SG11201910744WA - Vertical take-off and landing unmanned aerial vehicle having foldable fixed wing and based on twin-ducted fan power system - Google Patents
Vertical take-off and landing unmanned aerial vehicle having foldable fixed wing and based on twin-ducted fan power systemInfo
- Publication number
- SG11201910744WA SG11201910744WA SG11201910744WA SG11201910744WA SG11201910744WA SG 11201910744W A SG11201910744W A SG 11201910744WA SG 11201910744W A SG11201910744W A SG 11201910744WA SG 11201910744W A SG11201910744W A SG 11201910744WA SG 11201910744W A SG11201910744W A SG 11201910744WA
- Authority
- SG
- Singapore
- Prior art keywords
- twin
- power system
- aerial vehicle
- unmanned aerial
- fixed wing
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- 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
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
- B64C39/068—Aircraft not otherwise provided for having disc- or ring-shaped wings having multiple wings joined at the tips
-
- 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
- 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
- B64U60/00—Undercarriages
- B64U60/40—Undercarriages foldable or retractable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing 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
-
- 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
- B64U50/13—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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- 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
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710343539.0A CN107176286B (zh) | 2017-05-16 | 2017-05-16 | 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 |
PCT/CN2017/111341 WO2018209911A1 (zh) | 2017-05-16 | 2017-11-16 | 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 |
Publications (1)
Publication Number | Publication Date |
---|---|
SG11201910744WA true SG11201910744WA (en) | 2020-01-30 |
Family
ID=59831169
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG11201910744WA SG11201910744WA (en) | 2017-05-16 | 2017-11-16 | Vertical take-off and landing unmanned aerial vehicle having foldable fixed wing and based on twin-ducted fan power system |
Country Status (4)
Country | Link |
---|---|
US (1) | US11634222B2 (zh) |
CN (1) | CN107176286B (zh) |
SG (1) | SG11201910744WA (zh) |
WO (1) | WO2018209911A1 (zh) |
Families Citing this family (39)
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---|---|---|---|---|
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 |
CN107826247A (zh) * | 2017-11-15 | 2018-03-23 | 江苏航空职业技术学院 | 一种带固定机翼两倾转涵道四旋翼无人飞行器 |
CN108786143A (zh) * | 2018-05-30 | 2018-11-13 | 林洪烨 | 一种机身通用化的抗坠毁固定翼航模飞机 |
DE102018116147A1 (de) * | 2018-07-04 | 2020-01-09 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Luftfahrzeug |
CN109353505A (zh) * | 2018-09-21 | 2019-02-19 | 清华大学 | 一种气动力/推力矢量复合控制的尾座式无人机 |
CN109941426B (zh) * | 2019-03-29 | 2024-01-09 | 成都云鼎智控科技有限公司 | 飞行器尾部总成 |
CN109878710A (zh) * | 2019-04-04 | 2019-06-14 | 北京零偏科技有限责任公司 | 一种碟形涵道式无人机 |
CN110065352A (zh) * | 2019-05-24 | 2019-07-30 | 上海应用技术大学 | 一种倾转涵道式结构的飞行汽车 |
CN110641695B (zh) * | 2019-09-20 | 2022-03-18 | 南京航空航天大学 | 一种适用于小型垂直起降固定翼飞行器的动力系统 |
CN110775250A (zh) * | 2019-11-19 | 2020-02-11 | 南京航空航天大学 | 一种变体倾转旋翼机及其工作方法 |
CN111169621A (zh) * | 2019-12-18 | 2020-05-19 | 中国航空工业集团公司成都飞机设计研究所 | 一种可旋转至垂直状态安全分离的多功能机翼 |
CN111086625B (zh) * | 2019-12-23 | 2023-09-22 | 航天神舟飞行器有限公司 | 双涵道可变座舱尾座式垂直起降载人固定翼飞行器 |
CN111572756A (zh) * | 2020-05-14 | 2020-08-25 | 中国空气动力研究与发展中心 | 一种涵道风扇动力低成本高速长航时布局的飞行器 |
CN111942584A (zh) * | 2020-07-01 | 2020-11-17 | 中国航空研究院 | 一种积木式空中组合/分离无人飞行器 |
CN112124569B (zh) * | 2020-09-17 | 2022-04-01 | 西安电子科技大学 | 一种基于发射筒的垂直起降及稳定无人机系统 |
US20220177109A1 (en) * | 2020-12-09 | 2022-06-09 | Bell Textron Inc. | Detect and avoid sensor integration |
KR20220087212A (ko) * | 2020-12-17 | 2022-06-24 | 현대자동차주식회사 | 에어 모빌리티 |
CN112623183B (zh) * | 2020-12-29 | 2023-01-17 | 中国民航大学 | 一种便携式垂直起降的斜置翼飞行器 |
CN112937851B (zh) * | 2021-02-01 | 2022-10-18 | 河北利翔航空科技有限公司 | 一种使用康达效应增升的垂直起降固定翼飞行器 |
CN113602478B (zh) * | 2021-02-02 | 2023-06-13 | 中国空气动力研究与发展中心高速空气动力研究所 | 一种基于环量控制和垂直微喷流的流体控制舵面 |
CN112960106B (zh) * | 2021-04-06 | 2023-01-24 | 上海工程技术大学 | 一种可变形机翼及变形方法 |
CN113232826B (zh) * | 2021-05-07 | 2022-06-17 | 南京航空航天大学 | 一种机尾坐立式的垂直起降飞行器及其控制方法 |
CN113120223A (zh) * | 2021-05-13 | 2021-07-16 | 成都航空职业技术学院 | 一种可垂直起降的涵道扇翼无人机及其控制方法 |
CN113104195B (zh) * | 2021-05-19 | 2022-03-11 | 涵涡智航科技(玉溪)有限公司 | 一种双涵道复合翼飞行器 |
US11541999B2 (en) | 2021-06-01 | 2023-01-03 | Hoversurf, Inc. | Methods of vertical take-off/landing and horizontal straight flight of aircraft and aircraft for implementation |
CN113049211B (zh) * | 2021-06-01 | 2021-08-10 | 中国空气动力研究与发展中心低速空气动力研究所 | 一种风洞试验装置 |
US11383831B1 (en) * | 2021-06-01 | 2022-07-12 | Hoversurf, Inc. | Methods of vertical take-off/landing and horizontal straight flight of aircraft and aircraft for implementation |
EP4105125B1 (en) | 2021-06-18 | 2023-09-06 | Leonardo S.p.a. | Series of convertible aircrafts capable of hovering and method for configuring a convertible aircraft capable of hovering |
CN113443134B (zh) * | 2021-06-22 | 2022-08-05 | 南京航空航天大学 | 升力桨叶可变体收放的机尾坐立式垂直起降飞行器 |
US11377220B1 (en) | 2021-09-27 | 2022-07-05 | Hoversurf, Inc. | Methods of increasing flight safety, controllability and maneuverability of aircraft and aircraft for implementation thereof |
CN113753229A (zh) * | 2021-10-09 | 2021-12-07 | 吉林大学 | 一种可折叠式固定翼四旋翼复合无人机及其控制方法 |
CN114030603B (zh) * | 2021-10-27 | 2022-11-04 | 南京航空航天大学 | 一种变涵道尾座式高速无人机及其工作方法 |
CN113911330A (zh) * | 2021-11-12 | 2022-01-11 | 北京航空航天大学 | 一种油动涵道飞行器 |
CN114560073B (zh) * | 2021-12-30 | 2024-01-30 | 中国航空工业集团公司西安飞机设计研究所 | 一种螺旋桨飞机滑流预感知方向舵偏转控制方法及其系统 |
CN114486149B (zh) * | 2022-01-19 | 2023-11-24 | 山东交通学院 | 一种基于无人机测试的风场模拟发生装置及方法 |
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CN115056967B (zh) * | 2022-06-29 | 2023-04-25 | 浙江大学 | 一种双轴旋转折叠的刚性机翼及使用方法 |
CN115489716B (zh) * | 2022-09-22 | 2023-12-29 | 中国商用飞机有限责任公司 | 集成有分布式涵道风扇的机翼和电动飞机 |
USD1022797S1 (en) * | 2022-12-01 | 2024-04-16 | Autoflight (Kunshan) Co., Ltd. | Drone aircraft |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5086993A (en) * | 1989-02-09 | 1992-02-11 | Aca Industries | Airplane with variable-incidence wing |
US8720814B2 (en) * | 2005-10-18 | 2014-05-13 | Frick A. Smith | Aircraft with freewheeling engine |
CN101857086A (zh) | 2010-06-03 | 2010-10-13 | 哈尔滨盛世特种飞行器有限公司 | 双涵道垂直起降无人飞行器 |
FR2964944B1 (fr) | 2010-09-20 | 2013-05-24 | Snecma | Dispositif d'etancheite a soufflet pour la traversee de cloison par une biellette d'un systeme de commande de l'orientation des pales de soufflante d'un turbopropulseur |
US20130206921A1 (en) * | 2012-02-15 | 2013-08-15 | Aurora Flight Sciences Corporation | System, apparatus and method for long endurance vertical takeoff and landing vehicle |
CN102673780A (zh) * | 2012-06-07 | 2012-09-19 | 李建波 | 双构型飞行器 |
CN202966660U (zh) | 2012-09-05 | 2013-06-05 | 刘笠浩 | 一种安全的高速飞行包装置 |
CN103231805B (zh) | 2013-05-21 | 2015-09-16 | 吉林大学 | 涵道式折翼机 |
US9567088B2 (en) * | 2013-10-15 | 2017-02-14 | Swift Engineering, Inc. | Vertical take-off and landing aircraft |
US10054958B2 (en) * | 2014-05-08 | 2018-08-21 | Northrop Grumman Systems Corporation | Vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV) |
US9567079B2 (en) * | 2014-09-10 | 2017-02-14 | Jonathon Thomas Johnson | VTOL symmetric airfoil fuselage of fixed wing design |
WO2017035503A1 (en) * | 2015-08-27 | 2017-03-02 | Martin Uav, Llc | Vertical take off aircraft |
CN106494608A (zh) * | 2015-09-06 | 2017-03-15 | 陈康 | 多涵道螺旋桨可变机翼电动飞行器 |
CN105346715A (zh) * | 2015-09-29 | 2016-02-24 | 上海圣尧智能科技有限公司 | 一种垂直起降无人机 |
CN105711837B (zh) | 2016-01-28 | 2017-12-15 | 襄阳宏伟航空器有限责任公司 | 一种双涵道无人飞行器 |
CN205633014U (zh) * | 2016-05-25 | 2016-10-12 | 江苏数字鹰科技发展有限公司 | 一种折叠机翼垂直起降飞机 |
CN105947192A (zh) | 2016-06-01 | 2016-09-21 | 中国航空工业集团公司西安飞机设计研究所 | 一种倾转双涵道无人机 |
CN207208447U (zh) * | 2017-05-16 | 2018-04-10 | 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 |
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 |
IL272101B2 (en) * | 2017-07-18 | 2023-03-01 | St Eng Aerospace Ltd | Asymmetric aircraft |
US10583924B2 (en) * | 2017-10-01 | 2020-03-10 | Petru A. Simionescu | Vertical takeoff and landing unmanned aerial vehicle (VTOL-UAV) |
-
2017
- 2017-05-16 CN CN201710343539.0A patent/CN107176286B/zh active Active
- 2017-11-16 US US16/613,930 patent/US11634222B2/en active Active
- 2017-11-16 WO PCT/CN2017/111341 patent/WO2018209911A1/zh active Application Filing
- 2017-11-16 SG SG11201910744WA patent/SG11201910744WA/en unknown
Also Published As
Publication number | Publication date |
---|---|
US20220081111A1 (en) | 2022-03-17 |
WO2018209911A1 (zh) | 2018-11-22 |
CN107176286A (zh) | 2017-09-19 |
US11634222B2 (en) | 2023-04-25 |
CN107176286B (zh) | 2023-08-22 |
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