FR1285627A - Gas turbine engine group - Google Patents
Gas turbine engine groupInfo
- Publication number
- FR1285627A FR1285627A FR857575A FR857575A FR1285627A FR 1285627 A FR1285627 A FR 1285627A FR 857575 A FR857575 A FR 857575A FR 857575 A FR857575 A FR 857575A FR 1285627 A FR1285627 A FR 1285627A
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- turbine engine
- engine group
- group
- gas
- 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
- 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
- F23R3/52—Toroidal combustion chambers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
-
- 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
-
- 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
- F02K3/062—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 aft fan
-
- 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)
- Aviation & Aerospace Engineering (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR857575A FR1285627A (en) | 1961-03-31 | 1961-03-31 | Gas turbine engine group |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR857575A FR1285627A (en) | 1961-03-31 | 1961-03-31 | Gas turbine engine group |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR1285627A true FR1285627A (en) | 1962-02-23 |
Family
ID=8752238
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR857575A Expired FR1285627A (en) | 1961-03-31 | 1961-03-31 | Gas turbine engine group |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR1285627A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1233660B (en) * | 1963-01-31 | 1967-02-02 | Rolls Royce | Ring-shaped incinerator for gas turbine jet engines |
| DE1234096B (en) * | 1962-11-14 | 1967-02-09 | Saurer Ag Adolph | Gas turbine plant |
| DE1256483B (en) * | 1963-12-03 | 1967-12-14 | Rolls Royce | Gas turbine jet engine |
| FR2948735A1 (en) * | 2009-07-30 | 2011-02-04 | Turbomeca | Air diffuser for use at exit of last stage/floor of compressor of aviation turbo-machine i.e. turbo jet engine, in aircraft, has annular bent part whose concavity is provided opposite to that of intermediate bent portion |
| DE102011113784A1 (en) * | 2011-09-17 | 2013-06-27 | Diyan Petrov Petrov | Disc shaped vertical lifting turbocompressor for turbojet engine of aircraft, has combustion chamber which is arranged on the tangent line of rotary compressor for adjusting the time required for flow of gas through combustion chamber |
-
1961
- 1961-03-31 FR FR857575A patent/FR1285627A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1234096B (en) * | 1962-11-14 | 1967-02-09 | Saurer Ag Adolph | Gas turbine plant |
| DE1233660B (en) * | 1963-01-31 | 1967-02-02 | Rolls Royce | Ring-shaped incinerator for gas turbine jet engines |
| DE1256483B (en) * | 1963-12-03 | 1967-12-14 | Rolls Royce | Gas turbine jet engine |
| FR2948735A1 (en) * | 2009-07-30 | 2011-02-04 | Turbomeca | Air diffuser for use at exit of last stage/floor of compressor of aviation turbo-machine i.e. turbo jet engine, in aircraft, has annular bent part whose concavity is provided opposite to that of intermediate bent portion |
| DE102011113784A1 (en) * | 2011-09-17 | 2013-06-27 | Diyan Petrov Petrov | Disc shaped vertical lifting turbocompressor for turbojet engine of aircraft, has combustion chamber which is arranged on the tangent line of rotary compressor for adjusting the time required for flow of gas through combustion chamber |
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