GB1138807A - Aircraft - Google Patents
AircraftInfo
- Publication number
- GB1138807A GB1138807A GB25774/67A GB2577467A GB1138807A GB 1138807 A GB1138807 A GB 1138807A GB 25774/67 A GB25774/67 A GB 25774/67A GB 2577467 A GB2577467 A GB 2577467A GB 1138807 A GB1138807 A GB 1138807A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- engine
- line
- engines
- compressed air
- 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
- 239000007858 starting material Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/42—Arrangement or adaptation of brakes
- B64C25/423—Braking devices acting by reaction of gaseous medium
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/023—Aircraft characterised by the type or position of power plants of rocket type, e.g. for assisting taking-off or braking
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Control Of Turbines (AREA)
Abstract
1,138,807. Aircraft power plant. ROLLSROYCE Ltd. 5 June, 1967, No. 25774/67. Heading B7G. An aircraft having main engines for forward propulsion has an auxiliary engine to provide power for the operation of all the electrical, hydraulic and pneumatic equipment carried by the aircraft, which auxiliary engine alone is arranged to provide reverse thrust for the aircraft. Main gas turbine engines 11 mounted on wings (not shown) have starter devices 12 supplied with compressed air from a common line 13 and valve 14, line 13 being connected also by lines 15 and valves 16 to receive air from the engine compressors. An auxiliary gas turbine engine 20 mounted in the tail of the aircraft (not shown) drives a main compressor 21 connected through control valve 22 to line 13 and pressure regulator 24 to line 25 which supplies compressed air to all the pneumatic equipment carried by the aircraft. Two branch lines 26 provided with valves 27 connect line 13 to constant speed turbines 30 which drive alternators (not shown) to provide power for all the electrical services; and hydraulic pumps (not shown) to provide power for all the hydraulic services. Should engine 20 fail all services can be maintained by the main engines supplying compressed air through lines 15. The engine 20 may assist in forward propulsion of the aircraft and may have provision for thrust reversing. In an alternative embodiment all of the engines drive independent compressors, the outputs of which are fed to a common reducing and mixing regulator.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB25774/67A GB1138807A (en) | 1967-06-05 | 1967-06-05 | Aircraft |
DE19681756535 DE1756535A1 (en) | 1967-06-05 | 1968-06-04 | Airplane with thrust engines |
FR1579621D FR1579621A (en) | 1967-06-05 | 1968-06-17 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB25774/67A GB1138807A (en) | 1967-06-05 | 1967-06-05 | Aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1138807A true GB1138807A (en) | 1969-01-01 |
Family
ID=10233074
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB25774/67A Expired GB1138807A (en) | 1967-06-05 | 1967-06-05 | Aircraft |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1756535A1 (en) |
FR (1) | FR1579621A (en) |
GB (1) | GB1138807A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5855340A (en) * | 1994-04-11 | 1999-01-05 | Bacon; Richard J. | 3X multi-engine jet configuration and method of operation |
US8499874B2 (en) | 2009-05-12 | 2013-08-06 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
US8669670B2 (en) | 2010-09-03 | 2014-03-11 | Icr Turbine Engine Corporation | Gas turbine engine configurations |
US8866334B2 (en) | 2010-03-02 | 2014-10-21 | Icr Turbine Engine Corporation | Dispatchable power from a renewable energy facility |
US8984895B2 (en) | 2010-07-09 | 2015-03-24 | Icr Turbine Engine Corporation | Metallic ceramic spool for a gas turbine engine |
US9051873B2 (en) | 2011-05-20 | 2015-06-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine shaft attachment |
US10094288B2 (en) | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
-
1967
- 1967-06-05 GB GB25774/67A patent/GB1138807A/en not_active Expired
-
1968
- 1968-06-04 DE DE19681756535 patent/DE1756535A1/en active Pending
- 1968-06-17 FR FR1579621D patent/FR1579621A/fr not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5855340A (en) * | 1994-04-11 | 1999-01-05 | Bacon; Richard J. | 3X multi-engine jet configuration and method of operation |
US8499874B2 (en) | 2009-05-12 | 2013-08-06 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
US8708083B2 (en) | 2009-05-12 | 2014-04-29 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
US8866334B2 (en) | 2010-03-02 | 2014-10-21 | Icr Turbine Engine Corporation | Dispatchable power from a renewable energy facility |
US8984895B2 (en) | 2010-07-09 | 2015-03-24 | Icr Turbine Engine Corporation | Metallic ceramic spool for a gas turbine engine |
US8669670B2 (en) | 2010-09-03 | 2014-03-11 | Icr Turbine Engine Corporation | Gas turbine engine configurations |
US9051873B2 (en) | 2011-05-20 | 2015-06-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine shaft attachment |
US10094288B2 (en) | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
Also Published As
Publication number | Publication date |
---|---|
FR1579621A (en) | 1969-08-29 |
DE1756535A1 (en) | 1970-04-02 |
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