MX2018002328A - Una unidad de produccion de empuje con al menos dos ensambles de rotor y una carcasa. - Google Patents
Una unidad de produccion de empuje con al menos dos ensambles de rotor y una carcasa.Info
- Publication number
- MX2018002328A MX2018002328A MX2018002328A MX2018002328A MX2018002328A MX 2018002328 A MX2018002328 A MX 2018002328A MX 2018002328 A MX2018002328 A MX 2018002328A MX 2018002328 A MX2018002328 A MX 2018002328A MX 2018002328 A MX2018002328 A MX 2018002328A
- Authority
- MX
- Mexico
- Prior art keywords
- shrouding
- rotor assemblies
- producing unit
- thrust producing
- thrust
- Prior art date
Links
- 230000000712 assembly Effects 0.000 title abstract 3
- 238000000429 assembly Methods 0.000 title abstract 3
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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/001—Shrouded propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
- B64C11/48—Units of two or more coaxial propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/70—Constructional aspects of the UAV body
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/13—Propulsion using external fans or propellers
- B64U50/14—Propulsion using external fans or propellers ducted or shrouded
-
- 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
- B64D2241/00—NACA type air intakes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/20—Constructional aspects of UAVs for noise reduction
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Motor Or Generator Cooling System (AREA)
- Switches With Compound Operations (AREA)
- Moulding By Coating Moulds (AREA)
- Storage Of Web-Like Or Filamentary Materials (AREA)
- Coiling Of Filamentary Materials In General (AREA)
- Toys (AREA)
- Wind Motors (AREA)
- Automatic Assembly (AREA)
Abstract
La invención se refiere a una unidad de producción de empuje 3d para producir empuje en una dirección predeterminada, que comprende al menos dos ensambles de rotor 7d, 8d y una carcasa 6d que acomoda como mucho uno de dichos al menos dos ensambles de rotor 7d, 8d, en donde la carcasa 6d define un ducto de aire cilíndrico 20 que está delimitado axialmente por una región de entrada de aire 20e y una región de salida de aire 20f, y en donde la región de entrada de aire 20e exhibe en dirección circunferencial del ducto de aire cilíndrico 20 una geometría ondulada.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP17400008.3A EP3366586B1 (en) | 2017-02-27 | 2017-02-27 | A thrust producing unit with at least two rotor assemblies and a shrouding |
Publications (1)
Publication Number | Publication Date |
---|---|
MX2018002328A true MX2018002328A (es) | 2018-11-09 |
Family
ID=58410234
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2018002328A MX2018002328A (es) | 2017-02-27 | 2018-02-23 | Una unidad de produccion de empuje con al menos dos ensambles de rotor y una carcasa. |
Country Status (8)
Country | Link |
---|---|
US (1) | US11220325B2 (es) |
EP (1) | EP3366586B1 (es) |
JP (1) | JP6516888B2 (es) |
KR (1) | KR102049969B1 (es) |
CN (1) | CN108502151B (es) |
BR (1) | BR102018003220B1 (es) |
MX (1) | MX2018002328A (es) |
SG (1) | SG10201800731PA (es) |
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CN107614379A (zh) | 2015-05-25 | 2018-01-19 | 多特瑞尔技术有限公司 | 用于飞行器的护罩 |
JP2020530913A (ja) | 2017-07-24 | 2020-10-29 | ドテレル テクノロジーズ リミテッド | シュラウド |
WO2019210128A2 (en) * | 2018-04-27 | 2019-10-31 | Aai Corporation | Variable pitch rotor assembly for electrically driven vectored thrust aircraft applications |
AU2019271730A1 (en) | 2018-05-16 | 2020-12-24 | Dotterel Technologies Limited | Systems and methods for audio capture |
EP3581491B1 (en) | 2018-06-13 | 2020-06-24 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | A multirotor aircraft with a thrust producing unit that comprises an aerodynamically optimized shrouding |
US10822080B2 (en) * | 2018-06-28 | 2020-11-03 | The Boeing Company | Aircraft and methods of performing tethered and untethered flights using aircraft |
US11027836B2 (en) * | 2018-07-13 | 2021-06-08 | The Boeing Company | Rotorcraft with canted coaxial rotors |
BR112021001262A2 (pt) * | 2018-07-23 | 2021-04-20 | Airgility, Inc. | plataforma de veículo de sistema de partida, e, método de operação de uma plataforma de veículo de sistema de partida . |
JP7068126B2 (ja) * | 2018-10-01 | 2022-05-16 | トヨタ自動車株式会社 | 異常検出装置および制御装置 |
EP3730404B1 (en) * | 2019-04-23 | 2021-08-18 | LEONARDO S.p.A. | Vertical take-off and landing aircraft and related control method |
CN113784890B (zh) | 2019-04-26 | 2024-02-27 | 阿尔捷利集团公司 | 混合旋翼式飞行器 |
US11673657B2 (en) * | 2019-05-03 | 2023-06-13 | The Boeing Company | Multi-rotor rotorcraft |
KR102366194B1 (ko) * | 2020-03-26 | 2022-02-24 | 주식회사 풍산 | 동축 로터형 비행체 |
KR102337912B1 (ko) * | 2020-08-07 | 2021-12-10 | 한서대학교 산학협력단 | 림포일을 갖는 비행체의 추진유닛 제조방법, 림포일을 갖는 비행체의 추진유닛 및 비행체 |
CN112520026A (zh) * | 2020-12-23 | 2021-03-19 | 中国民用航空飞行学院 | 一种新型变体飞行器 |
US11247783B1 (en) * | 2021-03-08 | 2022-02-15 | Heleng Inc. | Aircraft |
WO2024001143A1 (zh) * | 2022-06-30 | 2024-01-04 | 亿航智能设备(广州)有限公司 | 涵道风扇、飞行器及其姿态控制方法、装置和相关设备 |
WO2024035714A1 (en) * | 2022-08-09 | 2024-02-15 | Pete Bitar | Compact and lightweight drone delivery device called an arcspear electric jet drone system having an electric ducted air propulsion system and being relatively difficult to track in flight |
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-
2017
- 2017-02-27 EP EP17400008.3A patent/EP3366586B1/en active Active
-
2018
- 2018-01-24 JP JP2018009621A patent/JP6516888B2/ja active Active
- 2018-01-29 SG SG10201800731PA patent/SG10201800731PA/en unknown
- 2018-02-13 CN CN201810150685.6A patent/CN108502151B/zh active Active
- 2018-02-20 BR BR102018003220-8A patent/BR102018003220B1/pt active IP Right Grant
- 2018-02-23 MX MX2018002328A patent/MX2018002328A/es unknown
- 2018-02-26 KR KR1020180022866A patent/KR102049969B1/ko active IP Right Grant
- 2018-02-27 US US15/906,013 patent/US11220325B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
BR102018003220B1 (pt) | 2022-05-17 |
US20180244367A1 (en) | 2018-08-30 |
US11220325B2 (en) | 2022-01-11 |
CN108502151A (zh) | 2018-09-07 |
KR102049969B1 (ko) | 2019-11-28 |
CN108502151B (zh) | 2021-06-08 |
JP6516888B2 (ja) | 2019-05-22 |
SG10201800731PA (en) | 2018-09-27 |
JP2018140772A (ja) | 2018-09-13 |
KR20180099522A (ko) | 2018-09-05 |
EP3366586B1 (en) | 2020-08-19 |
EP3366586A1 (en) | 2018-08-29 |
BR102018003220A2 (pt) | 2018-10-30 |
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