GB1163853A - Rotary Wing Aircraft - Google Patents
Rotary Wing AircraftInfo
- Publication number
- GB1163853A GB1163853A GB31799/67A GB3179967A GB1163853A GB 1163853 A GB1163853 A GB 1163853A GB 31799/67 A GB31799/67 A GB 31799/67A GB 3179967 A GB3179967 A GB 3179967A GB 1163853 A GB1163853 A GB 1163853A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- aircraft
- tracks
- blades
- pipes
- 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
- 125000004122 cyclic group Chemical group 0.000 abstract 2
- 239000012530 fluid Substances 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)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1,163,853. Rotary wing aircraft with aircushion undercarriage. VLM CORP. 11 July, 1967 [13 July, 1966; 16 June, 1967], No. 31799/67. Headings B7G, B7K and B7W. A rotary wing aircraft 10 (which may have a spherical fuselage) comprises aerofoils 16, 302 (which may be carried by wing members 70, 72) movable along annular tracks 12 and 14, 303 and 306 the outer tracks supporting the outer ends of the aerofoils which are driven by fluid pressure (e.g. by air jets from nozzles supplied from a compressor 56 via a reservoir 54 and pipes 26 or 32 and 40 or 42, impinging on a row of blades in the outer ring member 72). The exhaust air from these jets may pass out through jets 44 adjusted to prevent, or adjustable to control yaw motion. The ring members 70, 72, 328 may be supported in the tracks 12, 14, 303, 304 by air bearings. The horizontal motion of the aircraft 10 is controlled either by the tracks 12 and 14, Fig. 1, being held rigidly by pipes 26 and 32 in a plane tilted by jacks 20 and 21 or by blades 302, Fig. 17, being pivoted so that the planes containing them and the pipes 305 are free to cone, the blades having adjustable cyclic pitch change. Blade pitch control of the latter form, Figs. 19 and 21, comprises in the blade 302, a tube 350 having a cam slot 351 engaged by a follower 352 attached to a mass 353 slidable radially in the tube. The mass 353 is restrained from radially outward movement by a spring 354 in a cup 355 restrained by a cable 340. Rotor speed increase compresses the spring 354 increasing the collective pitch. The cable 340 passes through the blade to a ring 341 rotatable on an air bearing about a ring 342 which can be made eccentric of the aircraft by differential inflation of four balloons 348 causing cyclic pitch change. There may be a parachute in the top of the fuselage. The aircraft may have an air cushion undercarriage comprising a toroid 64, Fig. 3, containing a space below the fuselage 18 filled with air from the reservoir 54. The toroid 64 may be inflated to act as a buoyancy tank and may be assisted in this by a further inflated toroid (shown dotted).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US56480166A | 1966-07-13 | 1966-07-13 | |
US64659867A | 1967-06-16 | 1967-06-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1163853A true GB1163853A (en) | 1969-09-10 |
Family
ID=27073666
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB31799/67A Expired GB1163853A (en) | 1966-07-13 | 1967-07-11 | Rotary Wing Aircraft |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE1531466A1 (en) |
GB (1) | GB1163853A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2283720A (en) * | 1993-11-09 | 1995-05-17 | Derek Anthony Harris | Vertical take-off flying machine. |
US5993401A (en) * | 1995-12-25 | 1999-11-30 | Matsushita Electric Works, Ltd. | Relax inducing device with heartbeat detection unit |
CN104229132A (en) * | 2013-06-05 | 2014-12-24 | 倪明旺 | A transmission system of a coaxial propeller-reversing spherical aircraft |
CN110282133A (en) * | 2017-08-15 | 2019-09-27 | 郑小燕 | The flat winged method of flying saucer and wing ring machine |
CN113997738A (en) * | 2021-12-03 | 2022-02-01 | 江苏集萃智能制造技术研究所有限公司 | Spherical amphibious robot platform |
-
1967
- 1967-07-11 DE DE19671531466 patent/DE1531466A1/en active Pending
- 1967-07-11 GB GB31799/67A patent/GB1163853A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2283720A (en) * | 1993-11-09 | 1995-05-17 | Derek Anthony Harris | Vertical take-off flying machine. |
US5993401A (en) * | 1995-12-25 | 1999-11-30 | Matsushita Electric Works, Ltd. | Relax inducing device with heartbeat detection unit |
CN104229132A (en) * | 2013-06-05 | 2014-12-24 | 倪明旺 | A transmission system of a coaxial propeller-reversing spherical aircraft |
CN104229132B (en) * | 2013-06-05 | 2018-09-25 | 吴嘉馨 | Coaxial anti-paddle spherical aircraft transmission system |
CN110282133A (en) * | 2017-08-15 | 2019-09-27 | 郑小燕 | The flat winged method of flying saucer and wing ring machine |
CN113997738A (en) * | 2021-12-03 | 2022-02-01 | 江苏集萃智能制造技术研究所有限公司 | Spherical amphibious robot platform |
CN113997738B (en) * | 2021-12-03 | 2023-09-22 | 江苏集萃智能制造技术研究所有限公司 | Spherical amphibious robot platform |
Also Published As
Publication number | Publication date |
---|---|
DE1531466A1 (en) | 1969-08-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PLNP | Patent lapsed through nonpayment of renewal fees |