GB1536859A - Aircraft - Google Patents
AircraftInfo
- Publication number
- GB1536859A GB1536859A GB52711/75A GB5271175A GB1536859A GB 1536859 A GB1536859 A GB 1536859A GB 52711/75 A GB52711/75 A GB 52711/75A GB 5271175 A GB5271175 A GB 5271175A GB 1536859 A GB1536859 A GB 1536859A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- rotatable
- dec
- wing
- suspension device
- 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
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C37/00—Convertible aircraft
- B64C37/02—Flying units formed by separate aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
-
- 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
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
- Vehicle Body Suspensions (AREA)
- Body Structure For Vehicles (AREA)
- Tires In General (AREA)
Abstract
1536859 Aircraft ALL AMERICAN INDUSTRIES Inc 23 Dec 1975 [23 Dec 1974] 52711/75 Addition to 1460822 Heading B7W In an aircraft comprising a rotatable wing device and a ballon structure structurally linked to the rotatable wing device for rotation therewith and having a control cab disposed below the wing chamber by a rotatable joint as claimed in parent Specification the suspension device connecting the cab to the balloon structure has its rotatable joint positioned substantially at the centre of the balloon structure, which is formed with a downwardly opening conical cavity whereby the suspension device may swing laterally.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/535,417 US3976265A (en) | 1973-05-07 | 1974-12-23 | Semibuoyant composite aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1536859A true GB1536859A (en) | 1978-12-20 |
Family
ID=24134110
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB52711/75A Expired GB1536859A (en) | 1974-12-23 | 1975-12-23 | Aircraft |
GB52710/75A Expired GB1536858A (en) | 1974-12-23 | 1975-12-23 | Aircraft |
GB52712/75A Expired GB1536860A (en) | 1974-12-23 | 1975-12-23 | Aircraft |
Family Applications After (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB52710/75A Expired GB1536858A (en) | 1974-12-23 | 1975-12-23 | Aircraft |
GB52712/75A Expired GB1536860A (en) | 1974-12-23 | 1975-12-23 | Aircraft |
Country Status (6)
Country | Link |
---|---|
AU (1) | AU507594B2 (en) |
BR (1) | BR7508443A (en) |
CA (1) | CA1016145A (en) |
DE (1) | DE2556907A1 (en) |
FR (1) | FR2295875A2 (en) |
GB (3) | GB1536859A (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4601444A (en) * | 1983-06-08 | 1986-07-22 | Bernard Lindenbaum | Aerial load-lifting system |
DE202005009621U1 (en) | 2005-06-21 | 2005-12-15 | Singer, Csaba | Hybrid aircraft e.g. helicopter, has two wings arranged laterally at casing and engaging together with casing by rotating around axis using rotating mechanism, rotation symmetric and mirror symmetrical configuration |
DE102013219881A1 (en) * | 2013-04-24 | 2014-10-30 | Cl Cargolifter Gmbh & Co. Kgaa | Aircraft comprising an aerostat system with a control unit and a drive unit and a functional unit |
CN118295450A (en) * | 2024-04-02 | 2024-07-05 | 浙江大学湖州研究院 | A control method for near-ground flight of a rotary-wing UAV |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1838248A (en) * | 1930-06-21 | 1931-12-29 | Joseph M Bourland | Airship |
US3166129A (en) * | 1961-02-27 | 1965-01-19 | Harvard J Bryan | Dual thrust propeller and controls for rotary winged aircraft |
US3856236A (en) * | 1973-05-07 | 1974-12-24 | All American Ind | Composite aircraft |
-
1975
- 1975-11-10 AU AU86486/75A patent/AU507594B2/en not_active Expired
- 1975-12-17 DE DE19752556907 patent/DE2556907A1/en active Granted
- 1975-12-19 BR BR7508443*A patent/BR7508443A/en unknown
- 1975-12-19 CA CA242,142A patent/CA1016145A/en not_active Expired
- 1975-12-22 FR FR7539386A patent/FR2295875A2/en active Granted
- 1975-12-23 GB GB52711/75A patent/GB1536859A/en not_active Expired
- 1975-12-23 GB GB52710/75A patent/GB1536858A/en not_active Expired
- 1975-12-23 GB GB52712/75A patent/GB1536860A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
AU8648675A (en) | 1977-05-19 |
AU507594B2 (en) | 1980-02-21 |
GB1536860A (en) | 1978-12-20 |
GB1536858A (en) | 1978-12-20 |
FR2295875A2 (en) | 1976-07-23 |
FR2295875B2 (en) | 1982-09-24 |
BR7508443A (en) | 1976-08-24 |
CA1016145A (en) | 1977-08-23 |
DE2556907C2 (en) | 1987-10-29 |
DE2556907A1 (en) | 1976-07-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |