GB620446A - Improvements relating to gas-turbine-engines - Google Patents
Improvements relating to gas-turbine-enginesInfo
- Publication number
- GB620446A GB620446A GB163947A GB163947A GB620446A GB 620446 A GB620446 A GB 620446A GB 163947 A GB163947 A GB 163947A GB 163947 A GB163947 A GB 163947A GB 620446 A GB620446 A GB 620446A
- Authority
- GB
- United Kingdom
- Prior art keywords
- bushes
- fairings
- secured
- walls
- 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
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/04—Mounting of an exhaust cone in the jet pipe
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
620,446. Gas turbine plant for jet-propulsion. LOMBARD, A. A., and OULIANOFF, G. Jan. 17, 1947, No. 1639. [Class 110(iii)] In a gas turbine plant for jet propulsion of aircraft, the diametral rods 20, Fig. 2, which support the conical structure 12 within the exhaust duct shell 11, are enclosed in fairings 25. The fairings have a stream-line shape along the lines of flow and the walls 25a, 25b are curved transversely as shown in Fig. 3. The walls are welded to end plates 29. The rods are secured to bushes 22 on the shell 11 and pass through bushes 30 on the end plates 29 and bushes 24 on stiffening members 14 of the conical structure and on central tube 17. The tube 17 is secured at one end to a flexible flange 18 and at the other end is a sliding fit in the boss 19 of a stiffened disc 16 which supports a heat shield 15.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB163947A GB620446A (en) | 1947-01-17 | 1947-01-17 | Improvements relating to gas-turbine-engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB163947A GB620446A (en) | 1947-01-17 | 1947-01-17 | Improvements relating to gas-turbine-engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB620446A true GB620446A (en) | 1949-03-24 |
Family
ID=9725426
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB163947A Expired GB620446A (en) | 1947-01-17 | 1947-01-17 | Improvements relating to gas-turbine-engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB620446A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2788803A (en) * | 1952-11-12 | 1957-04-16 | Solar Aircraft Co | Tail cone |
US2813396A (en) * | 1952-02-20 | 1957-11-19 | Solar Aircraft Co | Tail cone and resilient mounting therefor |
US2938336A (en) * | 1956-12-06 | 1960-05-31 | United Aircraft Corp | Gas flow straightening vanes |
US3024969A (en) * | 1957-12-26 | 1962-03-13 | Gen Electric | Compressor rear frame |
CN104204490A (en) * | 2012-03-20 | 2014-12-10 | 埃尔塞乐公司 | Aircraft turbojet engine exhaust cone |
-
1947
- 1947-01-17 GB GB163947A patent/GB620446A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2813396A (en) * | 1952-02-20 | 1957-11-19 | Solar Aircraft Co | Tail cone and resilient mounting therefor |
US2788803A (en) * | 1952-11-12 | 1957-04-16 | Solar Aircraft Co | Tail cone |
US2938336A (en) * | 1956-12-06 | 1960-05-31 | United Aircraft Corp | Gas flow straightening vanes |
US3024969A (en) * | 1957-12-26 | 1962-03-13 | Gen Electric | Compressor rear frame |
CN104204490A (en) * | 2012-03-20 | 2014-12-10 | 埃尔塞乐公司 | Aircraft turbojet engine exhaust cone |
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