GB920894A - Improvements in or relating to aircraft - Google Patents
Improvements in or relating to aircraftInfo
- Publication number
- GB920894A GB920894A GB21240/61A GB2124061A GB920894A GB 920894 A GB920894 A GB 920894A GB 21240/61 A GB21240/61 A GB 21240/61A GB 2124061 A GB2124061 A GB 2124061A GB 920894 A GB920894 A GB 920894A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- flap
- engines
- pair
- shaft
- 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
- 238000009434 installation Methods 0.000 abstract 1
- 230000001141 propulsive effect Effects 0.000 abstract 1
- 230000001105 regulatory effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V3/00—Land vehicles, waterborne vessels, or aircraft, adapted or modified to travel on air cushions
- B60V3/08—Aircraft, e.g. air-cushion alighting-gear therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
- B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
- B64C21/06—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for sucking
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/08—Influencing air flow over aircraft surfaces, not otherwise provided for using Magnus effect
-
- 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
- B64C29/0025—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 the propellers being fixed relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/04—Boundary layer controls by actively generating fluid flow
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
920,894. Propelling aircraft. DORNIERWERKE G.m.b.H. June 13, 1961 [July 16, 1960; Aug. 20, 1960], No. 21240/61. Class 4. A power plant installation in an aircraft comprises a pair of engines 3 each separately connected through gearing and a freewheel device 4 to drive a continuous spanwise shaft 2 upon which are mounted transverse flow blowers 1 located symmetrically on both sides of the aircraft within the wing profile. The air outlet opening associated with each blower is provided with a flap 5, the flaps being pivotally interconnected by a shaft 6 connected by linkage 9 to a flap-adjusting mechanism 7, whereby lift and propulsive thrust may be regulated. There may be more than one pair of blowers and engines.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DED0033798 | 1960-07-16 | ||
DED0034057 | 1960-08-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB920894A true GB920894A (en) | 1963-03-13 |
Family
ID=25971117
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB21240/61A Expired GB920894A (en) | 1960-07-16 | 1961-06-13 | Improvements in or relating to aircraft |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1293888A (en) |
GB (1) | GB920894A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2014209198A1 (en) * | 2013-06-25 | 2014-12-31 | Försvarets Materielverk | Propulsion system for an aerial vehicle |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT1067613B (en) * | 1976-08-09 | 1985-03-16 | Bizzarri Alfredo | AIR INTAKE AND PUSHING SYSTEM APPLICABLE FOR SUPPORTING AND PROPULSION OF AIRCRAFT FOR PUSHING AND BRAKING OF RESTRICT AND NAVAL VEHICLES AND FOR OTHER APPLICATIONS |
-
1961
- 1961-06-13 GB GB21240/61A patent/GB920894A/en not_active Expired
- 1961-06-30 FR FR7182A patent/FR1293888A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2014209198A1 (en) * | 2013-06-25 | 2014-12-31 | Försvarets Materielverk | Propulsion system for an aerial vehicle |
US9789959B2 (en) | 2013-06-25 | 2017-10-17 | Forsvarets Materielverk | Propulsion system for an aerial vehicle |
Also Published As
Publication number | Publication date |
---|---|
FR1293888A (en) | 1962-05-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1066360A (en) | Aircraft | |
GB924078A (en) | Aircraft | |
US3029044A (en) | Return flow vertical lift airplane | |
GB895590A (en) | Improvements relating to aircraft for vertical take-off and landing | |
GB1108454A (en) | Improvements in or relating to gas turbine engines | |
GB978574A (en) | Improvements in aircraft | |
DE59404344D1 (en) | AIRCRAFT | |
GB914108A (en) | Improvements in thrust diverting means for vtol and stol aircraft | |
GB945078A (en) | Improvements in or relating to wing-fan doors of vertical take-off aircraft | |
GB1207149A (en) | Improvements in or relating to aircraft | |
GB920894A (en) | Improvements in or relating to aircraft | |
GB1166396A (en) | Improvements in Power Plant with Thrust Reverser. | |
GB1215843A (en) | A ducted fan propulsion unit | |
GB862032A (en) | Aircraft | |
FR2452426A1 (en) | Lifting body aircraft for vertical or STOL service - has movable flap on trailing edge and tiltable propeller | |
GB554425A (en) | Aircraft and method of propulsion | |
FR2303709A2 (en) | Vertical take off and landing aircraft - has lifting rotor within fuselage with hinged deflection shutters | |
GB1441669A (en) | Aerodynamic lift cell | |
GB942339A (en) | Improvements in vtol aircraft | |
GB1345513A (en) | Gas cushion vehicle | |
GB888943A (en) | Improvements in or relating to fan units | |
GB886111A (en) | Aircraft | |
CLARK | Ejector blown lift/cruise flap wind tunnel investigation[Final Report, Dec. 1971- May 1973] | |
GB941904A (en) | Improvements relating to aircraft having hinged wings, flaps, fins or like parts with control surfaces | |
GB1441516A (en) | Fan jet aircraft having means for controlling rolling motion |