GB8610559D0 - Gas turbine engines - Google Patents
Gas turbine enginesInfo
- Publication number
- GB8610559D0 GB8610559D0 GB868610559A GB8610559A GB8610559D0 GB 8610559 D0 GB8610559 D0 GB 8610559D0 GB 868610559 A GB868610559 A GB 868610559A GB 8610559 A GB8610559 A GB 8610559A GB 8610559 D0 GB8610559 D0 GB 8610559D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- turbine engines
- engines
- 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.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/065—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front and aft fans
-
- 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
- F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
- F02C5/02—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/072—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with counter-rotating, e.g. fan rotors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/56—Combustion chambers having rotary flame tubes
-
- 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
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08610559A GB2189844A (en) | 1986-04-30 | 1986-04-30 | Gas turbine engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08610559A GB2189844A (en) | 1986-04-30 | 1986-04-30 | Gas turbine engines |
Publications (2)
Publication Number | Publication Date |
---|---|
GB8610559D0 true GB8610559D0 (en) | 1986-11-26 |
GB2189844A GB2189844A (en) | 1987-11-04 |
Family
ID=10597108
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08610559A Withdrawn GB2189844A (en) | 1986-04-30 | 1986-04-30 | Gas turbine engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2189844A (en) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2192234B (en) * | 1986-07-02 | 1991-04-17 | Rolls Royce Plc | A turbofan gas turbine engine |
US5010729A (en) * | 1989-01-03 | 1991-04-30 | General Electric Company | Geared counterrotating turbine/fan propulsion system |
FR2645911B1 (en) * | 1989-04-18 | 1991-06-07 | Snecma | HIGH DILUTION MOTOR WITH UPSTREAM BLOWER AND DOWNSTREAM BLOWER |
DE4234248A1 (en) * | 1992-10-10 | 1994-04-14 | Asea Brown Boveri | Gas turbine group |
RU2052145C1 (en) * | 1993-08-08 | 1996-01-10 | Анатолий Михайлович Рахмаилов | Method of converting heat energy into mechanical work |
WO2005008043A2 (en) * | 2003-07-23 | 2005-01-27 | Eugene Thomas David Archery | Tangentially exhausting revolving combustion chamber in a revolving ramjet, turbojet, turbofan, gas turbine or other jet engine |
FR2866074B1 (en) * | 2004-02-11 | 2006-04-28 | Snecma Moteurs | ARCHITECTURE OF A TURBOJET ENGINE HAVING A DOUBLE BLOWER FORWARD |
US7185484B2 (en) | 2004-08-11 | 2007-03-06 | General Electric Company | Methods and apparatus for assembling a gas turbine engine |
ES2342586B1 (en) * | 2008-04-30 | 2011-06-14 | Futur Investment Partners, S.A. | AERONAUTICAL TURBOPROPULSOR. |
DE102014226696A1 (en) * | 2014-12-19 | 2016-06-23 | Rolls-Royce Deutschland Ltd & Co Kg | Pre-compressor device, retrofit kit and aircraft engine |
FR3067056B1 (en) * | 2017-06-01 | 2019-07-26 | Safran Aircraft Engines | NON-CAREN ROTOR TYPE TURBOREACTOR |
GB201813674D0 (en) | 2018-08-22 | 2018-10-03 | Rolls Royce Plc | Turbomachine |
GB201813672D0 (en) | 2018-08-22 | 2018-10-03 | Rolls Royce Plc | Turbomachine |
GB201813671D0 (en) | 2018-08-22 | 2018-10-03 | Rolls Royce Plc | Turbomachine |
GB201813675D0 (en) | 2018-08-22 | 2018-10-03 | Rolls Royce Plc | Turbomachine |
GB201813670D0 (en) | 2018-08-22 | 2018-10-03 | Rolls Royce Plc | Turbomachine |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1321657A (en) * | 1970-09-16 | 1973-06-27 | Secr Defence | Ducted fan gas turbine jet propulsion engine |
NL8303401A (en) * | 1982-11-01 | 1984-06-01 | Gen Electric | DRIVE TURBINE FOR OPPOSITE ROTATING PROPELLERS. |
-
1986
- 1986-04-30 GB GB08610559A patent/GB2189844A/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2189844A (en) | 1987-11-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |