GB1271102A - An aircraft with a wing pivotable about a spanwise axis - Google Patents
An aircraft with a wing pivotable about a spanwise axisInfo
- Publication number
- GB1271102A GB1271102A GB90069A GB90069A GB1271102A GB 1271102 A GB1271102 A GB 1271102A GB 90069 A GB90069 A GB 90069A GB 90069 A GB90069 A GB 90069A GB 1271102 A GB1271102 A GB 1271102A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- aircraft
- spar
- fuselage
- axis
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
Abstract
1,271,102. Convertible aircraft. WESTLAND AIRCRAFT Ltd. 22 Dec., 1969 [7 Jan., 1969], No. 900/69. Headings B7G and B7W. A convertible aircraft has a wing which supports at least two propulsion units and is pivotable about a spanwise axis at approximately the 25% chord of the wing, the axis being below the horizontal centreline of the fuselage. As shown in Fig. 4, the wing 12 is in the vertical position, the aircraft being ready for vertical flight, and the propulsion units are mounted below the undersurface of the wing 12 which is pivotable about axis 16 corresponding to the forward edge of the spar 17 underneath the floor 18 (Fig. 3) of the fuselage 11. The craft is convertible for forward flight by pivoting the wing so that the trailing edge of the spar 17 underneath the fuselage moves upwardly and rearwardly. Fig. 3 shows that the lines of thrust 20 of the propulsion units 14 pass through the centre of gravity 19 of aircraft. In Fig. 2 the wing 12 is set for forward flight. The part of the wing forward of the spar, 24, may fold back on the wing so that the undercarriage may be made shorter when the wing is in the vertical position (Fig. 5, not shown). The wing may fold about axes transverse to and on either side of the central portion 23 of the spar (Fig. 4) when the wings are in the vertical position, so that they lie parallel to the fuselage during storage.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB90069A GB1271102A (en) | 1969-01-07 | 1969-01-07 | An aircraft with a wing pivotable about a spanwise axis |
| DE19691965387 DE1965387A1 (en) | 1969-01-07 | 1969-12-30 | Transformation plane |
| FR7000204A FR2027858A1 (en) | 1969-01-07 | 1970-01-06 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB90069A GB1271102A (en) | 1969-01-07 | 1969-01-07 | An aircraft with a wing pivotable about a spanwise axis |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1271102A true GB1271102A (en) | 1972-04-19 |
Family
ID=9712458
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB90069A Expired GB1271102A (en) | 1969-01-07 | 1969-01-07 | An aircraft with a wing pivotable about a spanwise axis |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE1965387A1 (en) |
| FR (1) | FR2027858A1 (en) |
| GB (1) | GB1271102A (en) |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4296896A (en) * | 1979-08-27 | 1981-10-27 | Grumman Aerospace Corporation | VTOL Airplane |
| US5141176A (en) * | 1991-06-12 | 1992-08-25 | Grumman Aerospace Corporation | Tilt wing VTOL aircraft |
| WO2015143093A2 (en) | 2014-03-18 | 2015-09-24 | Joby Aviation, Inc. | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades |
| US10556700B2 (en) | 2014-03-18 | 2020-02-11 | Joby Aero, Inc. | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades |
| US10919641B2 (en) | 2018-07-02 | 2021-02-16 | Joby Aero, Inc | System and method for airspeed determination |
| US10960785B2 (en) | 2019-04-23 | 2021-03-30 | Joby Aero, Inc. | Battery thermal management system and method |
| US10988248B2 (en) | 2019-04-25 | 2021-04-27 | Joby Aero, Inc. | VTOL aircraft |
| US11230384B2 (en) | 2019-04-23 | 2022-01-25 | Joby Aero, Inc. | Vehicle cabin thermal management system and method |
| US11323214B2 (en) | 2018-09-17 | 2022-05-03 | Joby Aero, Inc. | Aircraft control system |
| US11407510B2 (en) | 2018-12-07 | 2022-08-09 | Joby Aero, Inc. | Rotary airfoil and design therefore |
| US11560221B2 (en) | 2014-03-18 | 2023-01-24 | Joby Aero, Inc. | Rotor deployment mechanism for electric vertical take-off and landing aircraft |
| US11747830B2 (en) | 2018-12-19 | 2023-09-05 | Joby Aero, Inc. | Vehicle navigation system |
| US11827347B2 (en) | 2018-05-31 | 2023-11-28 | Joby Aero, Inc. | Electric power system architecture and fault tolerant VTOL aircraft using same |
| US11940816B2 (en) | 2018-12-07 | 2024-03-26 | Joby Aero, Inc. | Aircraft control system and method |
-
1969
- 1969-01-07 GB GB90069A patent/GB1271102A/en not_active Expired
- 1969-12-30 DE DE19691965387 patent/DE1965387A1/en active Pending
-
1970
- 1970-01-06 FR FR7000204A patent/FR2027858A1/fr not_active Withdrawn
Cited By (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4296896A (en) * | 1979-08-27 | 1981-10-27 | Grumman Aerospace Corporation | VTOL Airplane |
| US5141176A (en) * | 1991-06-12 | 1992-08-25 | Grumman Aerospace Corporation | Tilt wing VTOL aircraft |
| US11613370B2 (en) | 2014-03-18 | 2023-03-28 | Joby Aero, Inc. | Aerodynamically efficient lightweight vertical take-off and landing aircraft with deployable rotors |
| US10625852B2 (en) | 2014-03-18 | 2020-04-21 | Joby Aero, Inc. | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades |
| EP4324740A3 (en) * | 2014-03-18 | 2024-04-10 | Joby Aero, Inc. | Erodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowable rotor blades |
| US10556700B2 (en) | 2014-03-18 | 2020-02-11 | Joby Aero, Inc. | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades |
| US11919652B2 (en) | 2014-03-18 | 2024-03-05 | Joby Aero, Inc. | Vertical take-off and landing aircraft with deployable rotors |
| US11866186B2 (en) | 2014-03-18 | 2024-01-09 | Joby Aero, Inc. | Aerodynamically efficient lightweight vertical take-off and landing aircraft |
| US11661202B2 (en) | 2014-03-18 | 2023-05-30 | Joby Aero, Inc. | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and box wing design |
| US11560221B2 (en) | 2014-03-18 | 2023-01-24 | Joby Aero, Inc. | Rotor deployment mechanism for electric vertical take-off and landing aircraft |
| WO2015143093A2 (en) | 2014-03-18 | 2015-09-24 | Joby Aviation, Inc. | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades |
| CN106573678B (en) * | 2014-03-18 | 2021-04-13 | 杰欧比飞行有限公司 | Aircraft suitable for vertical take-off and horizontal flight |
| CN106573678A (en) * | 2014-03-18 | 2017-04-19 | 杰欧比航空有限公司 | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades |
| EP3119673A4 (en) * | 2014-03-18 | 2017-11-15 | Joby Aviation, Inc. | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades |
| US11827347B2 (en) | 2018-05-31 | 2023-11-28 | Joby Aero, Inc. | Electric power system architecture and fault tolerant VTOL aircraft using same |
| US10919641B2 (en) | 2018-07-02 | 2021-02-16 | Joby Aero, Inc | System and method for airspeed determination |
| US11597532B2 (en) | 2018-07-02 | 2023-03-07 | Joby Aero, Inc. | System and method for airspeed determination |
| US11323214B2 (en) | 2018-09-17 | 2022-05-03 | Joby Aero, Inc. | Aircraft control system |
| US11940816B2 (en) | 2018-12-07 | 2024-03-26 | Joby Aero, Inc. | Aircraft control system and method |
| US11407510B2 (en) | 2018-12-07 | 2022-08-09 | Joby Aero, Inc. | Rotary airfoil and design therefore |
| US11747830B2 (en) | 2018-12-19 | 2023-09-05 | Joby Aero, Inc. | Vehicle navigation system |
| US10960785B2 (en) | 2019-04-23 | 2021-03-30 | Joby Aero, Inc. | Battery thermal management system and method |
| US11794905B2 (en) | 2019-04-23 | 2023-10-24 | Joby Aero, Inc. | Vehicle cabin thermal management system and method |
| US11548407B2 (en) | 2019-04-23 | 2023-01-10 | Joby Aero, Inc. | Battery thermal management system and method |
| US11230384B2 (en) | 2019-04-23 | 2022-01-25 | Joby Aero, Inc. | Vehicle cabin thermal management system and method |
| US11479146B2 (en) | 2019-04-23 | 2022-10-25 | Joby Aero, Inc. | Battery thermal management system and method |
| US10988248B2 (en) | 2019-04-25 | 2021-04-27 | Joby Aero, Inc. | VTOL aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| DE1965387A1 (en) | 1970-11-26 |
| FR2027858A1 (en) | 1970-10-02 |
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