BR112023025636A2 - Série de aeronaves, e, método para configurar uma aeronave - Google Patents
Série de aeronaves, e, método para configurar uma aeronaveInfo
- Publication number
- BR112023025636A2 BR112023025636A2 BR112023025636A BR112023025636A BR112023025636A2 BR 112023025636 A2 BR112023025636 A2 BR 112023025636A2 BR 112023025636 A BR112023025636 A BR 112023025636A BR 112023025636 A BR112023025636 A BR 112023025636A BR 112023025636 A2 BR112023025636 A2 BR 112023025636A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- series
- configuring
- wings
- core
- Prior art date
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
- B64C29/0025—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 fixed relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/20—Vertical take-off and landing [VTOL] 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L50/00—Electric propulsion with power supplied within the vehicle
- B60L50/50—Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells
- B60L50/60—Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells using power supplied by batteries
- B60L50/61—Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells using power supplied by batteries by batteries charged by engine-driven generators, e.g. series hybrid electric vehicles
-
- 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
- B64C39/00—Aircraft not otherwise provided for
- B64C39/08—Aircraft not otherwise provided for having multiple wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/12—Canard-type aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/30—Aircraft characterised by electric power plants
- B64D27/34—All-electric aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/30—Aircraft characterised by electric power plants
- B64D27/35—Arrangements for on-board electric energy production, distribution, recovery or storage
- B64D27/357—Arrangements for on-board electric energy production, distribution, recovery or storage using batteries
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D41/00—Power installations for auxiliary purposes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/40—Modular UAVs
-
- 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
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/11—Propulsion using internal combustion piston engines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
- B64U50/33—Supply or distribution of electrical power generated by combustion engines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
- B64U50/34—In-flight charging
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L2200/00—Type of vehicles
- B60L2200/10—Air crafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2211/00—Modular constructions of airplanes or helicopters
-
- 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
- B64U2101/61—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons for transporting passengers
-
- 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
- B64U2101/64—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons for parcel delivery or retrieval
-
- 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
-
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Sustainable Energy (AREA)
- Sustainable Development (AREA)
- Life Sciences & Earth Sciences (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Transmission Devices (AREA)
- Toys (AREA)
- Details Of Aerials (AREA)
- Retarders (AREA)
- Tires In General (AREA)
- Braking Arrangements (AREA)
Abstract
série de aeronaves, e, método para configurar uma aeronave. é descrita uma série de aeronaves conversíveis (1, 1') com um núcleo (100) com uma estrutura da aeronave (2) definindo um primeiro eixo geométrico (y); um primeiro, um segundo, um terceiro, um quarto, um quinto e um sexto rotores (20a, 20b, 21a, 21b, 22a, 22b) que são giratórios em torno dos respectivos primeiro, segundo, terceiro, quarto, quinto e sexto eixos geométricos (b, c, d, e, f, g) e operáveis independentemente um do outro, de modo a gerar respectivamente um primeiro, um segundo, um terceiro, um quarto, um quinto e um sexto valores de impulso (t1, t2, t3, t4 , t5, t6) independentes entre si; o núcleo (100) compreende primeira e segunda porções (11, 17) das respectivas meias-asas (3) e superfícies aerodinâmicas (9) e cada módulo (110, 120, 130, 140) compreende terceira e quarta porções (12, 18) das respectivas meias-asas (3) e superfícies aerodinâmicas (9).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP21180435.6A EP4105125B1 (en) | 2021-06-18 | 2021-06-18 | Series of convertible aircrafts capable of hovering and method for configuring a convertible aircraft capable of hovering |
PCT/IB2022/054836 WO2022263949A1 (en) | 2021-06-18 | 2022-05-24 | Series of convertible aircraft capable of hovering and method for configuring a convertible aircraft capable of hovering |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112023025636A2 true BR112023025636A2 (pt) | 2024-02-27 |
Family
ID=77249655
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112023025636A BR112023025636A2 (pt) | 2021-06-18 | 2022-05-24 | Série de aeronaves, e, método para configurar uma aeronave |
Country Status (10)
Country | Link |
---|---|
US (1) | US20240270415A1 (pt) |
EP (1) | EP4105125B1 (pt) |
JP (1) | JP2024522585A (pt) |
KR (1) | KR20240046426A (pt) |
CN (1) | CN117529434A (pt) |
AU (1) | AU2022294242A1 (pt) |
BR (1) | BR112023025636A2 (pt) |
CA (1) | CA3221628A1 (pt) |
IL (1) | IL309088A (pt) |
WO (1) | WO2022263949A1 (pt) |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5645250A (en) * | 1993-08-26 | 1997-07-08 | Gevers; David E. | Multi-purpose aircraft |
US7866610B2 (en) * | 2007-12-28 | 2011-01-11 | Samuel Hall Bousfield | Telescoping wing and airfoil control mechanism |
US20160236775A1 (en) * | 2015-02-18 | 2016-08-18 | Siniger LLC | Vertical takeoff and landing aircraft |
US10011349B2 (en) | 2016-08-31 | 2018-07-03 | Bell Helicopter Textron Inc. | Tiltrotor aircraft having rotatable wing extensions |
CN107176286B (zh) * | 2017-05-16 | 2023-08-22 | 华南理工大学 | 基于双涵道风扇动力系统的可折叠式固定翼垂直起降无人飞行器 |
EP3470332B1 (en) * | 2017-10-13 | 2020-04-22 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | A multirotor aircraft with an airframe and at least one wing |
IL263301B2 (en) | 2018-11-25 | 2023-09-01 | Israel Aerospace Ind Ltd | Aircraft and the method of operation of aircraft |
EP3656669B1 (en) * | 2018-11-26 | 2021-01-13 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | A vertical take-off and landing multirotor aircraft with at least eight thrust producing units |
US11387693B2 (en) * | 2018-12-12 | 2022-07-12 | Aurora Flight Sciences Corporation | Motor cooling system and method |
-
2021
- 2021-06-18 EP EP21180435.6A patent/EP4105125B1/en active Active
-
2022
- 2022-05-24 KR KR1020237042943A patent/KR20240046426A/ko unknown
- 2022-05-24 IL IL309088A patent/IL309088A/en unknown
- 2022-05-24 AU AU2022294242A patent/AU2022294242A1/en active Pending
- 2022-05-24 CN CN202280043305.3A patent/CN117529434A/zh active Pending
- 2022-05-24 JP JP2023575459A patent/JP2024522585A/ja active Pending
- 2022-05-24 CA CA3221628A patent/CA3221628A1/en active Pending
- 2022-05-24 BR BR112023025636A patent/BR112023025636A2/pt unknown
- 2022-05-24 US US18/568,384 patent/US20240270415A1/en active Pending
- 2022-05-24 WO PCT/IB2022/054836 patent/WO2022263949A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
KR20240046426A (ko) | 2024-04-09 |
JP2024522585A (ja) | 2024-06-21 |
AU2022294242A1 (en) | 2023-12-21 |
US20240270415A1 (en) | 2024-08-15 |
IL309088A (en) | 2024-02-01 |
CN117529434A (zh) | 2024-02-06 |
EP4105125B1 (en) | 2023-09-06 |
WO2022263949A1 (en) | 2022-12-22 |
CA3221628A1 (en) | 2022-12-22 |
EP4105125A1 (en) | 2022-12-21 |
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