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Found results for
 patents
1.
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Vertical take off aircraft
| Application Number |
15896894 |
| Grant Number |
10486808 |
| Status |
In Force |
| Filing Date |
2018-02-14 |
| First Publication Date |
2018-08-23 |
| Grant Date |
2019-11-26 |
| Owner |
MARTIN UAV, LLC (USA)
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| Inventor |
Morris, Stephen
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Abstract
An aircraft includes a fuselage, a wing, a ducted fan and a controller. The wing and the ducted fan are coupled to the fuselage. The controller is operable to control the aircraft in a vertical flight mode, a horizontal flight mode, and transition the aircraft from the vertical flight mode to the horizontal flight mode.
IPC Classes ?
- B64C 29/00 - Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C 29/02 - 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
- B64C 11/00 - Propellers, e.g. of ducted typeFeatures common to propellers and rotors for rotorcraft
- G05D 1/08 - Control of attitude, i.e. control of roll, pitch, or yaw
- G05D 1/10 - Simultaneous control of position or course in three dimensions
- B64C 9/00 - Adjustable control surfaces or members, e.g. rudders
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2.
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Vertical take off aircraft
| Application Number |
15402784 |
| Grant Number |
09902494 |
| Status |
In Force |
| Filing Date |
2017-01-10 |
| First Publication Date |
2017-10-19 |
| Grant Date |
2018-02-27 |
| Owner |
MARTIN UAV, LLC (USA)
|
| Inventor |
Morris, Stephen
|
Abstract
An aircraft includes a fuselage, a wing, a ducted fan and a controller. The wing and the ducted fan are coupled to the fuselage. The controller is operable to control the aircraft in a vertical flight mode, a horizontal flight mode, and transition the aircraft from the vertical flight mode to the horizontal flight mode.
IPC Classes ?
- B64C 29/00 - Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C 29/02 - 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
- G05D 1/10 - Simultaneous control of position or course in three dimensions
- G05D 1/08 - Control of attitude, i.e. control of roll, pitch, or yaw
- B64C 11/00 - Propellers, e.g. of ducted typeFeatures common to propellers and rotors for rotorcraft
- B64C 9/00 - Adjustable control surfaces or members, e.g. rudders
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3.
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Vertical take off aircraft
| Application Number |
15152413 |
| Grant Number |
09828090 |
| Status |
In Force |
| Filing Date |
2016-05-11 |
| First Publication Date |
2017-03-02 |
| Grant Date |
2017-11-28 |
| Owner |
MARTIN UAV, LLC (USA)
|
| Inventor |
Morris, Stephen
|
Abstract
An aircraft includes a fuselage, a wing, a ducted fan and a controller. The wing and the ducted fan are coupled to the fuselage. The controller is operable to control the aircraft in a vertical flight mode, a horizontal flight more, and transition the aircraft from the vertical flight mode to the horizontal flight mode.
IPC Classes ?
- B64C 29/00 - Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C 29/02 - 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
- B64C 11/00 - Propellers, e.g. of ducted typeFeatures common to propellers and rotors for rotorcraft
- G05D 1/08 - Control of attitude, i.e. control of roll, pitch, or yaw
- G05D 1/10 - Simultaneous control of position or course in three dimensions
- B64C 9/00 - Adjustable control surfaces or members, e.g. rudders
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4.
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VERTICAL TAKE OFF AIRCRAFT
| Application Number |
US2016049086 |
| Publication Number |
2017/035503 |
| Status |
In Force |
| Filing Date |
2016-08-26 |
| Publication Date |
2017-03-02 |
| Owner |
MARTIN UAV, LLC (USA)
|
| Inventor |
Morris, Stephen
|
Abstract
An aircraft includes a fuselage, a wing, a ducted fan and a controller. The wing and the ducted fan are coupled to the fuselage. The controller is operable to control the aircraft in a vertical flight mode, a horizontal flight more, and transition the aircraft from the vertical flight mode to the horizontal flight mode.
IPC Classes ?
- B64C 29/02 - 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
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5.
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Vertical take off aircraft
| Application Number |
15152416 |
| Grant Number |
09567071 |
| Status |
In Force |
| Filing Date |
2016-05-11 |
| First Publication Date |
2017-02-14 |
| Grant Date |
2017-02-14 |
| Owner |
MARTIN UAV, LLC (USA)
|
| Inventor |
Morris, Stephen
|
Abstract
An aircraft includes a fuselage, a wing, a ducted fan and a controller. The wing and the ducted fan are coupled to the fuselage. The controller is operable to control the aircraft in a vertical flight mode, a horizontal flight more, and transition the aircraft from the vertical flight mode to the horizontal flight mode.
IPC Classes ?
- B64C 29/00 - Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C 29/02 - 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
- G05D 1/08 - Control of attitude, i.e. control of roll, pitch, or yaw
- G05D 1/10 - Simultaneous control of position or course in three dimensions
- B64C 11/00 - Propellers, e.g. of ducted typeFeatures common to propellers and rotors for rotorcraft
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