GB720394A - Improvements relating to aircraft and aircraft engine installations - Google Patents
Improvements relating to aircraft and aircraft engine installationsInfo
- Publication number
- GB720394A GB720394A GB1939651A GB1939651A GB720394A GB 720394 A GB720394 A GB 720394A GB 1939651 A GB1939651 A GB 1939651A GB 1939651 A GB1939651 A GB 1939651A GB 720394 A GB720394 A GB 720394A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- slave units
- fuel
- gas turbine
- aircraft
- 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
-
- 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
- B64C29/0091—Accessories not provided for elsewhere
-
- 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
- B64C29/0041—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 jet motors
- B64C29/0075—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 jet motors the motors being tiltable relative to the fuselage
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
- F02C7/228—Dividing fuel between various burners
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
-
- 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
- F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
- F02K1/008—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector in any rearward direction
-
- 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
- F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
- F23R3/48—Flame tube interconnectors, e.g. cross-over tubes
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Supercharger (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1939651A GB720394A (en) | 1951-08-16 | 1951-08-16 | Improvements relating to aircraft and aircraft engine installations |
FR1065631D FR1065631A (fr) | 1951-08-16 | 1952-08-11 | Perfectionnements aux installations d'aérodynes et de moteurs d'aérodynes |
CH308179D CH308179A (de) | 1951-08-16 | 1952-08-15 | Flugzeug. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1939651A GB720394A (en) | 1951-08-16 | 1951-08-16 | Improvements relating to aircraft and aircraft engine installations |
Publications (1)
Publication Number | Publication Date |
---|---|
GB720394A true GB720394A (en) | 1954-12-22 |
Family
ID=10128653
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1939651A Expired GB720394A (en) | 1951-08-16 | 1951-08-16 | Improvements relating to aircraft and aircraft engine installations |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH308179A (fr) |
FR (1) | FR1065631A (fr) |
GB (1) | GB720394A (fr) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2843340A (en) * | 1955-01-12 | 1958-07-15 | Wibault Michel Henri Ma Joseph | Jet aircraft |
US2964267A (en) * | 1955-09-28 | 1960-12-13 | Power Jets Res & Dev Ltd | Aircraft engine fuel systems |
US2964264A (en) * | 1956-01-27 | 1960-12-13 | Martin Co | Power flap for aircraft |
US2986877A (en) * | 1957-03-07 | 1961-06-06 | Paul C Emmons | Rotatable afterburners for jet aircraft |
GB2266561A (en) * | 1992-04-30 | 1993-11-03 | Snecma | Variable cycle turbojet combination. |
GB2402660A (en) * | 2003-06-11 | 2004-12-15 | Rolls Royce Plc | Aircraft propulsion arrangement with a large number of small propulsive assemblies |
EP3998194A1 (fr) * | 2021-02-19 | 2022-05-18 | Lilium eAircraft GmbH | Ensemble ailes pour aéronef |
WO2022175071A1 (fr) * | 2021-02-19 | 2022-08-25 | Lilium Eaircraft Gmbh | Ensemble aile pour aéronef |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3026065A (en) * | 1956-07-10 | 1962-03-20 | Jr Raymond Prunty Holland | Supersonic vertical-rising aircraft |
US3064923A (en) * | 1958-05-02 | 1962-11-20 | Daimler Benz Ag | Gas turbine propulsion plant and an airplane equipped therewith |
FR2883840A1 (fr) * | 2005-03-31 | 2006-10-06 | Noel Gil | Genre de reacteurs encastres dans les ailes et dans la queue de l'avion, marchant par action de frappes d'air comprime |
-
1951
- 1951-08-16 GB GB1939651A patent/GB720394A/en not_active Expired
-
1952
- 1952-08-11 FR FR1065631D patent/FR1065631A/fr not_active Expired
- 1952-08-15 CH CH308179D patent/CH308179A/de unknown
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2843340A (en) * | 1955-01-12 | 1958-07-15 | Wibault Michel Henri Ma Joseph | Jet aircraft |
US2964267A (en) * | 1955-09-28 | 1960-12-13 | Power Jets Res & Dev Ltd | Aircraft engine fuel systems |
US2964264A (en) * | 1956-01-27 | 1960-12-13 | Martin Co | Power flap for aircraft |
US2986877A (en) * | 1957-03-07 | 1961-06-06 | Paul C Emmons | Rotatable afterburners for jet aircraft |
GB2266561A (en) * | 1992-04-30 | 1993-11-03 | Snecma | Variable cycle turbojet combination. |
GB2266561B (en) * | 1992-04-30 | 1995-06-14 | Snecma | Variable cycle propulsion unit for aircraft |
GB2402660A (en) * | 2003-06-11 | 2004-12-15 | Rolls Royce Plc | Aircraft propulsion arrangement with a large number of small propulsive assemblies |
GB2402660B (en) * | 2003-06-11 | 2005-08-17 | Rolls Royce Plc | Propulsion arrangement |
US7364118B2 (en) | 2003-06-11 | 2008-04-29 | Rolls-Royce Plc | Propulsion arrangement |
EP3998194A1 (fr) * | 2021-02-19 | 2022-05-18 | Lilium eAircraft GmbH | Ensemble ailes pour aéronef |
WO2022175071A1 (fr) * | 2021-02-19 | 2022-08-25 | Lilium Eaircraft Gmbh | Ensemble aile pour aéronef |
Also Published As
Publication number | Publication date |
---|---|
FR1065631A (fr) | 1954-05-28 |
CH308179A (de) | 1955-06-30 |
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