GB592081A - Improvements in gas turbine systems - Google Patents

Improvements in gas turbine systems

Info

Publication number
GB592081A
GB592081A GB17148/44A GB1714844A GB592081A GB 592081 A GB592081 A GB 592081A GB 17148/44 A GB17148/44 A GB 17148/44A GB 1714844 A GB1714844 A GB 1714844A GB 592081 A GB592081 A GB 592081A
Authority
GB
United Kingdom
Prior art keywords
pressure
turbine
compressor
discharge
compressors
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
GB17148/44A
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.)
Ljungstroms Angturbin AB
Original Assignee
Ljungstroms Angturbin AB
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 Ljungstroms Angturbin AB filed Critical Ljungstroms Angturbin AB
Publication of GB592081A publication Critical patent/GB592081A/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
    • F02C6/003Gas-turbine plants with heaters between turbine stages

Landscapes

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

Abstract

592,081. Fluid-pressure servomotorcontrol systems. AKTIEBOLAGET LJUNGSTROMS ANGTURBIN.. Sept. 8, 1944, No. 17148. Convention date, Jan. 28. [Class 135] [Also in Group XXVI] A gas turbine driving a compressor is controlled through a servomotor by the discharge pressure of the compressor. The throttle valve 62 in the intake duct 46 of the turbine is operated by a servomotor 68, the control piston 74 of which is balanced between the pressure in a diaphragm 78 and a spring 80. Any change of pressure in the diaphragm causes the control piston to move and allow pressure oil to pass from the pipe 84 to one side or the other of the piston 66 and so open or close the valve 62 to alter the speed of the turbine and bring the pressure at the discharge of the compressor back to the required value. The pressure required can be pre-set by means of the hand wheel 82 which increases or decreases the compression in the spring 80. The throttle valve 62 can be replaced by means whereby some of the turbine nozzles are cut in or out of service. In a plant employing high pressure *and low pressure turbines driving high and lowpressure compressors, the discharge pressure of both compressors may be used conjointly to control the low-pressure turbine.
GB17148/44A 1944-01-28 1944-09-08 Improvements in gas turbine systems Expired GB592081A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE592081X 1944-01-28

Publications (1)

Publication Number Publication Date
GB592081A true GB592081A (en) 1947-09-08

Family

ID=20312644

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17148/44A Expired GB592081A (en) 1944-01-28 1944-09-08 Improvements in gas turbine systems

Country Status (1)

Country Link
GB (1) GB592081A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2289721A (en) * 1994-05-26 1995-11-29 Abb Management Ag Gas turbine engine fuel control

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2289721A (en) * 1994-05-26 1995-11-29 Abb Management Ag Gas turbine engine fuel control
GB2289721B (en) * 1994-05-26 1998-03-18 Abb Management Ag Method of controlling a gas-turbine group

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