GB888109A - Improvements relating to gas turbine power plant - Google Patents
Improvements relating to gas turbine power plantInfo
- Publication number
- GB888109A GB888109A GB22637/60A GB2263760A GB888109A GB 888109 A GB888109 A GB 888109A GB 22637/60 A GB22637/60 A GB 22637/60A GB 2263760 A GB2263760 A GB 2263760A GB 888109 A GB888109 A GB 888109A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- duct
- attached
- wall
- gas turbine
- 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
- 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
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
888,109. Generating combustion products under pressure. CANADIAN PRATT & WHITNEY AIRCRAFT CO. Ltd. June 28, 1960 [July 17, 1959], No. 22637/60. Class 51 (1). [Also in Group XXVI] Combustion equipment 10 of a gas-turbine plant comprises an annular flame tube 156 located between the cylindrical portion 70a of the diffuser casing and the outer wall 150 of the turbine exhaust duct and the outer shrouds 152, 154 of the turbine. The plane tube, which is approximately U-shaped in cross-section having a closed upstream.end 158, has slidable connections 156a, 170 with the turbine inlet duct 160. The outer wall 166 of the duct 160 is attached to a ring 170 by a breechblock of bayonet-type of attachment and has a heat shield 172 extending in parallel relation with it. The flame tubes are attached to the casing 70a by clips 181.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US888109XA | 1959-07-17 | 1959-07-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB888109A true GB888109A (en) | 1962-01-24 |
Family
ID=22213627
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB22637/60A Expired GB888109A (en) | 1959-07-17 | 1960-07-28 | Improvements relating to gas turbine power plant |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB888109A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1206659B (en) * | 1962-05-17 | 1965-12-09 | Daimler Benz Ag | Arrangement and drive of the lubricant units in gas turbine engines |
GB2139292A (en) * | 1983-05-02 | 1984-11-07 | Mtu Muenchen Gmbh | Compressor casings |
-
1960
- 1960-07-28 GB GB22637/60A patent/GB888109A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1206659B (en) * | 1962-05-17 | 1965-12-09 | Daimler Benz Ag | Arrangement and drive of the lubricant units in gas turbine engines |
GB2139292A (en) * | 1983-05-02 | 1984-11-07 | Mtu Muenchen Gmbh | Compressor casings |
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