GB898360A - Disc-type aircraft - Google Patents
Disc-type aircraftInfo
- Publication number
- GB898360A GB898360A GB13790/54A GB1379054A GB898360A GB 898360 A GB898360 A GB 898360A GB 13790/54 A GB13790/54 A GB 13790/54A GB 1379054 A GB1379054 A GB 1379054A GB 898360 A GB898360 A GB 898360A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- gases
- shutters
- annular
- ports
- 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
- 239000007789 gas Substances 0.000 abstract 7
- 238000002485 combustion reaction Methods 0.000 abstract 1
- 230000000694 effects Effects 0.000 abstract 1
- 239000002828 fuel tank Substances 0.000 abstract 1
- 230000003068 static effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/001—Flying saucers
Abstract
898,360. Aircraft. AVRO AIRCRAFT Ltd. May 10, 1955 [May 11, 1954], No. 13790/54. Class 4. In an aircraft comprising a generally lentiform structure as described in Specification 898,358, a group of gas turbine engines 37 is positioned between the aerofoil surfaces in a generally radial arrangement with their intakes directed towards the centre of the structure and their outlets directed towards its perimeter. Each engine 37 is attached to a segment 11 and is housed in a cylindrical shell 38 within an annular fuel tank 13 with the aid of mounting means 43; 40, 39. The air intakes of the engines register with openings in an annular plenum chamber between walls 14 and 21, to which air is admitted through ports 29 or through spring closed ports 27, Fig. 8 (not shown), during take-off when the ports 29 are closed to avoid admission of combustion products from the " gas cushion " on which the craft rises. It is stated that, because of this ground cushion effect, the aircraft rises vertically although it may have a weight greater than combined static thrust of all its engines; The gases from the engine outlets, are ejected from the periphery of the aircraft and their flow is controlled to control the aircraft similar to the manner described in Specification 898,359 and as described in Specification 898,362. In " take-off" position a selector handle 80 closes shutters 72 so that all gases are ejected downwardly through an annular nozzle 69, but during flight this handle is moved to allow gases to be ejected from upper and lower nozzles 68, 69, the annular shutters being then eccentrically disposed to close both nozzles at the front and to locate them open to a progressively increasing extent towards the rear. A control handle 79 causesdifferential movement of the shutters so that its movement to port reduces. the proportion of port flowing gases having a downward component and increases the proportion of starboard flowing gases havinga downward component. Rudder pedals 83 control shutters 82 for openings 81 to port and starboard. Specification 892,401 also is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB13790/54A GB898360A (en) | 1954-05-11 | 1954-05-11 | Disc-type aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB13790/54A GB898360A (en) | 1954-05-11 | 1954-05-11 | Disc-type aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB898360A true GB898360A (en) | 1962-06-06 |
Family
ID=10029420
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB13790/54A Expired GB898360A (en) | 1954-05-11 | 1954-05-11 | Disc-type aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB898360A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0304614A2 (en) * | 1987-08-24 | 1989-03-01 | von Kozierowski, Joachim | Flying object taking off and landing vertically |
-
1954
- 1954-05-11 GB GB13790/54A patent/GB898360A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0304614A2 (en) * | 1987-08-24 | 1989-03-01 | von Kozierowski, Joachim | Flying object taking off and landing vertically |
EP0304614A3 (en) * | 1987-08-24 | 1990-04-25 | Joachim Von Kozierowski | Centrifugal-force ring |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1012832A (en) | Improvements in or relating to vertical take off and landing aircraft | |
GB1228806A (en) | ||
GB898360A (en) | Disc-type aircraft | |
GB817507A (en) | Improvements in or relating to aircraft | |
GB877838A (en) | Improvements relating to gas turbine engine air intakes | |
GB1415509A (en) | Ducted fan gas turbine jet propulsion engines | |
GB1170476A (en) | Improvements in or relating to Ground-Effect Machines | |
GB788290A (en) | Improvements relating to aircraft | |
GB890703A (en) | An improved tiltable pod for jet power units on aircraft | |
GB1032274A (en) | Mounting of ducted fan turbine engines in the tail of an aircraft | |
GB898358A (en) | Vertical take-off aircraft | |
GB1092478A (en) | Vertical take off and landing jet aircraft | |
GB792993A (en) | Improvements in or relating to aircraft | |
GB883634A (en) | Improved gas turbine engine | |
GB851273A (en) | Aircraft air intakes | |
GB885659A (en) | Wingless supersonic aircraft | |
GB712682A (en) | Supersonic speed aircraft | |
GB1225004A (en) | Housings for aircraft jet engines | |
GB862476A (en) | Improvements in jet-propelled aircraft | |
GB909466A (en) | Vertical take-off aircraft | |
GB1018234A (en) | Improved high speed aircraft | |
GB1101042A (en) | Improvements in or relating to turbojet engines for vertical take-off and landing aircraft | |
GB794768A (en) | Jet propelling unit | |
GB745673A (en) | Variable-area propelling nozzle | |
GB849448A (en) | Improvements in or relating to nozzles for jet propulsion purposes |