GB1227804A - - Google Patents
Info
- Publication number
- GB1227804A GB1227804A GB3559968A GB3559968A GB1227804A GB 1227804 A GB1227804 A GB 1227804A GB 3559968 A GB3559968 A GB 3559968A GB 3559968 A GB3559968 A GB 3559968A GB 1227804 A GB1227804 A GB 1227804A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flap
- flaps
- jet
- aircraft
- july
- 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
- B64C29/0008—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
- B64C29/0058—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 with vertical jet
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/16—Fairings movable in conjunction with undercarriage elements
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Transmission Devices (AREA)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEV34149A DE1284851B (de) | 1967-07-26 | 1967-07-26 | Flugzeug mit zumindest einem Hubtriebwerk, dessen Auslass durch zwei hintereinanderliegende Klappen verschliessbar ist |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1227804A true GB1227804A (zh) | 1971-04-07 |
Family
ID=7588659
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3559968A Expired GB1227804A (zh) | 1967-07-26 | 1968-07-25 |
Country Status (4)
Country | Link |
---|---|
US (1) | US3486721A (zh) |
DE (1) | DE1284851B (zh) |
FR (1) | FR1579036A (zh) |
GB (1) | GB1227804A (zh) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2279629A (en) * | 1993-06-25 | 1995-01-11 | Rolls Royce Plc | Vectorable nozzle for aircraft. |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4760960A (en) * | 1987-05-22 | 1988-08-02 | United Technologies Corporation | Linkage for area controlled, thrust vectoring vane cascade |
FR2634251B1 (fr) * | 1988-07-18 | 1993-08-13 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a double flux equipe de bords de deviation mobiles |
US5213286A (en) * | 1990-10-10 | 1993-05-25 | General Electric Company | Door for aircraft nacelle |
GB2435637B (en) * | 1991-12-06 | 2008-02-06 | British Aerospace | Jet Propulsion Outlets |
GB0002264D0 (en) * | 2000-02-02 | 2000-03-22 | British Aerospace | Landing gear doors |
US6345786B1 (en) | 2000-03-03 | 2002-02-12 | The Boeing Company | Linked multi-segment landing gear door for aircraft |
US6352221B1 (en) | 2000-03-03 | 2002-03-05 | The Boeing Company | Rotary landing gear assembly |
DE10313729B4 (de) * | 2003-03-27 | 2007-11-29 | Airbus Deutschland Gmbh | Luftauslaßventil für ein Flugzeug |
US8342920B2 (en) * | 2008-10-20 | 2013-01-01 | Honeywell International Inc. | Outflow valve having J-shaped bellmouth and cabin pressure control system employing the same |
US8376818B2 (en) * | 2009-01-29 | 2013-02-19 | Honeywell International Inc. | Thrust recovery, or other valve, containing two independently actuated doors and control system |
DE102009010150B4 (de) * | 2009-02-23 | 2013-09-19 | Airbus Operations Gmbh | System und Verfahren zur Notbelüftung einer Flugzeugkabine |
US20120096772A1 (en) * | 2010-10-25 | 2012-04-26 | Hamilton Sundstrand Corporation | Door System |
US9573690B2 (en) * | 2011-09-06 | 2017-02-21 | Honeywell International Inc. | Thrust recovery outflow valve with a single bi-fold door and method of controlling aircraft cabin pressure |
US9067680B2 (en) * | 2011-09-29 | 2015-06-30 | The Boeing Company | Aircraft outflow valve |
FR3021626B1 (fr) * | 2014-05-28 | 2017-12-22 | Airbus Operations Sas | Equipement de fuselage formant une porte d'acces et comprenant une vanne de regulation d'echappement d'air de pressurisation |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3127130A (en) * | 1964-03-31 | Variable shaped airfoil | ||
DE1109530B (de) * | 1959-01-08 | 1961-06-22 | Rolls Royce | Senkrecht startendes Flugzeug |
US3045947A (en) * | 1959-04-24 | 1962-07-24 | Bertin & Cie | Ejectors, particularly for producing lift in aircraft |
GB998341A (en) * | 1963-07-02 | 1965-07-14 | Rolls Royce | Improvements in or relating to vertical lift jet engines |
FR1497434A (fr) * | 1966-10-25 | 1967-10-06 | Entwicklungsring Sued Gmbh | Dispositif de volet pour aile d'avion |
-
1967
- 1967-07-26 DE DEV34149A patent/DE1284851B/de active Pending
-
1968
- 1968-06-18 FR FR155381A patent/FR1579036A/fr not_active Expired
- 1968-07-19 US US746088A patent/US3486721A/en not_active Expired - Lifetime
- 1968-07-25 GB GB3559968A patent/GB1227804A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2279629A (en) * | 1993-06-25 | 1995-01-11 | Rolls Royce Plc | Vectorable nozzle for aircraft. |
GB2279629B (en) * | 1993-06-25 | 1997-03-05 | Rolls Royce Plc | Vectorable nozzle for aircraft |
Also Published As
Publication number | Publication date |
---|---|
FR1579036A (zh) | 1969-08-22 |
DE1284851B (de) | 1968-12-05 |
US3486721A (en) | 1969-12-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1227804A (zh) | ||
GB1284108A (en) | Improvements in or relating to aircraft wings | |
JPH05505992A (ja) | 垂直および短距離離着陸飛行機のための推進システム | |
GB1227316A (zh) | ||
GB638063A (en) | Improved means for braking aircraft | |
GB1294349A (en) | Improvements in or relating to high speed aircraft | |
US3921942A (en) | Rudder boundary layer control device | |
GB1083309A (en) | Variable-geometry aircraft | |
US2404956A (en) | Wing lift modification | |
US2070705A (en) | Airplane construction | |
GB1040814A (en) | A thrust reverser for a jet propulsion engine | |
US3997134A (en) | Fuselage tail jet engine thrust reverser | |
GB1181991A (en) | Aircraft Lift-Increasing Device | |
GB800770A (en) | Nozzle assemblies for jet propulsion apparatus | |
US2698149A (en) | Aircraft speed retarding device | |
GB759891A (en) | Lock for jet thrust reversing mechansim on aircraft | |
GB1381646A (en) | Aircraft with short take-off and landing characteristics | |
US3570767A (en) | Thrust reversing apparatus | |
GB1191311A (en) | Improvements relating to Variable-Geometry Aircraft | |
GB1014250A (en) | Improvements in ducted fan powerplants | |
GB1191720A (en) | Aerodynamic Obturator Device for a Variable Geometry Aircraft | |
US2679991A (en) | Closure for air ducts of aircraft | |
GB1220130A (en) | Flap system for controlling the orifice of an aircraft jet-lift engine | |
GB1140472A (en) | Articulated structure especially for jet propulsion nozzle | |
GB1073049A (en) | Closure device for the outlet of a jet lift engine passage |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PLNP | Patent lapsed through nonpayment of renewal fees |