GB201307739D0 - Aircraft for vertical take-off and landing with hinged and bendable wings - Google Patents
Aircraft for vertical take-off and landing with hinged and bendable wingsInfo
- Publication number
- GB201307739D0 GB201307739D0 GBGB1307739.1A GB201307739A GB201307739D0 GB 201307739 D0 GB201307739 D0 GB 201307739D0 GB 201307739 A GB201307739 A GB 201307739A GB 201307739 D0 GB201307739 D0 GB 201307739D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- landing
- aircraft
- hinged
- vertical take
- bendable wings
- 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.)
- Ceased
Links
Classifications
-
- 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
- B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/80—Vertical take-off or landing, e.g. using rockets
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB1307739.1A GB201307739D0 (en) | 2013-04-30 | 2013-04-30 | Aircraft for vertical take-off and landing with hinged and bendable wings |
PCT/EP2014/058765 WO2014177589A1 (en) | 2013-04-30 | 2014-04-29 | Aircraft for vertical take-off and landing with hinged and bendable wings |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB1307739.1A GB201307739D0 (en) | 2013-04-30 | 2013-04-30 | Aircraft for vertical take-off and landing with hinged and bendable wings |
Publications (1)
Publication Number | Publication Date |
---|---|
GB201307739D0 true GB201307739D0 (en) | 2013-06-12 |
Family
ID=48627027
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GBGB1307739.1A Ceased GB201307739D0 (en) | 2013-04-30 | 2013-04-30 | Aircraft for vertical take-off and landing with hinged and bendable wings |
Country Status (2)
Country | Link |
---|---|
GB (1) | GB201307739D0 (en) |
WO (1) | WO2014177589A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9550567B1 (en) | 2014-10-27 | 2017-01-24 | Amazon Technologies, Inc. | In-flight reconfigurable hybrid unmanned aerial vehicle |
CN104443390A (en) * | 2014-11-13 | 2015-03-25 | 南京航空航天大学 | Aquatic sport airplane with rotatable wings |
US10252798B2 (en) * | 2017-04-27 | 2019-04-09 | Pterodynamics | Vertical takeoff and landing airframe |
IL253667B (en) * | 2017-07-25 | 2022-09-01 | Michael Bar | Empennage |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2479125A (en) * | 1943-10-06 | 1949-08-16 | Lloyd H Leonard | Variable attitude helicopter airplane |
GB639947A (en) * | 1946-09-10 | 1950-07-12 | Roger Aime Robert | Aircraft |
US2866608A (en) * | 1955-05-18 | 1958-12-30 | Lloyd H Leonard | Vertical-take-off type aircraft with jet driven rotor system |
US3210025A (en) * | 1961-08-07 | 1965-10-05 | Kaman Aircraft Corp | Empennage construction for a space missile |
GB1003057A (en) * | 1963-02-20 | 1965-09-02 | Edward Burke Wilford | Improvements in and relating to vertical take-off aircraft |
-
2013
- 2013-04-30 GB GBGB1307739.1A patent/GB201307739D0/en not_active Ceased
-
2014
- 2014-04-29 WO PCT/EP2014/058765 patent/WO2014177589A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2014177589A1 (en) | 2014-11-06 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3057867A4 (en) | Vertical take-off and landing aircraft | |
GB201214887D0 (en) | Aircraft for vertical take-off and landing with two wing arrangement | |
EP2899122A4 (en) | Vertical takeoff and landing aircraft | |
HK1244762A1 (en) | High speed multi-rotor vertical takeoff and landing aircraft | |
IL260120B (en) | Aircraft with vertical takeoff and landing and its operating process | |
ZA201701274B (en) | Vertical take-off and landing aircraft | |
IL239205A0 (en) | Vertical takeoff and landing aircraft | |
EP3458356A4 (en) | Vertical takeoff and landing aircraft with tilted-wing configurations | |
PL3024726T3 (en) | Vertical take-off and landing aerial vehicle | |
PL3172130T3 (en) | Aircraft with wing-borne flight mode and hover flight mode | |
EP2945858A4 (en) | Aircraft fuselage | |
DK2991897T3 (en) | VERTICAL TAKE OFF AND LANDING (VTOL) AIRCRAFT | |
GB201301748D0 (en) | Aircraft for Vertical Take-off and Landing with a Wing Arrangement comprising an extendible lift increasing system | |
EP2979977A4 (en) | Fuel tank, main wings, aircraft fuselage, aircraft, and moving body | |
EP2727833A4 (en) | Vertical takeoff and landing aircraft | |
GB2506464B (en) | An Aircraft Powerplant | |
EP2826710A4 (en) | Vertical take-off and landing device | |
SG2013063532A (en) | In-flight computing device for aircraft cabin crew | |
GB201305461D0 (en) | Lift-reducing apparatus for aircraft wings | |
EP3024729A4 (en) | Aircraft engine pylon | |
EP2998221A4 (en) | Vertical take-off and landing aircraft | |
GB2504369B (en) | Aircraft wing | |
EP2979976A4 (en) | Fuel tank, main wings, aircraft fuselage, aircraft, and moving body | |
EP2987721A4 (en) | Nose cone structure for pylon of aircraft with wing-hung layout | |
GB201307739D0 (en) | Aircraft for vertical take-off and landing with hinged and bendable wings |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AT | Applications terminated before publication under section 16(1) |