GB934169A - Aircraft - Google Patents
AircraftInfo
- Publication number
- GB934169A GB934169A GB16484/62A GB1648462A GB934169A GB 934169 A GB934169 A GB 934169A GB 16484/62 A GB16484/62 A GB 16484/62A GB 1648462 A GB1648462 A GB 1648462A GB 934169 A GB934169 A GB 934169A
- Authority
- GB
- United Kingdom
- Prior art keywords
- group
- valves
- passages
- deflectors
- aircraft
- 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
- 238000005096 rolling process Methods 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Air-Flow Control Members (AREA)
- Fluid-Pressure Circuits (AREA)
Abstract
934,169. Aircraft. L. Z. FREELAND. April 30, 1962, No. 16484/62. Class 4. An aircraft has a body 12, Fig. 1, having upper and lower panels 16, 18 defining an annular chamber 22 into which air is drawn through openings 48, 50, 52, 54 by air moving means 34, 36, 38, 40, a plurality of groups 58, 60, 62, 64 of ducts register with chamber 22, each duct branching into laterally and downwardly opening passages 88, 90, Fig. 4, with a control deflector 94 at the junction of passages 88, 90 to direct air from chamber 22 selectively to passages 88, 90. The panels 16, 18 are connected by walls 20, 26. The deflectors 94 of each group of duets have their shafts 96 coupled together by universal joints as have valves 100 and 102 in passages 88, 90. The position of deflectors 94 and valves 100, 102 is controlled by separate electric motors, Fig. 5 (not shown). For vertical take off, all the deflectors are adjusted to the Fig. 1 position. For forward flight the deflectors of group 64 are moved to the Fig. 4 position whilst the remainder are in the Fig. 1 position with the valves 102 of group 60 closed. Rolling moments are obtained by opening the valves 102 of one group 58 or 62 more than the other, and pitching is obtaining by opening the valves 102 of one group 60 or 64 more than the other. The equivalent of yaw control is obtained by permitting discharge through the passages of group 58, 62 which together with the discharge through group 64 produces a movement of the aircraft to the left or right.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB16484/62A GB934169A (en) | 1962-04-30 | 1962-04-30 | Aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB16484/62A GB934169A (en) | 1962-04-30 | 1962-04-30 | Aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB934169A true GB934169A (en) | 1963-08-14 |
Family
ID=10078187
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB16484/62A Expired GB934169A (en) | 1962-04-30 | 1962-04-30 | Aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB934169A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2004030783A2 (en) * | 2002-09-27 | 2004-04-15 | Dieter Wagels | Flying device |
-
1962
- 1962-04-30 GB GB16484/62A patent/GB934169A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2004030783A2 (en) * | 2002-09-27 | 2004-04-15 | Dieter Wagels | Flying device |
WO2004030783A3 (en) * | 2002-09-27 | 2004-09-30 | Dieter Wagels | Flying device |
CN100368044C (en) * | 2002-09-27 | 2008-02-13 | 迪特尔·瓦格尔斯 | Flying device |
US7465236B2 (en) | 2002-09-27 | 2008-12-16 | Dieter Wagels | Flying arrangement |
US7722470B2 (en) | 2002-09-27 | 2010-05-25 | Dieter Wagels | Flying arrangement |
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