GB704274A - Improvements in and relating to gas turbines - Google Patents

Improvements in and relating to gas turbines

Info

Publication number
GB704274A
GB704274A GB2082551A GB2082551A GB704274A GB 704274 A GB704274 A GB 704274A GB 2082551 A GB2082551 A GB 2082551A GB 2082551 A GB2082551 A GB 2082551A GB 704274 A GB704274 A GB 704274A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
pressure
low
compressors
duct
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
GB2082551A
Inventor
John Leslie Barrett
Jerzy Andrzej Lesl Latoszyncki
Clifford Morris
Adolf Frankel
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.)
English Electric Co Ltd
Original Assignee
English Electric Co 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 English Electric Co Ltd filed Critical English Electric Co Ltd
Priority to GB2082551A priority Critical patent/GB704274A/en
Publication of GB704274A publication Critical patent/GB704274A/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
    • F02C3/36—Open cycles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)

Abstract

704,274. Gas turbine plant. ENGLISH ELECTRIC CO., Ltd. Aug. 29, 1952 [Sept. 4, 1951], No. 20825/51. Class 110 (3) A gas turbine plant comprises two gas turbine units, each of which consists of a high-pressure compressor directty coupled to a high-pressure gas turbine, an independently rotatable lowpressure gas turbine in alignment therewith and a combustion chamber. The low-pressure gas turbine 10 of one unit drives the useful load, such as a generator 11, whilst the low-pressure gas turbine 9 of the other unit drives an axially aligned low-pressure compressor 1 which discharges through an intercooler 2 into the inlets of the high-pressure compressors 3, 4 connected in parallel. A balancing duct 16 interconnects the outlets of the compressors 3, 4 and a valvecontrolled blow-off duct 12 connects the intercooler with the inlet duct of the compressor 1. A balancing duct or ducts 17, 18 is connected across the outlets of the high-pressure turbines 7, 8 as shown. The blade heights of the highpressure compressors and/or the high-pressure turbines may be adjusted to suit different mass flows required by the low-pressure turbines associated therewith.
GB2082551A 1951-09-04 1951-09-04 Improvements in and relating to gas turbines Expired GB704274A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2082551A GB704274A (en) 1951-09-04 1951-09-04 Improvements in and relating to gas turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2082551A GB704274A (en) 1951-09-04 1951-09-04 Improvements in and relating to gas turbines

Publications (1)

Publication Number Publication Date
GB704274A true GB704274A (en) 1954-02-17

Family

ID=10152339

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2082551A Expired GB704274A (en) 1951-09-04 1951-09-04 Improvements in and relating to gas turbines

Country Status (1)

Country Link
GB (1) GB704274A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1002991B (en) * 1954-09-10 1957-02-21 Henschel & Sohn Gmbh Gas turbine plant operated in an open circuit
GB2266561A (en) * 1992-04-30 1993-11-03 Snecma Variable cycle turbojet combination.

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1002991B (en) * 1954-09-10 1957-02-21 Henschel & Sohn Gmbh Gas turbine plant operated in an open circuit
GB2266561A (en) * 1992-04-30 1993-11-03 Snecma Variable cycle turbojet combination.
GB2266561B (en) * 1992-04-30 1995-06-14 Snecma Variable cycle propulsion unit for aircraft

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