GB809811A - Improvements in and relating to gas turbines - Google Patents
Improvements in and relating to gas turbinesInfo
- Publication number
- GB809811A GB809811A GB35959/56A GB3595956A GB809811A GB 809811 A GB809811 A GB 809811A GB 35959/56 A GB35959/56 A GB 35959/56A GB 3595956 A GB3595956 A GB 3595956A GB 809811 A GB809811 A GB 809811A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- axis
- compressor
- degrees
- tailpipe
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/30—Exhaust heads, chambers, or the like
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
Abstract
809,811. Gas turbine plant. GENERAL ELECTRIC CO. Nov. 23, 1956 [Nov. 25, 1955], No. 35959/56. Class 110 (3). A gas turbine plant comprising in a common casing an axial flow compressor feeding a combustion chamber supplying combustion gas to a turbine driving the compressor and a useful output turbine positioned downstream of and coaxial with the first turbine, has a curved tailpipe which communicates with the atmosphere through an end opening the axis of which makes an angle less than 90 degrees with the axis of the casing and is provided with a depression in its wall on the outside of the curvature which supports a bearing for the turbine output shaft. The compressor 16 supplies air to an annular combustion system 18 feeding a turbine 20 driving the compressor. A separate useful output turbine 22 drives through a shaft 24 and reduction gear 39 a tractor propeller 42 or a pusher propeller 48, or both. The turbine 22 exhausts through a tailpipe 26 which is curved so that the axis of the end opening 28 makes an angle of less than 90 degrees, say 60 degrees, with the engine axis. The output shaft bearing 34 is supported by a pad 37 mounted on the outside of a depression 36 in the tail pipe. The tail pipe may be rotated so that its median plane does not coincide with that of the engine.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US809811XA | 1955-11-25 | 1955-11-25 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB809811A true GB809811A (en) | 1959-03-04 |
Family
ID=22160912
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB35959/56A Expired GB809811A (en) | 1955-11-25 | 1956-11-23 | Improvements in and relating to gas turbines |
Country Status (2)
| Country | Link |
|---|---|
| FR (1) | FR1161685A (en) |
| GB (1) | GB809811A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2117054A (en) * | 1982-02-17 | 1983-10-05 | Rolls Royce | Aircraft propulsion engine having a rear mounted propfan |
| GB2138507A (en) * | 1983-04-22 | 1984-10-24 | Rolls Royce | Mounting end exhausting in turbo-propellor aircraft engines |
| EP1496201A1 (en) * | 2001-01-25 | 2005-01-12 | Mitsubishi Heavy Industries, Ltd. | Gas turbine |
| ITFI20120221A1 (en) * | 2012-10-22 | 2014-04-23 | Nuovo Pignone Srl | "EXHAUST GAS COLLECTOR AND GAS TURBINE" |
| US11473450B2 (en) | 2018-12-28 | 2022-10-18 | General Electric Company | Turbine exhaust collector |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1079896B (en) * | 1959-05-02 | 1960-04-14 | M A N Turbomotoren G M B H | Propeller turbine air jet engine (PTL engine) |
-
1956
- 1956-11-23 FR FR1161685D patent/FR1161685A/en not_active Expired
- 1956-11-23 GB GB35959/56A patent/GB809811A/en not_active Expired
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2117054A (en) * | 1982-02-17 | 1983-10-05 | Rolls Royce | Aircraft propulsion engine having a rear mounted propfan |
| US4488399A (en) * | 1982-02-17 | 1984-12-18 | Rolls-Royce Limited | Propfan aircraft propulsion engine |
| GB2138507A (en) * | 1983-04-22 | 1984-10-24 | Rolls Royce | Mounting end exhausting in turbo-propellor aircraft engines |
| EP1496201A1 (en) * | 2001-01-25 | 2005-01-12 | Mitsubishi Heavy Industries, Ltd. | Gas turbine |
| ITFI20120221A1 (en) * | 2012-10-22 | 2014-04-23 | Nuovo Pignone Srl | "EXHAUST GAS COLLECTOR AND GAS TURBINE" |
| WO2014064031A1 (en) * | 2012-10-22 | 2014-05-01 | Nuovo Pignone Srl | Exhaust gas collector and gas turbine |
| CN105026696A (en) * | 2012-10-22 | 2015-11-04 | 诺沃皮尼奥内股份有限公司 | Exhaust gas collector and gas turbine |
| JP2015532392A (en) * | 2012-10-22 | 2015-11-09 | ヌオーヴォ ピニォーネ ソチエタ レスポンサビリタ リミタータＮｕｏｖｏ Ｐｉｇｎｏｎｅ Ｓ．Ｒ．Ｌ． | Exhaust gas collector and gas turbine |
| RU2668302C2 (en) * | 2012-10-22 | 2018-09-28 | Нуово Пиньоне СРЛ | Exhaust gas manifold and the gas turbine |
| US11473450B2 (en) | 2018-12-28 | 2022-10-18 | General Electric Company | Turbine exhaust collector |
Also Published As
| Publication number | Publication date |
|---|---|
| FR1161685A (en) | 1958-09-03 |
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