GB8321281D0 - Underwing engine installation - Google Patents
Underwing engine installationInfo
- Publication number
- GB8321281D0 GB8321281D0 GB838321281A GB8321281A GB8321281D0 GB 8321281 D0 GB8321281 D0 GB 8321281D0 GB 838321281 A GB838321281 A GB 838321281A GB 8321281 A GB8321281 A GB 8321281A GB 8321281 D0 GB8321281 D0 GB 8321281D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine installation
- underwing
- underwing engine
- installation
- engine
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
- B64C7/02—Nacelles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
- B64C21/10—Influencing air flow over aircraft surfaces by affecting boundary layer flow using other surface properties, e.g. roughness
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/16—Aircraft characterised by the type or position of power plant of jet type
- B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
-
- 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
- Y02T50/10—Drag reduction
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB838321281A GB8321281D0 (en) | 1983-08-06 | 1983-08-06 | Underwing engine installation |
GB08419904A GB2144688B (en) | 1983-08-06 | 1984-08-03 | Underwing engine installation for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB838321281A GB8321281D0 (en) | 1983-08-06 | 1983-08-06 | Underwing engine installation |
Publications (1)
Publication Number | Publication Date |
---|---|
GB8321281D0 true GB8321281D0 (en) | 1983-09-28 |
Family
ID=10546964
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB838321281A Pending GB8321281D0 (en) | 1983-08-06 | 1983-08-06 | Underwing engine installation |
GB08419904A Expired GB2144688B (en) | 1983-08-06 | 1984-08-03 | Underwing engine installation for aircraft |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08419904A Expired GB2144688B (en) | 1983-08-06 | 1984-08-03 | Underwing engine installation for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (2) | GB8321281D0 (en) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2555960B1 (en) * | 1983-12-06 | 1986-09-19 | Aerospatiale | BOOM AIRCRAFT WING PROVIDED WITH A HYPERSUSTENTATOR SYSTEM AND AN ENGINE SUSPENSION MAT, AS WELL AS AN ENGINE SUSPENSION MAT FOR SUCH A WING |
US5443230A (en) * | 1993-12-21 | 1995-08-22 | United Technologies Corporation | Aircraft wing/nacelle combination |
WO1998017529A1 (en) | 1996-10-22 | 1998-04-30 | The Boeing Company | Airplane with unswept slotted cruise wing airfoil |
DE19910551C2 (en) * | 1999-03-10 | 2001-04-05 | Eads Airbus Gmbh | Aircraft wing with at least one short-coupled engine |
US6964397B2 (en) | 2003-07-18 | 2005-11-15 | The Boeing Company | Nacelle chine installation for drag reduction |
US6799739B1 (en) | 2003-11-24 | 2004-10-05 | The Boeing Company | Aircraft control surface drive system and associated methods |
US7494094B2 (en) | 2004-09-08 | 2009-02-24 | The Boeing Company | Aircraft wing systems for providing differential motion to deployable lift devices |
US7264206B2 (en) | 2004-09-30 | 2007-09-04 | The Boeing Company | Leading edge flap apparatuses and associated methods |
US7338018B2 (en) | 2005-02-04 | 2008-03-04 | The Boeing Company | Systems and methods for controlling aircraft flaps and spoilers |
US7721999B2 (en) | 2005-05-20 | 2010-05-25 | The Boeing Company | Aerospace vehicle fairing systems and associated methods |
US7475854B2 (en) | 2005-11-21 | 2009-01-13 | The Boeing Company | Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods |
US7708231B2 (en) | 2005-11-21 | 2010-05-04 | The Boeing Company | Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods |
FR2899201B1 (en) * | 2006-03-31 | 2009-02-13 | Airbus France Sas | AIRCRAFT WING ARRANGEMENT COMPRISING A MOTOR ATTACHING MATTING DEFINING IN ZONE BEFORE A SIDE CHANNEL OF AIR FLOW |
US7954769B2 (en) | 2007-12-10 | 2011-06-07 | The Boeing Company | Deployable aerodynamic devices with reduced actuator loads, and related systems and methods |
US7766282B2 (en) | 2007-12-11 | 2010-08-03 | The Boeing Company | Trailing edge device catchers and associated systems and methods |
US8382045B2 (en) | 2009-07-21 | 2013-02-26 | The Boeing Company | Shape-changing control surface |
FR2954270B1 (en) * | 2009-12-18 | 2012-06-01 | Airbus Operations Sas | AIR FENDER WITH MOBILE ATTACK INCOPORING A JUNCTION COMPONENT WITH THE ENGINE MAT |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1118340A (en) * | 1966-12-30 | 1968-07-03 | Rolls Royce | Mounting means for an aircraft engine |
US4314681A (en) * | 1979-08-31 | 1982-02-09 | General Electric Company | Drag-reducing component |
DE3279243D1 (en) * | 1982-09-30 | 1989-01-05 | Boeing Co | Shock inducing pod for causing flow separation |
-
1983
- 1983-08-06 GB GB838321281A patent/GB8321281D0/en active Pending
-
1984
- 1984-08-03 GB GB08419904A patent/GB2144688B/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB2144688B (en) | 1986-09-17 |
GB8419904D0 (en) | 1984-09-05 |
GB2144688A (en) | 1985-03-13 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB8426577D0 (en) | Combustion system | |
GB8405425D0 (en) | Lubrication system | |
DE3479016D1 (en) | Engine mount | |
GB8313907D0 (en) | Engine cooling system | |
GB8419904D0 (en) | Underwing engine installation | |
DE3477228D1 (en) | Diesel engine | |
GB8405305D0 (en) | Fuel-injection system | |
GB8505019D0 (en) | I c engine | |
GB8321910D0 (en) | Engines | |
GB8314471D0 (en) | Engine | |
GB8321909D0 (en) | Engines | |
GB2131321B (en) | Engine system | |
GB8327153D0 (en) | Engines | |
GB8412696D0 (en) | Engine | |
GB8327150D0 (en) | Engine system | |
GB8411842D0 (en) | Ignition system | |
GB8334031D0 (en) | Motor cylinders | |
GB2105271A (en) | Aircraft engine mount | |
GB8418423D0 (en) | Calcinaton installation | |
GB8427169D0 (en) | Piston engine | |
GB8428843D0 (en) | Engine system | |
GB8324844D0 (en) | Engine system | |
GB8701531D0 (en) | I c engine | |
GB8430764D0 (en) | I c engine | |
GB8329239D0 (en) | Engines |