FR2824924B1 - Dispositif de pilotage pour aeronef a decollage vertical - Google Patents
Dispositif de pilotage pour aeronef a decollage verticalInfo
- Publication number
- FR2824924B1 FR2824924B1 FR0106380A FR0106380A FR2824924B1 FR 2824924 B1 FR2824924 B1 FR 2824924B1 FR 0106380 A FR0106380 A FR 0106380A FR 0106380 A FR0106380 A FR 0106380A FR 2824924 B1 FR2824924 B1 FR 2824924B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- steering device
- vertical take
- take
- vertical
- 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 - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/52—Tilting of rotor bodily relative to fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
- B64U30/26—Ducted or shrouded rotors
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0106380A FR2824924B1 (fr) | 2001-05-15 | 2001-05-15 | Dispositif de pilotage pour aeronef a decollage vertical |
PCT/FR2002/001594 WO2002093283A1 (fr) | 2001-05-15 | 2002-05-13 | Dispositif de pilotage pour aeronef a decollage vertical |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0106380A FR2824924B1 (fr) | 2001-05-15 | 2001-05-15 | Dispositif de pilotage pour aeronef a decollage vertical |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2824924A1 FR2824924A1 (fr) | 2002-11-22 |
FR2824924B1 true FR2824924B1 (fr) | 2003-09-05 |
Family
ID=8863288
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0106380A Expired - Fee Related FR2824924B1 (fr) | 2001-05-15 | 2001-05-15 | Dispositif de pilotage pour aeronef a decollage vertical |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR2824924B1 (fr) |
WO (1) | WO2002093283A1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2980117B1 (fr) * | 2011-09-16 | 2014-06-13 | Francois Viguier | Engin volant a decollage et atterrissage vertical a rotor contrarotatif |
CN106314771B (zh) * | 2015-06-27 | 2019-10-29 | 深圳市大疆创新科技有限公司 | 飞行器及其动力装置 |
CN113022845B (zh) * | 2021-05-27 | 2021-08-10 | 北京航空航天大学 | 一种共轴倾转旋翼飞行器及其组合的薄膜类飞行器 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2863621A (en) * | 1957-04-12 | 1958-12-09 | John W Davis | Vertical and horizontal flight aircraft |
US4958786A (en) * | 1987-02-03 | 1990-09-25 | Sumitomo Precision Products Co., Ltd. | Active control mechanism for a helicopter |
US6170778B1 (en) * | 1999-04-22 | 2001-01-09 | Sikorsky Aircraft Corporation | Method of reducing a nose-up pitching moment on a ducted unmanned aerial vehicle |
-
2001
- 2001-05-15 FR FR0106380A patent/FR2824924B1/fr not_active Expired - Fee Related
-
2002
- 2002-05-13 WO PCT/FR2002/001594 patent/WO2002093283A1/fr not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
FR2824924A1 (fr) | 2002-11-22 |
WO2002093283A1 (fr) | 2002-11-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20130131 |