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CN205316736U - 多轴载人飞行器 - Google Patents

多轴载人飞行器 Download PDF

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CN205316736U
CN205316736U CN201521110704.0U CN201521110704U CN205316736U CN 205316736 U CN205316736 U CN 205316736U CN 201521110704 U CN201521110704 U CN 201521110704U CN 205316736 U CN205316736 U CN 205316736U
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cabin
water
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cooler
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杜昊
林祖明
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Guangzhou Ehang Intelligent Technology Co Ltd
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Priority to NZ716749A priority patent/NZ716749A/en
Priority to US15/056,088 priority patent/US20170183099A1/en
Priority to EP16159553.3A priority patent/EP3184430A1/en
Priority to AU2016100267A priority patent/AU2016100267A4/en
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    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B21/00—Machines, plants or systems, using electric or magnetic effects
    • F25B21/02—Machines, plants or systems, using electric or magnetic effects using Peltier effect; using Nernst-Ettinghausen effect
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    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
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    • H05K7/005—Constructional details common to different types of electric apparatus arrangements of circuit components without supporting structure
    • 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
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space the air being conditioned
    • B64D2013/0603—Environmental Control Systems
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    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space
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    • B—PERFORMING OPERATIONS; TRANSPORTING
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    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
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Abstract

本实用新型涉及一种多轴载人飞行器，包括电气系统、换热系统、机舱、位于机舱内的安置舱，安置舱内容置有电气系统，换热系统至少包括连通机舱外部的进风口、与安置舱连通的出风口、设有进气端和出气端的冷却器，进风口与进气端连通，出风口与出气端连通。工作时，飞行器外部的空气从进风口进入换热系统，空气通过进气端进入冷却器，冷却器根据需求对空气进行制冷，制冷后的空气从出气端流出，并通过出风口进入安置舱内，为安置舱提供冷气，给电气系统散热，使电气系统工作更稳定，提高飞行器的安全系数，保证飞行器的安全。

Description

多轴载人飞行器
技术领域
本实用新型涉及飞行器技术领域，特别涉及一种多轴载人飞行器。
背景技术
目前，多轴载人飞行器因其具有良好的机动性和操纵性，应用越来越广泛。飞行时，飞行器的电气系统给飞行器的各个用电器件供电，电气系统会产生大量的热量，容易使电气系统工作不稳定，且加速电气系统的老化，并存在安全隐患，降低多轴载人飞行器的安全系数。
实用新型内容
本实用新型的目的在于提供一种多轴载人飞行器，能够为电气系统散热，延长电气系统的使用寿命，保证飞行器的安全。
为实现本实用新型的目的，采取的技术方案是：
一种多轴载人飞行器，包括电气系统、换热系统、机舱、位于机舱内的安置舱，安置舱内容置有电气系统，换热系统至少包括连通机舱外部的进风口、与安置舱连通的出风口、设有进气端和出气端的冷却器，进风口与进气端连通，出风口与出气端连通。
工作时，飞行器外部的空气从进风口进入换热系统，空气通过进气端进入冷却器，冷却器对空气进行制冷，制冷后的空气从出气端流出，并通过出风口进入安置舱内，为安置舱提供冷气，给电气系统散热，使电气系统工作更稳定，提高飞行器的安全系数，保证飞行器的安全。
下面对技术方案进一步说明：
进一步的是，冷却器设有由若干半导体制冷片围绕形成的换热风道，进气端和出气端均与换热风道连通。冷却器通过半导体制冷片制冷或制热，无需压缩机和制冷剂，安全环保，提高多轴载人飞行器的安全系数；体积小、重量轻，减少飞行器的重量；且没有滑动部件，可靠性高，噪声低，进一步提高乘坐的舒适度。
进一步的是，换热系统还包括循环管道、设于循环管道上的水排和水泵，冷却器设有用于安置制冷片的容纳腔、连通容纳腔的进水口和出水口，循环管道的两端分别与进水口和所述出水口连通。半导体制冷片在工作过程中产生大量的热量，通过水排进行散热，散热效果好，延长半导体制冷片的使用寿命。
进一步的是，水排有两个，两个水排对称设置于循环管道上。通过对称设置的两个水排，使散热效果更好。
进一步的是，多轴载人飞行器还包括位于安置舱内的温度传感器、与温度传感器电性连接的控制器，控制器与冷却器电性连接。温度传感器检测安置舱内的温度，并将采集的信息发送至控制器，控制器通过控制冷气器的工作，调整安置舱内的温度，使调整更智能。
进一步的是，换热系统还包括与出气端和出风口连通的出风管道，出风管道上连接有第一离心风机。通过第一离心风机将制冷的空气送入出风口，使空气的流通更顺畅。
进一步的是，进风口上设有第二离心风机。通过第二离心风机将外部空气送入冷却器的进气端，使空气的流通更顺畅。
与现有技术相比，本实用新型具有以下有益效果：
本实用新型工作时，飞行器外部的空气从进风口进入换热系统，空气通过进气端进入冷却器，冷却器对空气进行制冷，制冷后的空气从出气端流出，并通过出风口进入安置舱内，为安置舱提供冷气，给电气系统散热，使电气系统工作更稳定，提高飞行器的安全系数，保证飞行器的安全。
附图说明
图1是本实用新型实施例多轴载人飞行器的结构示意图。
附图标记说明：
10.进风口，20.出风口，30.冷却器，310.进气端，320.出气端，330.进水口，340.出水口，410.循环管道，420.水排，430.水泵，50.出风管道，60.第一离心风机，70.第二离心风机，80.导气管道。
具体实施方式
下面结合附图对本实用新型的实施例进行详细说明：
如图1所示，一种多轴载人飞行器，包括电气系统(附图未标识)、换热系统、机舱(附图未标识)、位于机舱内的安置舱(附图未标识)，安置舱内容置有电气系统，换热系统至少包括连通机舱外部的进风口10、与安置舱连通的出风口20、设有进气端310和出气端320的冷却器30，进风口10与进气端310连通，出风口20与出气端320连通。
工作时，飞行器外部的空气从进风口10进入换热系统，空气通过进气端310进入冷却器30，冷却器30对空气进行制冷，制冷后的空气从出气端320流出，并通过出风口20进入安置舱内，为安置舱提供冷气，给电气系统散热，使电气系统工作更稳定，提高飞行器的安全系数，保证飞行器的安全。
在本实施例中，冷却器30设有由若干半导体制冷片(附图未标识)围绕形成的换热风道(附图未标识)，进气端310和出气端320均与换热风道连通。冷却器30通过半导体制冷片制冷或制热，无需压缩机和制冷剂，安全环保，提高多轴载人飞行器的安全系数；体积小、重量轻，减少飞行器的重量；且没有滑动部件，可靠性高，噪声低，进一步提高乘坐的舒适度。冷却器30还可以根据实际需要采用其他换热方式。
如图1所示，换热系统还包括循环管道410、设于循环管道410上的水排420和水泵430，冷却器30设有用于安置制冷片的容纳腔(附图未标识)、连通容纳腔的进水口330和出水口340，循环管道410的两端分别与进水口330和出水口340连通。半导体制冷片在工作过程中产生大量的热量，通过水排420进行散热，散热效果好，延长半导体制冷片的使用寿命。
在本实施例中，水排420有两个，两个水排420对称设置于循环管道410上。通过对称设置的两个水排420，使散热效果更好。水排420还可以根据实际需要设置一个以上。
多轴载人飞行器还包括位于安置舱内的温度传感器(附图未标识)、与温度传感器电性连接的控制器(附图未标识)，控制器与冷却器30电性连接。温度传感器检测安置舱内的温度，并将采集的信息发送至控制器，控制器通过控制冷气器30的工作，调整安置舱内的温度，使调整更智能。
如图1所示，换热系统还包括与出气端320和出风口20连通的出风管道50，出风管道上连接有第一离心风机60。通过第一离心风机60将制冷的空气送入出风口，使空气的流通。
在本实施例中，多轴载人飞行器设有两个进风口10，进风口10上设有第二离心风机70，出风管道50连接有两个出风口20，第二离心风机70安装在机舱的顶部，冷却器30安装在机舱的侧板，安置舱设置在机舱的底部，第二离心风机920把吸入的空气，沿着导气管道80输送到冷却器30中，再通过出气端320输送至安置舱。第二离心风机70、冷却器30、安置舱还可以根据实际需要设置到机舱的其他位置。进风口10、出风口20的数量还可以根据实际需要设置一个以上。
以上所述实施例的各技术特征可以进行任意的组合，为使描述简洁，未对上述实施例中的各个技术特征所有可能的组合都进行描述，然而，只要这些技术特征的组合不存在矛盾，都应当认为是本说明书记载的范围。
以上所述实施例仅表达了本实用新型的几种实施方式，其描述较为具体和详细，但并不能因此而理解为对实用新型专利范围的限制。应当指出的是，对于本领域的普通技术人员来说，在不脱离本实用新型构思的前提下，还可以做出若干变形和改进，这些都属于本实用新型的保护范围。因此，本实用新型专利的保护范围应以所附权利要求为准。

Claims (7)

1.一种多轴载人飞行器，其特征在于，包括电气系统、换热系统、机舱、位于所述机舱内的安置舱，所述安置舱内容置有所述电气系统，所述换热系统至少包括连通所述机舱外部的进风口、与所述安置舱连通的出风口、设有进气端和出气端的冷却器，所述进风口与所述进气端连通，所述出风口与所述出气端连通。
2.根据权利要求1所述的多轴载人飞行器，其特征在于，所述冷却器设有由若干半导体制冷片围绕形成的换热风道，所述进气端和所述出气端均与所述换热风道连通。
3.根据权利要求2所述的多轴载人飞行器，其特征在于，所述换热系统还包括循环管道、设于所述循环管道上的水排和水泵，所述冷却器设有用于安置所述制冷片的容纳腔、连通所述容纳腔的进水口和出水口，所述循环管道的两端分别与所述进水口和所述出水口连通。
4.根据权利要求3所述的多轴载人飞行器，其特征在于，所述水排有两个，两个所述水排对称设置于所述循环管道上。
5.根据权利要求1所述的多轴载人飞行器，其特征在于，还包括位于所述安置舱内的温度传感器、与所述温度传感器电性连接的控制器，所述控制器与所述冷却器电性连接。
6.根据权利要求1至5任一项所述的多轴载人飞行器，其特征在于，所述换热系统还包括与所述出气端和所述出风口连通的出风管道，所述出风管道上连接有第一离心风机。
7.根据权利要求1至5任一项所述的多轴载人飞行器，其特征在于，所述进风口上设有第二离心风机。
CN201521110704.0U 2015-12-25 2015-12-25 多轴载人飞行器 Active CN205316736U (zh)

Priority Applications (6)

Application Number Priority Date Filing Date Title
CN201521110704.0U CN205316736U (zh) 2015-12-25 2015-12-25 多轴载人飞行器
NZ716749A NZ716749A (en) 2015-12-25 2016-02-09 Multi-axis passenger-carrying aircraft
US15/056,088 US20170183099A1 (en) 2015-12-25 2016-02-29 Multi-axis passenger-carrying aircraft
EP16159553.3A EP3184430A1 (en) 2015-12-25 2016-03-10 Electrical system cooling in a multi-axis passenger-carrying aircraft
AU2016100267A AU2016100267A4 (en) 2015-12-25 2016-03-10 Multi-axis passenger-carrying aircraft
PCT/CN2016/106629 WO2017107719A1 (zh) 2015-12-25 2016-11-21 多轴载人飞行器

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CN118034460A (zh) * 2024-03-18 2024-05-14 苏州知悉科技有限公司 一种环境数据处理系统及方法

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AU2016100267A4 (en) 2016-04-07
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WO2017107719A1 (zh) 2017-06-29
EP3184430A1 (en) 2017-06-28

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