FR3083774B1 - VERTICAL TAKE-OFF AND LANDING AIRCRAFT - Google Patents
VERTICAL TAKE-OFF AND LANDING AIRCRAFT Download PDFInfo
- Publication number
- FR3083774B1 FR3083774B1 FR1856407A FR1856407A FR3083774B1 FR 3083774 B1 FR3083774 B1 FR 3083774B1 FR 1856407 A FR1856407 A FR 1856407A FR 1856407 A FR1856407 A FR 1856407A FR 3083774 B1 FR3083774 B1 FR 3083774B1
- Authority
- FR
- France
- Prior art keywords
- mass
- vertical take
- landing aircraft
- aircraft
- displacement means
- 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.)
- Active
Links
- 238000006073 displacement reaction Methods 0.000 abstract 3
- 230000005484 gravity Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C17/00—Aircraft stabilisation not otherwise provided for
- B64C17/02—Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus
-
- 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
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Transmission Devices (AREA)
- Testing Of Balance (AREA)
Abstract
L'invention concerne aéronef (2), à décollage et atterrissage verticaux dédié au transport d'une charge utile, comprenant : - au moins une masse ; - des moyens de déplacement (18) de ladite au moins une masse ; - des moyens de commande (20) des moyens de déplacement (18) de ladite au moins une masse en fonction de la position du centre de gravité ; caractérisé en ce que les moyens de déplacement sont (18) configurés pour permettre un positionnement de ladite au moins une masse selon au moins deux directions définissant entre elles un plan parallèle à un plan comprenant un axe de tangage (A') et un axe de roulis (B') de l'aéronef (2)The invention relates to an aircraft (2), with vertical take-off and landing dedicated to the transport of a payload, comprising: - at least one mass; - displacement means (18) of said at least one mass; - Control means (20) of the displacement means (18) of said at least one mass depending on the position of the center of gravity; characterized in that the displacement means are (18) configured to allow said at least one mass to be positioned in at least two directions defining between them a plane parallel to a plane comprising a pitch axis (A') and a roll (B') of the aircraft (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1856407A FR3083774B1 (en) | 2018-07-12 | 2018-07-12 | VERTICAL TAKE-OFF AND LANDING AIRCRAFT |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1856407 | 2018-07-12 | ||
FR1856407A FR3083774B1 (en) | 2018-07-12 | 2018-07-12 | VERTICAL TAKE-OFF AND LANDING AIRCRAFT |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3083774A1 FR3083774A1 (en) | 2020-01-17 |
FR3083774B1 true FR3083774B1 (en) | 2022-04-29 |
Family
ID=65031415
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1856407A Active FR3083774B1 (en) | 2018-07-12 | 2018-07-12 | VERTICAL TAKE-OFF AND LANDING AIRCRAFT |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3083774B1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11753146B1 (en) * | 2018-07-09 | 2023-09-12 | Pinto Geoffrey P | VTOL aircraft having modular payload |
US11535366B2 (en) * | 2020-03-25 | 2022-12-27 | Aurora Flight Sciences Corporation, a subsidiary of The Boeing Company | Shifting a center of gravity of an aircraft |
SG10202003837UA (en) * | 2020-04-27 | 2021-11-29 | F Drones Pte Ltd | Unmanned aircraft |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1883414A (en) * | 1928-05-31 | 1932-10-18 | Sears | Air vehicle |
US3709450A (en) * | 1970-12-11 | 1973-01-09 | Boeing Co | Cargo loading system for aircraft |
ES2508990B1 (en) * | 2013-04-16 | 2015-07-29 | Universidad De Sevilla | GRAVITY CENTER DISPLACEMENT COMPENSATION SYSTEM FOR LOAD HANDLING FOR UNTRIPULATED AIR SYSTEM EQUIPPED WITH ROBOTIC ARM. |
CN205311892U (en) * | 2015-12-30 | 2016-06-15 | 苏州妙旋无人机应用有限公司 | Controllable formula unmanned aerial vehicle of focus |
CN108163188B (en) * | 2018-01-12 | 2024-06-18 | 成都力钧科技有限责任公司 | Unmanned aerial vehicle combined system that can prune |
-
2018
- 2018-07-12 FR FR1856407A patent/FR3083774B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3083774A1 (en) | 2020-01-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR3083774B1 (en) | VERTICAL TAKE-OFF AND LANDING AIRCRAFT | |
EP3922565A3 (en) | Drone box | |
WO2017195026A3 (en) | Heads-up display with variable image plane | |
FR3022530B1 (en) | METHOD FOR CONTROLLING THE ORBIT OF A SATELLITE IN TERRESTRIAL ORBIT, SATELLITE AND SYSTEM FOR CONTROLLING THE ORBIT OF SUCH A SATELLITE | |
GB2546931A (en) | Projected interactive virtual desktop | |
FR3051774B1 (en) | DEVICE FOR PACKAGING A SHIMMING ELEMENT IN A CARTON | |
FR3032183B1 (en) | AEROPREINING SYSTEM FOR SATELLITE DESORBITATION | |
BR112015031515A2 (en) | apparatus and chamber for a cryostat | |
WO2019135791A3 (en) | Vertical takeoff and landing transportation system | |
BR112017023402A2 (en) | fluid dispenser for food supply area | |
FR3072337B3 (en) | . | |
FR3050717B1 (en) | RETRACTABLE WINDOW FOR AIRCRAFT CAB | |
FR3064323B1 (en) | METHOD FOR MANUFACTURING A PENDULUM DAMPING DEVICE AND DEVICE OBTAINED THEREBY | |
EP2733530A3 (en) | Device for compensating time dispersion applied to the generation of ultra-short light pulses | |
FR3067780B1 (en) | ROLLER SCREW MECHANISM | |
FR3068326B1 (en) | STORAGE DEVICE NEAR THE CEILING OF A TRANSPORT VEHICLE | |
FR3002360B1 (en) | METHOD AND DEVICE FOR DISPLAYING A DYNAMIC IMAGE USING AT LEAST ONE LASER SOURCE ON A MOBILE DEVICE, IN PARTICULAR AN AIRCRAFT. | |
ES2545803B1 (en) | Vision system for refueling in flight | |
RU2587318C2 (en) | Device for fixation or release of solid bodies to superlight aircraft | |
ES2568027T3 (en) | Vibration device for transporting a metal load to a fusion plant | |
FR3083526B1 (en) | PERFECTED FILLING SYSTEM | |
FR3048405B1 (en) | AUTONOMOUS MOTORIZED ROBOT FOR TRANSPORTING LOADS | |
FR3031585B1 (en) | METHOD AND DEVICE FOR AIDING THE PILOTAGE OF AN AIRCRAFT, AT LEAST ONE FLIGHT PHASE HAVING A PLURALITY OF STEPPING STEPS. | |
EP3028916A3 (en) | Gangway arrangement, intended to equip a public transport jointed vehicle, in particular a railway vehicle | |
FR3016156B1 (en) | STRUCTURE FOR REGULATING THE AEROACOUSTIC ENVIRONMENT IN AN AIRCRAFT ARMOR |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20200117 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
|
PLFP | Fee payment |
Year of fee payment: 4 |
|
PLFP | Fee payment |
Year of fee payment: 5 |
|
PLFP | Fee payment |
Year of fee payment: 6 |
|
PLFP | Fee payment |
Year of fee payment: 7 |