GB9205454D0 - A device for adjusting guide vanes - Google Patents

A device for adjusting guide vanes

Info

Publication number
GB9205454D0
GB9205454D0 GB929205454A GB9205454A GB9205454D0 GB 9205454 D0 GB9205454 D0 GB 9205454D0 GB 929205454 A GB929205454 A GB 929205454A GB 9205454 A GB9205454 A GB 9205454A GB 9205454 D0 GB9205454 D0 GB 9205454D0
Authority
GB
United Kingdom
Prior art keywords
guide vanes
adjusting guide
adjusting
vanes
guide
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.)
Withdrawn
Application number
GB929205454A
Other versions
GB2264984A (en
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.)
Rolls Royce Deutschland Ltd and Co KG
Original Assignee
BMW Rolls Royce GmbH
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 BMW Rolls Royce GmbH filed Critical BMW Rolls Royce GmbH
Priority to GB9205454A priority Critical patent/GB2264984A/en
Publication of GB9205454D0 publication Critical patent/GB9205454D0/en
Priority to DE19924216033 priority patent/DE4216033A1/en
Publication of GB2264984A publication Critical patent/GB2264984A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB9205454A 1992-03-12 1992-03-12 A device for adjusting gas turbine guide vanes. Withdrawn GB2264984A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB9205454A GB2264984A (en) 1992-03-12 1992-03-12 A device for adjusting gas turbine guide vanes.
DE19924216033 DE4216033A1 (en) 1992-03-12 1992-05-15 GUIDE BLADE ADJUSTMENT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9205454A GB2264984A (en) 1992-03-12 1992-03-12 A device for adjusting gas turbine guide vanes.

Publications (2)

Publication Number Publication Date
GB9205454D0 true GB9205454D0 (en) 1992-04-22
GB2264984A GB2264984A (en) 1993-09-15

Family

ID=10712038

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9205454A Withdrawn GB2264984A (en) 1992-03-12 1992-03-12 A device for adjusting gas turbine guide vanes.

Country Status (2)

Country Link
DE (1) DE4216033A1 (en)
GB (1) GB2264984A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19516382A1 (en) * 1995-05-04 1996-11-07 Deutsche Forsch Luft Raumfahrt Adjustment ring
DE19901509B4 (en) * 1999-01-16 2010-11-25 Rolls-Royce Deutschland Ltd & Co Kg Method for adjusting the guide vanes of a fluid flow machine
GB0326544D0 (en) 2003-11-14 2003-12-17 Rolls Royce Plc Variable stator vane arrangement for a compressor
DE102007012119A1 (en) 2007-03-13 2008-09-18 Rolls-Royce Deutschland Ltd & Co Kg Throttling degree dependent blade adjustment in turbomachines

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB857800A (en) * 1957-04-29 1961-01-04 Gen Electric Improvements in compressor
DE2247400C2 (en) * 1972-09-27 1975-01-16 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Device for blowing off compressed air from a compressor of a gas turbine jet engine
US4035101A (en) * 1976-03-24 1977-07-12 Westinghouse Electric Corporation Gas turbine nozzle vane adjusting mechanism
US4373859A (en) * 1981-09-23 1983-02-15 General Motors Corporation Unison ring support system
US4989406A (en) * 1988-12-29 1991-02-05 General Electric Company Turbine engine assembly with aft mounted outlet guide vanes
DE4102188C2 (en) * 1991-01-25 1994-09-22 Mtu Muenchen Gmbh Guide vane adjustment device of a turbine of a gas turbine engine

Also Published As

Publication number Publication date
GB2264984A (en) 1993-09-15
DE4216033A1 (en) 1993-09-16

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)