BR112022023131A2 - Controle de aeronaves com capacidades de decolagem e pouso vertical - Google Patents
Controle de aeronaves com capacidades de decolagem e pouso verticalInfo
- Publication number
- BR112022023131A2 BR112022023131A2 BR112022023131A BR112022023131A BR112022023131A2 BR 112022023131 A2 BR112022023131 A2 BR 112022023131A2 BR 112022023131 A BR112022023131 A BR 112022023131A BR 112022023131 A BR112022023131 A BR 112022023131A BR 112022023131 A2 BR112022023131 A2 BR 112022023131A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- wings
- vertical take
- configuration
- folded configuration
- Prior art date
Links
Classifications
-
- 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
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
- G05D1/102—Simultaneous control of position or course in three dimensions specially adapted for aircraft specially adapted for vertical take-off of aircraft
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/10—Wings
- B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M1/00—Testing static or dynamic balance of machines or structures
- G01M1/12—Static balancing; Determining position of centre of gravity
- G01M1/122—Determining position of centre of gravity
- G01M1/125—Determining position of centre of gravity of aircraft
- G01M1/127—Determining position of centre of gravity of aircraft during the flight
-
- 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
- G05D1/20—Control system inputs
- G05D1/24—Arrangements for determining position or orientation
-
- 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
- G05D1/40—Control within particular dimensions
- G05D1/46—Control of position or course in three dimensions [3D]
-
- 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
- G05D1/40—Control within particular dimensions
- G05D1/49—Control of attitude, i.e. control of roll, pitch or yaw
- G05D1/495—Control of attitude, i.e. control of roll, pitch or yaw to ensure stability
- G05D1/496—Control of attitude, i.e. control of roll, pitch or yaw to ensure stability compensating for coupling between different axes of movement
-
- 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
- G05D1/60—Intended control result
- G05D1/617—Safety or protection, e.g. defining protection zones around obstacles or avoiding hazards
- G05D1/621—Safety or protection, e.g. defining protection zones around obstacles or avoiding hazards responding to weather conditions, e.g. storms or wind shear
-
- 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
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D2109/00—Types of controlled vehicles
- G05D2109/20—Aircraft, e.g. drones
- G05D2109/22—Aircraft, e.g. drones with fixed wings
- G05D2109/23—Vertical take-off and landing [VTOL] aircraft; Short take-off and landing [STOL, STOVL] aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D2109/00—Types of controlled vehicles
- G05D2109/20—Aircraft, e.g. drones
- G05D2109/22—Aircraft, e.g. drones with fixed wings
- G05D2109/23—Vertical take-off and landing [VTOL] aircraft; Short take-off and landing [STOL, STOVL] aircraft
- G05D2109/24—Convertible aircraft, e.g. tiltrotor aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Automation & Control Theory (AREA)
- Mechanical Engineering (AREA)
- Traffic Control Systems (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Automatic Assembly (AREA)
- Circuits Of Receivers In General (AREA)
- Transmission Devices (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US202063024693P | 2020-05-14 | 2020-05-14 | |
| PCT/US2021/032258 WO2021242535A2 (en) | 2020-05-14 | 2021-05-13 | Control of aircraft with vertical take-off and landing capabilities |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BR112022023131A2 true BR112022023131A2 (pt) | 2023-02-07 |
Family
ID=78745069
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BR112022023131A BR112022023131A2 (pt) | 2020-05-14 | 2021-05-13 | Controle de aeronaves com capacidades de decolagem e pouso vertical |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US12455574B2 (https=) |
| EP (1) | EP4149835A4 (https=) |
| JP (1) | JP7738337B2 (https=) |
| KR (1) | KR20230010733A (https=) |
| CN (1) | CN115916645A (https=) |
| AU (1) | AU2021278828A1 (https=) |
| BR (1) | BR112022023131A2 (https=) |
| CA (1) | CA3178662A1 (https=) |
| IL (1) | IL298177B1 (https=) |
| WO (1) | WO2021242535A2 (https=) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2621982A (en) * | 2022-08-24 | 2024-03-06 | Airbus Operations Ltd | Aircraft attitude controller and wing system |
| US20250346373A1 (en) * | 2024-05-10 | 2025-11-13 | Lockheed Martin Corporation | Airspeed driven tilt angle for electric tiltrotor aircraft |
| KR102802164B1 (ko) * | 2024-09-05 | 2025-05-02 | 주식회사 에이디시스템 | 접익형 수직 이착륙 무인 비행 장치 |
Family Cites Families (73)
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| US1793056A (en) | 1929-08-01 | 1931-02-17 | Cairns Dev Company | Folding wing |
| US1846992A (en) | 1931-05-05 | 1932-02-23 | Decker Virgil Cecil | Four winged aeroplane |
| US2572421A (en) | 1947-09-20 | 1951-10-23 | Jr Edmund Abel | Aircraft folding wing construction |
| US2674422A (en) | 1949-05-12 | 1954-04-06 | Pellarini Luigi | Folding wing for roadable aircraft |
| US3081964A (en) | 1958-12-08 | 1963-03-19 | Boeing Co | Airplanes for vertical and/or short take-off and landing |
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| US4691878A (en) * | 1985-11-06 | 1987-09-08 | The United States Of America As Represented By The Secretary Of The Navy | Tilt-rotor wing fold mechanism and method |
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| US5094412A (en) | 1989-10-13 | 1992-03-10 | Bell Helicopter Textron Inc. | Flaperon system for tilt rotor wings |
| BR9106696A (pt) | 1990-07-25 | 1993-06-08 | Sadleir Vtol Aircraft Co Pty L | Unidade de empuxo para aeronave do tipo vtol |
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| US9776715B2 (en) | 2002-10-01 | 2017-10-03 | Andrew H B Zhou | Amphibious vertical takeoff and landing unmanned device |
| WO2008065664A2 (en) * | 2006-11-30 | 2008-06-05 | Urban Aeronautics Ltd. | Flight control cockpit modes in ducted fan vtol vehicles |
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| WO2010012285A2 (en) | 2008-07-28 | 2010-02-04 | Fleck Fitness Concepts Gmbh | Combined air, water and road vehicle |
| US8366049B2 (en) | 2008-10-09 | 2013-02-05 | Abe Karem | Hover delivery of cabin payload in tilt-rotor and tilt-wing aircraft |
| RU2403177C1 (ru) | 2009-07-31 | 2010-11-10 | Общество С Ограниченной Ответственностью "Научно-Производственная Фирма "Сигма-Тс" | Самолет со складываемым крылом и устройство складывания крыла самолета |
| FR2948628B1 (fr) * | 2009-08-03 | 2012-02-03 | Airbus Operations Sas | Avion a controle en lacet par trainee differentielle |
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| US8800912B2 (en) | 2009-10-09 | 2014-08-12 | Oliver Vtol, Llc | Three wing, six-tilt propulsion unit, VTOL aircraft |
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| US11541987B2 (en) * | 2019-08-19 | 2023-01-03 | Textron Innovations Inc. | Aircraft with foldable tail |
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-
2021
- 2021-05-13 US US17/924,789 patent/US12455574B2/en active Active
- 2021-05-13 EP EP21814018.4A patent/EP4149835A4/en active Pending
- 2021-05-13 CA CA3178662A patent/CA3178662A1/en active Pending
- 2021-05-13 AU AU2021278828A patent/AU2021278828A1/en active Pending
- 2021-05-13 WO PCT/US2021/032258 patent/WO2021242535A2/en not_active Ceased
- 2021-05-13 JP JP2022568826A patent/JP7738337B2/ja active Active
- 2021-05-13 CN CN202180041497.XA patent/CN115916645A/zh active Pending
- 2021-05-13 BR BR112022023131A patent/BR112022023131A2/pt unknown
- 2021-05-13 KR KR1020227043918A patent/KR20230010733A/ko active Pending
- 2021-05-13 IL IL298177A patent/IL298177B1/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| US20230195143A1 (en) | 2023-06-22 |
| CN115916645A (zh) | 2023-04-04 |
| JP2023526056A (ja) | 2023-06-20 |
| JP7738337B2 (ja) | 2025-09-12 |
| AU2021278828A8 (en) | 2023-02-16 |
| AU2021278828A1 (en) | 2023-01-19 |
| WO2021242535A2 (en) | 2021-12-02 |
| US12455574B2 (en) | 2025-10-28 |
| IL298177A (en) | 2023-01-01 |
| IL298177B1 (en) | 2026-01-01 |
| WO2021242535A3 (en) | 2022-03-10 |
| EP4149835A4 (en) | 2024-04-17 |
| EP4149835A2 (en) | 2023-03-22 |
| KR20230010733A (ko) | 2023-01-19 |
| CA3178662A1 (en) | 2021-12-02 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B06W | Patent application suspended after preliminary examination (for patents with searches from other patent authorities) chapter 6.23 patent gazette] |