GB1174207A - Improvements in or relating to fluid flow machines - Google Patents

Improvements in or relating to fluid flow machines

Info

Publication number
GB1174207A
GB1174207A GB2592268A GB2592268A GB1174207A GB 1174207 A GB1174207 A GB 1174207A GB 2592268 A GB2592268 A GB 2592268A GB 2592268 A GB2592268 A GB 2592268A GB 1174207 A GB1174207 A GB 1174207A
Authority
GB
United Kingdom
Prior art keywords
pressure
chamber
axial
fluid
gap
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
GB2592268A
Inventor
Ronald Albert Gilbert
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 PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB2592268A priority Critical patent/GB1174207A/en
Publication of GB1174207A publication Critical patent/GB1174207A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/025Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

1,174,207. Turbines; gas turbine plant. ROLLS-ROYCE Ltd. May 30, 1968, No.25922/68. Headings F1G and F1T. [Also in Divisions F2 and G3] Apparatus for controlling the axial gap between a fixed structure and an axially movable rotatable structure of a fluid-flow machine comprises fluidpressure means responsive to changes in a supply pressure and controlling a power source capable of producing relative axial movement between the fixed and rotatable structures, the supply pressure being fed to the fluid-pressure means from a chamber bounded by the structures via an orifice which is closable by a part of the rotatable structure so as to vary the supply pressure in dependence on the size of the gap. When applied to a gas turbine engine to maintain constant the axial clearance "A" between the tips of the turbine rotor blades 22 and part of the housing 21, the invention includes a chamber 20 bounded by a heat shield 18 and pressurized by air from the engine compressor. Axial and radially extending seals 30, 32 maintain the air pressure in chamber 20. An annular flange 26 on an extension 28 of the turbine disc 10 co-operates with a pad 34 secured to heat shield 18, the size of the axial gap between the flange and pad determining the rate of leak-off of air from chamber 20 to a duct 36, 38 and hence the pressure in the duct. The latter is connected to a chamber 40 on one side of a spring loaded diaphragm 44 attached to a spool valve 50 slidable in a bore 52 in a housing 54. A hydraulic pump 68 supplies fluid through a pipe 70 to an inlet port 60 of the bore 52 and, according to the position of spool valve 50, the fluid may pass to one or other of pipes 74, 76, leading to opposite sides of an annular piston 78 slidable in a fixed cylinder 80. The piston 78 is attached to the outer race 82 of a bearing 84, the inner race 86 of which is mounted on the shaft 14 connecting the turbine 10 to the high-pressure compressor (6, Fig.1, not shown), of the engine. Thus any change in pressure in duct 38 as a result of a departure from the desired value of the axial gap causes adjustment of the spool valve 50 and axial movement of bearing 84 and shaft 14 to restore the gap to its desired value. In a modification, the piston 78 is fixed and cylinder 80 movable and attached to shaft 14.
GB2592268A 1968-05-30 1968-05-30 Improvements in or relating to fluid flow machines Expired GB1174207A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2592268A GB1174207A (en) 1968-05-30 1968-05-30 Improvements in or relating to fluid flow machines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2592268A GB1174207A (en) 1968-05-30 1968-05-30 Improvements in or relating to fluid flow machines

Publications (1)

Publication Number Publication Date
GB1174207A true GB1174207A (en) 1969-12-17

Family

ID=10235517

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2592268A Expired GB1174207A (en) 1968-05-30 1968-05-30 Improvements in or relating to fluid flow machines

Country Status (1)

Country Link
GB (1) GB1174207A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS49101714A (en) * 1972-12-16 1974-09-26
EP2025875A2 (en) 2007-08-17 2009-02-18 United Technologies Corporation Hydrostatic seal and back-up seal of a gas turbine engine and corresponding turbine assembly
EP2025876A2 (en) * 2007-08-17 2009-02-18 United Technologies Corporation Hydrostatic seal and back-up seal of a gas turbine engine and corresponding turbine assembly
EP2025877A2 (en) * 2007-08-17 2009-02-18 United Technologies Corporation Hydrostatic seal of a gas turbine engine and corresponding turbine assembly
US8105021B2 (en) 2007-08-20 2012-01-31 United Technologies Corp. Gas turbine engine systems involving hydrostatic face seals with integrated back-up seals
US8109716B2 (en) 2007-08-17 2012-02-07 United Technologies Corp. Gas turbine engine systems involving hydrostatic face seals with anti-fouling provisioning
US8499874B2 (en) 2009-05-12 2013-08-06 Icr Turbine Engine Corporation Gas turbine energy storage and conversion system
US8669670B2 (en) 2010-09-03 2014-03-11 Icr Turbine Engine Corporation Gas turbine engine configurations
US8866334B2 (en) 2010-03-02 2014-10-21 Icr Turbine Engine Corporation Dispatchable power from a renewable energy facility
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS49101714A (en) * 1972-12-16 1974-09-26
US8109717B2 (en) 2007-08-17 2012-02-07 United Technologies Corp. Gas turbine engine systems involving hydrostatic face seals with integrated back-up seals
EP2025875A3 (en) * 2007-08-17 2011-05-25 United Technologies Corporation Hydrostatic seal and back-up seal of a gas turbine engine and corresponding turbine assembly
EP2025877A2 (en) * 2007-08-17 2009-02-18 United Technologies Corporation Hydrostatic seal of a gas turbine engine and corresponding turbine assembly
EP2025876A3 (en) * 2007-08-17 2011-05-18 United Technologies Corporation Hydrostatic seal and back-up seal of a gas turbine engine and corresponding turbine assembly
US8109716B2 (en) 2007-08-17 2012-02-07 United Technologies Corp. Gas turbine engine systems involving hydrostatic face seals with anti-fouling provisioning
EP2025877A3 (en) * 2007-08-17 2011-05-25 United Technologies Corporation Hydrostatic seal of a gas turbine engine and corresponding turbine assembly
EP2025876A2 (en) * 2007-08-17 2009-02-18 United Technologies Corporation Hydrostatic seal and back-up seal of a gas turbine engine and corresponding turbine assembly
EP2025875A2 (en) 2007-08-17 2009-02-18 United Technologies Corporation Hydrostatic seal and back-up seal of a gas turbine engine and corresponding turbine assembly
US8105021B2 (en) 2007-08-20 2012-01-31 United Technologies Corp. Gas turbine engine systems involving hydrostatic face seals with integrated back-up seals
US8499874B2 (en) 2009-05-12 2013-08-06 Icr Turbine Engine Corporation Gas turbine energy storage and conversion system
US8708083B2 (en) 2009-05-12 2014-04-29 Icr Turbine Engine Corporation Gas turbine energy storage and conversion system
US8866334B2 (en) 2010-03-02 2014-10-21 Icr Turbine Engine Corporation Dispatchable power from a renewable energy facility
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
US8669670B2 (en) 2010-09-03 2014-03-11 Icr Turbine Engine Corporation Gas turbine engine configurations
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine

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Legal Events

Date Code Title Description
PS Patent sealed
PLE Entries relating assignments, transmissions, licences in the register of patents
PLNP Patent lapsed through nonpayment of renewal fees