CN205396561U - 一种有防撞气囊的飞行器 - Google Patents
一种有防撞气囊的飞行器 Download PDFInfo
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- CN205396561U CN205396561U CN201620169660.7U CN201620169660U CN205396561U CN 205396561 U CN205396561 U CN 205396561U CN 201620169660 U CN201620169660 U CN 201620169660U CN 205396561 U CN205396561 U CN 205396561U
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- 241000736305 Marsilea quadrifolia Species 0.000 claims description 6
- 230000001681 protective effect Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000009993 protective function Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/006—Safety devices
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/30—Lighter-than-air aircraft, e.g. aerostatic 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U60/00—Undercarriages
- B64U60/50—Undercarriages with landing legs
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- 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
- B64D2201/00—Airbags mounted in aircraft for any use
-
- 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
- B64D27/353—Arrangements for on-board electric energy production, distribution, recovery or storage using solar cells
-
- 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
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
- B64U2101/31—UAVs specially adapted for particular uses or applications for imaging, photography or videography for surveillance
-
- 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
- B64U50/31—Supply or distribution of electrical power generated by photovoltaics
-
- 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
- B64U50/32—Supply or distribution of electrical power generated by fuel cells
-
- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
- Studio Devices (AREA)
Abstract
一种有防撞气囊的飞行器,包括动力装置、机架、支撑杆、气囊、摄像装置;所述动力装置安装在机架上;所述支撑杆的一端安装在机架上,另一端固定连接摄像装置;所述支撑杆共四根,所述支撑杆的形状为弧形,四根支撑杆组成伞形结构;所述机架外壁设有凹槽,所述凹槽环绕机架一周;所述气囊环套在机架外侧,气囊内侧壁与机架的凹槽卡接。本实用新型提供了一种有防撞气囊的飞行器,该飞行器装有气囊,能够有效的防止意外撞击时候损伤飞行器;以及在降落时还能防止撞击伤到人体。
Description
技术领域
本实用新型涉及飞行器领域。
背景技术
随着媒体发展的需要,越来越多的使用到航拍设备。现有一种航拍设备防撞装置,主要由:飞行器、防护架、螺丝等构成。这种结构的航拍设备防撞装置,存在的问题是,防护架只能保护侧面,使螺旋桨外露,航拍设备碰撞时所起到的防护功能不强造成跌落,从而影响航拍设备安全性。而且防护架坚硬,撞击时冲击力大,容易损坏航拍设配。因此,需要一种能有效的缓冲撞击的航拍设备。
发明内容
为了有效的解决上述提出的技术问题,本实用新型提供了一种有防撞气囊的飞行器;
一种有防撞气囊的飞行器,包括动力装置、机架、支撑杆、气囊、摄像装置;所述动力装置安装在机架上;支撑杆的一端安装在机架上,另一端固定连接摄像装置;所述支撑杆共四根,所述支撑杆的形状为弧形,四根支撑杆组成伞形结构;所述机架外壁设有凹槽,所述凹槽环绕机架一周;所述气囊环套在机架外侧,气囊内侧壁与机架的凹槽卡接。
优选地,所述气囊下方设有用于支撑飞行器的支撑部,所述支撑部与气囊一体成型。
优选地,所述机架的外形为四叶草形,所述气囊内侧壁形状为四叶草形;所述气囊的内侧壁与机架凹槽紧密配合。
优选地,为了减轻机架的重量,所述机架上设有通孔。
相比现有技术,本实用新型的有益效果在于:本实用新型在机架外环套有气囊,气囊具有良好的缓冲效果,而且质量小,能有效的防止意外撞击时候破坏飞行器;以及在降落时还能防止撞击伤到人体。
附图说明
图1为有防撞气囊的飞行器的俯视图;
图2为有防撞气囊的飞行器的正视图;
图3为有防撞气囊的飞行器的爆炸图;
图中:1、动力装置;2、气囊;21、内侧壁;22、支撑部;3、机架;31、凹槽;32、通孔;4、摄像装置;5、支撑杆。
具体实施方式
下面,结合附图以及具体实施方式,对本实用新型做进一步描述:
实施例一
如图1~3所示,一种有防撞气囊的飞行器,包括动力装置1、机架3、支撑杆5、气囊2、摄像装置4;所述动力装置1安装在机架3上;所述动力装置1为安装有螺旋桨的电机和电池。支撑杆5的一端安装在机架3上,另一端固定连接摄像装置4;所述摄像装置4为摄像机。所述支撑杆5共四根,所述支撑杆5的形状为弧形,四根支撑杆5组成伞形结构。所述机架3外壁设有凹槽31,所述凹槽31环绕机架3一周;所述气囊2环套在机架3外侧,气囊2内侧壁21与机架3的凹槽31卡接。所述机架3的外形为四叶草形,所述气囊2内侧壁21形状为四叶草形;所述气囊2的内侧壁21与机架3凹槽31紧密配合。气囊2与机架3紧密贴合,能全方位的保护机架3受到撞击,同时四叶草形的机架3有助于飞行器的飞行稳定。所述气囊2下方设有用于支撑飞行器的支撑部22,所述支撑部22与气囊2一体成型。支撑部22可以防止飞行器由于降落过快撞击地面损坏飞行器。为了减轻飞行器自身的重量,在机架3上设有通孔32。
对本领域的技术人员来说,可根据以上描述的技术方案以及构思,做出其它各种相应的改变以及形变,而所有的这些改变以及形变都应该属于本实用新型权利要求的保护范围之内。
Claims (4)
1.一种有防撞气囊的飞行器,包括动力装置、机架、支撑杆、气囊、摄像装置;所述动力装置安装在机架上;所述支撑杆的一端安装在机架上,另一端固定连接摄像装置;所述支撑杆共四根,所述支撑杆的形状为弧形,四根支撑杆组成伞形结构;所述机架外壁设有凹槽,所述凹槽环绕机架一周;所述气囊环套在机架外侧,气囊内侧壁与机架的凹槽卡接。
2.根据权利要求1所述的飞行器,其特征在于:所述气囊下方设有用于支撑飞行器的支撑部,所述支撑部与气囊一体成型。
3.根据权利要求2所述的飞行器,其特征在于:所述机架的外形为四叶草形,所述气囊内侧壁形状为四叶草形;所述气囊的内侧壁与机架凹槽紧密配合。
4.根据权利要求3所述的飞行器,其特征在于:所述机架上设有通孔。
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CN201620169660.7U CN205396561U (zh) | 2016-03-04 | 2016-03-04 | 一种有防撞气囊的飞行器 |
US15/207,577 US20170253325A1 (en) | 2016-03-04 | 2016-07-12 | Unmanned aerial vehicle (uav) and a method of improving the performance thereof |
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CN201620169660.7U CN205396561U (zh) | 2016-03-04 | 2016-03-04 | 一种有防撞气囊的飞行器 |
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Cited By (5)
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CN106184784A (zh) * | 2016-08-24 | 2016-12-07 | 上海与德通讯技术有限公司 | 无人机控制方法、装置和无人机 |
CN106628209A (zh) * | 2017-01-06 | 2017-05-10 | 尚青 | 一种多轴载人飞行器 |
CN109715496A (zh) * | 2016-11-04 | 2019-05-03 | 株式会社松屋R&D | 带有安全气囊的无人飞机 |
CN111056027A (zh) * | 2019-12-28 | 2020-04-24 | 河南省科宇信息技术有限公司 | 一种高续航防碰撞监测巡检无人机 |
AU2018205033B2 (en) * | 2016-12-31 | 2020-09-10 | Jayant RATTI | High endurance unmanned aerial vehicle |
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CN205989812U (zh) * | 2015-06-25 | 2017-03-01 | 瑞德利斯技术公司 | 多旋翼无人机 |
JP6037190B1 (ja) * | 2015-07-31 | 2016-12-07 | パナソニックIpマネジメント株式会社 | 飛行体 |
WO2017022209A1 (ja) * | 2015-07-31 | 2017-02-09 | パナソニックIpマネジメント株式会社 | 飛行体 |
US10553122B1 (en) * | 2016-03-22 | 2020-02-04 | Amazon Technologies, Inc. | Unmanned aerial vehicle data collection for routing |
CN107323666B (zh) * | 2016-04-28 | 2020-11-06 | 深圳富泰宏精密工业有限公司 | 无人飞行器 |
US10689109B2 (en) * | 2016-10-13 | 2020-06-23 | Dynetics, Inc. | Interceptor unmanned aerial system |
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IT202100002609A1 (it) * | 2021-02-05 | 2022-08-05 | C I R A Centro Italiano Ricerche Aerospaziali S C P A | Aeromobile gonfiabile ibrido di tipo unmanned |
DE102021118351B3 (de) | 2021-07-15 | 2022-11-24 | Technische Universität Chemnitz, Körperschaft des öffentlichen Rechts | Drohne |
US11753161B2 (en) * | 2022-01-28 | 2023-09-12 | Tony Wayne Thomas, SR. | Buoyancy and impact recovery system |
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EP3459859B1 (en) * | 2014-02-27 | 2020-09-02 | SZ DJI Technology Co., Ltd. | Impact protection apparatus |
JP5875093B1 (ja) * | 2015-06-17 | 2016-03-02 | 浩平 中村 | 浮揚型飛行体 |
US10000284B1 (en) * | 2015-06-26 | 2018-06-19 | Amazon Technologies, Inc. | Collaborative unmanned aerial vehicle for an inventory system |
JP6037190B1 (ja) * | 2015-07-31 | 2016-12-07 | パナソニックIpマネジメント株式会社 | 飛行体 |
-
2016
- 2016-03-04 CN CN201620169660.7U patent/CN205396561U/zh not_active Expired - Fee Related
- 2016-07-12 US US15/207,577 patent/US20170253325A1/en not_active Abandoned
Cited By (7)
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CN106184784A (zh) * | 2016-08-24 | 2016-12-07 | 上海与德通讯技术有限公司 | 无人机控制方法、装置和无人机 |
CN109715496A (zh) * | 2016-11-04 | 2019-05-03 | 株式会社松屋R&D | 带有安全气囊的无人飞机 |
CN115535274A (zh) * | 2016-11-04 | 2022-12-30 | 株式会社松屋R&D | 带有安全气囊的无人飞机 |
US11772597B2 (en) | 2016-11-04 | 2023-10-03 | Matsuya R&D Co., Ltd. | Drone with airbag |
AU2018205033B2 (en) * | 2016-12-31 | 2020-09-10 | Jayant RATTI | High endurance unmanned aerial vehicle |
CN106628209A (zh) * | 2017-01-06 | 2017-05-10 | 尚青 | 一种多轴载人飞行器 |
CN111056027A (zh) * | 2019-12-28 | 2020-04-24 | 河南省科宇信息技术有限公司 | 一种高续航防碰撞监测巡检无人机 |
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