GB1174207A - Improvements in or relating to fluid flow machines - Google Patents
Improvements in or relating to fluid flow machinesInfo
- 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
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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
- F01D11/025—Seal 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.
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)
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 |
-
1968
- 1968-05-30 GB GB2592268A patent/GB1174207A/en not_active Expired
Cited By (17)
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 |