CN114761323A - 多旋翼飞行器及其与固定翼飞行器空中分离的相关方法 - Google Patents
多旋翼飞行器及其与固定翼飞行器空中分离的相关方法 Download PDFInfo
- Publication number
- CN114761323A CN114761323A CN202080079896.0A CN202080079896A CN114761323A CN 114761323 A CN114761323 A CN 114761323A CN 202080079896 A CN202080079896 A CN 202080079896A CN 114761323 A CN114761323 A CN 114761323A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- fixed
- rotor
- wing
- wing aircraft
- 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.)
- Pending
Links
- 238000000034 method Methods 0.000 title claims description 31
- 238000000926 separation method Methods 0.000 title claims description 28
- 210000001503 joint Anatomy 0.000 claims abstract description 25
- 238000003032 molecular docking Methods 0.000 claims description 69
- 230000007246 mechanism Effects 0.000 claims description 48
- 230000000712 assembly Effects 0.000 claims description 24
- 238000000429 assembly Methods 0.000 claims description 24
- 238000006073 displacement reaction Methods 0.000 claims description 10
- 230000005484 gravity Effects 0.000 claims description 8
- 239000000314 lubricant Substances 0.000 claims description 7
- 230000007423 decrease Effects 0.000 claims description 4
- 230000001133 acceleration Effects 0.000 claims 1
- 238000005096 rolling process Methods 0.000 claims 1
- 238000013459 approach Methods 0.000 description 6
- 230000005540 biological transmission Effects 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- 230000009286 beneficial effect Effects 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 239000002828 fuel tank Substances 0.000 description 4
- 230000006870 function Effects 0.000 description 4
- 239000002775 capsule Substances 0.000 description 3
- 230000008859 change Effects 0.000 description 3
- 238000004590 computer program Methods 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000002457 bidirectional effect Effects 0.000 description 2
- 230000000903 blocking effect Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000004308 accommodation Effects 0.000 description 1
- 230000001174 ascending effect Effects 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000003028 elevating effect Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
-
- 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
-
- 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
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Transmission Devices (AREA)
Abstract
一种多旋翼飞行器(1)，包括机架(11)和第一驱动组件(12)，机架(11)包括本体(111)和两对接部(112)，两对接部(112)分别设于本体(111)的相对两侧或顶端上；第一驱动组件(12)包括分别设于两对接部(112)底面上或本体(111)上的两组第一旋翼单元(120)，在多旋翼飞行器(1)与固定翼飞行器(2)对接后，第一旋翼单元(120)与固定翼飞行器(2)的机翼(22)通过对接部(112)和/或本体(111)隔挡。本发明通过多旋翼飞行器(1)与固定翼飞行器(2)对接和分离，辅助固定翼飞行器(2)实现垂直起降功能；多旋翼飞行器(1)通过对接部(112)与固定翼飞行器(2)的机翼(22)对接，使得多旋翼飞行器(1)与固定翼飞行器(2)在其纵向和横向的可对接长度增加，有利于提高对接的成功率；在多旋翼飞行器(1)与固定翼飞行器(2)对接和分离的前后，还能够有效避免第一旋翼单元(120)与固定翼飞行器(2)的机翼(22)发生碰撞。
Description
PCT国内申请，说明书已公开。
Claims (20)
- PCT国内申请，权利要求书已公开。
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2019219474652 | 2019-11-12 | ||
| CN201921947465 | 2019-11-12 | ||
| PCT/CN2020/000274 WO2021093135A1 (zh) | 2019-11-12 | 2020-11-11 | 多旋翼飞行器及其与固定翼飞行器空中分离的相关方法 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114761323A true CN114761323A (zh) | 2022-07-15 |
Family
ID=75911694
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202080079896.0A Pending CN114761323A (zh) | 2019-11-12 | 2020-11-11 | 多旋翼飞行器及其与固定翼飞行器空中分离的相关方法 |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN114761323A (zh) |
| WO (1) | WO2021093135A1 (zh) |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5000398A (en) * | 1988-10-25 | 1991-03-19 | Rashev Michael S | Flying multi-purpose aircraft carrier and method of V/STOL assisted flight |
| CN105711852B (zh) * | 2016-04-12 | 2017-10-10 | 吕孔东 | 一种舰载机弹射器 |
| CN106043689B (zh) * | 2016-07-22 | 2019-08-27 | 绵阳空天科技有限公司 | 背负式固定翼飞行器垂直起飞辅助系统 |
| CN106965935A (zh) * | 2017-03-10 | 2017-07-21 | 佛山市神风航空科技有限公司 | 一种组合飞行器及其降落方式 |
| CN206885351U (zh) * | 2017-03-10 | 2018-01-16 | 佛山市神风航空科技有限公司 | 一种飞机起降系统 |
| CN208053674U (zh) * | 2018-03-13 | 2018-11-06 | 珠海天晴航空航天科技有限公司 | 一种无人机弹射起飞装置 |
| CN208264586U (zh) * | 2018-05-08 | 2018-12-21 | 龚日鸿 | 可共享的无人机的能源模块更换系统 |
| CN110116806B (zh) * | 2019-04-28 | 2022-05-03 | 南京航空航天大学 | 一种用于固定翼无人机与旋翼发射平台对接的装置 |
-
2020
- 2020-11-11 CN CN202080079896.0A patent/CN114761323A/zh active Pending
- 2020-11-11 WO PCT/CN2020/000274 patent/WO2021093135A1/zh active Application Filing
Also Published As
| Publication number | Publication date |
|---|---|
| WO2021093135A1 (zh) | 2021-05-20 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11753159B2 (en) | VTOL aircraft | |
| EP3587263A1 (en) | Vertical take-off and landing unmanned aerial vehicle | |
| US10287011B2 (en) | Air vehicle | |
| US4678141A (en) | Aircraft launcher and retriever | |
| US8366049B2 (en) | Hover delivery of cabin payload in tilt-rotor and tilt-wing aircraft | |
| CN115867486A (zh) | 垂直起降飞行器 | |
| EP3768592B1 (en) | A structure construction for an aircraft and aircraft comprising the structure construction | |
| CN102133926A (zh) | 一种尾坐式垂直起降无人飞行器 | |
| US20060016931A1 (en) | High-lift, low-drag dual fuselage aircraft | |
| US11912435B2 (en) | Air vehicle system | |
| US12105528B2 (en) | Walking VTOL drone and related systems and methods | |
| AU2017238355B2 (en) | Vertical take-off and landing aircraft | |
| CN114761323A (zh) | 多旋翼飞行器及其与固定翼飞行器空中分离的相关方法 | |
| CN114148513B (zh) | 一种无人机起降平台及一种无人机起飞、降落系统 | |
| CN218617171U (zh) | 一种多旋翼飞行器 | |
| CN213384709U (zh) | 垂直起降空中无人机 | |
| CN113415406A (zh) | 机翼间距调节模块、包含其的飞行器及飞行器控制方法 | |
| US10654556B2 (en) | VTOL aircraft with wings | |
| CN213974456U (zh) | 垂直起降空中无人机 | |
| CN212890923U (zh) | 垂直起降的固定翼倾斜旋翼飞行器 | |
| CN218258701U (zh) | 飞行体 | |
| CN220948591U (zh) | 飞行体 | |
| CN215514111U (zh) | 倾转旋翼飞机 | |
| CN117382882A (zh) | 可水上垂直起降和游动的涵道风扇飞行器及其操作方法 | |
| WO2023287715A2 (en) | Vtol transport clusters |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |