whitney Canada Corp. Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
US11555453B2 (en) 2016-09-15 2023-01-17 Pratt & Whitney Canada Corp. Reverse-flow gas turbine engine
US11415063B2 (en) 2016-09-15 2022-08-16 Pratt & Whitney Canada Corp. Reverse-flow gas turbine engine
US11408352B2 (en) 2016-09-15 2022-08-09 Pratt & Whitney Canada Corp. Reverse-flow gas turbine engine
US11041443B2 (en) 2016-09-15 2021-06-22 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine architecture
US10815899B2 (en) 2016-11-15 2020-10-27 Pratt & Whitney Canada Corp. Gas turbine engine accessories arrangement
US10808624B2 (en) 2017-02-09 2020-10-20 Pratt & Whitney Canada Corp. Turbine rotor with low over-speed requirements
US10738709B2 (en) 2017-02-09 2020-08-11 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine
US10975726B2 (en) 2017-03-14 2021-04-13 Pratt & Whitney Canada Corp. Inter-shaft bearing arrangement
US10215052B2 (en) 2017-03-14 2019-02-26 Pratt & Whitney Canada Corp. Inter-shaft bearing arrangement
US10746188B2 (en) 2017-03-14 2020-08-18 Pratt & Whitney Canada Corp. Inter-shaft bearing connected to a compressor boost system
US11536153B2 (en) 2018-08-08 2022-12-27 Pratt & Whitney Canada Corp. Turboshaft gas turbine engine
US11920479B2 (en) 2018-08-08 2024-03-05 Pratt & Whitney Canada Corp. Multi-engine system and method

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