GB621422A - Improvements relating to gas-turbine-engines - Google Patents
Improvements relating to gas-turbine-enginesInfo
- Publication number
- GB621422A GB621422A GB5347/47A GB534747A GB621422A GB 621422 A GB621422 A GB 621422A GB 5347/47 A GB5347/47 A GB 5347/47A GB 534747 A GB534747 A GB 534747A GB 621422 A GB621422 A GB 621422A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tube
- wall
- bosses
- rods
- sleeve
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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
621,422. Gas turbine plant. LOMBARD, A. A., and OULIANOFF, G. Feb. 24, 1947, No. 5347. [Class 110(iii)] In an exhaust assembly for a gas turbine, an outer converging wall 11, an inner conical structure 12 and a central tube 17 are secured together by two pairs of rods 20, at right angles, which are fastened by bolts 21 in bosses 23 on the wall 11 and are a sliding fit in bosses 24 on the inside of the structure 12 and on the tube 17. The parts of the rods within the exhaust passage are enclosed in fairings 25 as described in Specification 620,446. The tube 17, at its down-stream end, is secured to the structure 12 by a diaphragm 18 and at its upstream end has a sliding fit in a sleeve 19. The sleeve 19 is fixed to an end wall 16 and a heat shield 15. Specification 582,978 also is referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB5347/47A GB621422A (en) | 1947-02-24 | 1947-02-24 | Improvements relating to gas-turbine-engines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB5347/47A GB621422A (en) | 1947-02-24 | 1947-02-24 | Improvements relating to gas-turbine-engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB621422A true GB621422A (en) | 1949-04-08 |
Family
ID=9794391
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB5347/47A Expired GB621422A (en) | 1947-02-24 | 1947-02-24 | Improvements relating to gas-turbine-engines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB621422A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2916018A1 (en) * | 2007-05-10 | 2008-11-14 | Snecma Propulsion Solide Sa | EXHAUST SYSTEM FOR GAS TURBINE |
-
1947
- 1947-02-24 GB GB5347/47A patent/GB621422A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2916018A1 (en) * | 2007-05-10 | 2008-11-14 | Snecma Propulsion Solide Sa | EXHAUST SYSTEM FOR GAS TURBINE |
| WO2008148999A2 (en) * | 2007-05-10 | 2008-12-11 | Snecma Propulsion Solide | Exhaust system for gas turbine |
| WO2008148999A3 (en) * | 2007-05-10 | 2009-03-26 | Snecma Propulsion Solide | Exhaust system for gas turbine |
| US8424312B2 (en) | 2007-05-10 | 2013-04-23 | Snecma Propulsion Solide | Exhaust system for gas turbine |
| CN101675238B (en) * | 2007-05-10 | 2013-11-06 | 斯奈克玛动力部件公司 | Exhaust system for gas turbine |
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