WO2018019152A1 - 用于多旋翼植保飞行器的电调电机安装座 - Google Patents
用于多旋翼植保飞行器的电调电机安装座 Download PDFInfo
- Publication number
- WO2018019152A1 WO2018019152A1 PCT/CN2017/093263 CN2017093263W WO2018019152A1 WO 2018019152 A1 WO2018019152 A1 WO 2018019152A1 CN 2017093263 W CN2017093263 W CN 2017093263W WO 2018019152 A1 WO2018019152 A1 WO 2018019152A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- fastening portion
- electric motor
- semicircular
- bump
- mounting base
- Prior art date
Links
- 229910052751 metal Inorganic materials 0.000 claims description 7
- 239000002184 metal Substances 0.000 claims description 7
- 229910000838 Al alloy Inorganic materials 0.000 claims description 6
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- 239000004917 carbon fiber Substances 0.000 claims description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 3
- 230000003014 reinforcing effect Effects 0.000 claims description 2
- 230000004308 accommodation Effects 0.000 claims 1
- 238000012423 maintenance Methods 0.000 abstract description 5
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 230000000694 effects Effects 0.000 abstract description 2
- 238000005507 spraying Methods 0.000 description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 5
- 229910052799 carbon Inorganic materials 0.000 description 5
- 239000007788 liquid Substances 0.000 description 3
- 239000000956 alloy Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 1
- 238000011900 installation process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- -1 seeds Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Classifications
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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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
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- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Definitions
- the utility model relates to a multi-rotor plant protection aircraft, in particular to an electric motor mounting seat for a multi-rotor plant protection aircraft.
- the plant protection aircraft is a drone for agricultural and forestry plant protection operations, and external spraying is used to achieve spraying operations such as spraying chemicals, seeds, powders, and the like.
- ESC directly affects the safe operation of plant protection aircraft.
- the ESC is generally installed inside the center plate of the aircraft, which is not conducive to the disassembly and maintenance of the ESC. Or directly install the ESC on the outside of the arm, so that the ESC is completely exposed to the external environment, which greatly reduces the appearance of the product and even affects the product quality and operational safety of the aircraft.
- the technical problem to be solved by the utility model is to provide an electric motor mounting seat for a multi-rotor plant protection aircraft that facilitates the disassembly, maintenance and protection of the ESC.
- an electric motor mounting seat for a multi-rotor plant protection aircraft which comprises a mounting seat and a connecting pipe, the mounting seat is at the top surface Forming a motor mounting position, and forming an accommodating space for installing an ESC;
- the connecting tube is disposed at one side of the mounting body, and includes a first semicircular tube and a first semicircular tube a second semicircular tube, a gap is formed between the first semicircular tube and the second semicircular tube, and a first fastening portion is formed at an end of the first semicircular tube at an end of the second semicircular tube Forming a second fastening portion corresponding to the first fastening portion, using the fastener to pierce the first fastening portion and the second fastening portion, and tightening by the fastener The first semicircular tube and the second semicircular tube.
- the mounting base includes a receiving seat and a cover plate, and the receiving seat is enclosed by a top plate and surrounding side plates, and the cover plate covers the receiving seat The opening.
- a plurality of oblong holes are formed in the top plate of the mounting seat corresponding to the mounting position of the motor.
- a reinforcing rib is formed in the accommodating space of the mounting seat corresponding to the mounting position of the motor.
- the first fastening portion includes a first protrusion formed on both sides of the end of the first semicircular tube
- the second fastening portion includes a second semicircle formed on the second semicircle a second bump on both sides of the end of the tube, one of the first bump and the second bump forming an internally threaded hole, and the other forming a circular hole corresponding to the position of the internally threaded hole .
- the first fastening portion includes a first protrusion formed on both sides of the end of the first semicircular tube
- the second fastening portion includes a second semicircle formed on the second semicircle a second bump on both sides of the end of the tube, and an internal threaded hole is formed on the first bump and the second bump.
- the first fastening portion includes a first protrusion formed on both sides of the end of the first semicircular tube
- the second fastening portion includes a second semicircle formed on the second semicircle a second bump on both sides of the end of the tube, and a circular hole is formed on the first bump and the second bump.
- a radially through locking hole is formed at the proximal end of the connecting pipe.
- the ESC has a metal heat sink, and the metal heat sink is embedded in the cover.
- the receiving seat is an aluminum alloy receiving seat
- the connecting pipe is an aluminum alloy connecting pipe
- the cover plate is a carbon fiber cover plate
- the electric motor mounting seat comprises a mounting base for mounting the electric adjusting motor and the motor, and a connecting pipe for fixing the electric adjusting motor mounting seat to the plant protection flying vehicle, and the electric adjusting device is mounted on the mounting seat.
- the electric adjusting device In the accommodating space, it is fixed on the carbon tube of the plant protection aircraft through the connecting pipe. This not only facilitates the disassembly and maintenance of the ESC, but also avoids splashing of the liquid on the ESC during the spraying operation of the plant protection aircraft. And cause damage.
- Figure 1 is a schematic exploded view of the ESC mount.
- Figure 2 is a side view showing the structure of the electric motor mount.
- Figure 3 is a bottom view of the electric motor mount.
- the electric motor mounting seat disclosed by the utility model is used as a component of a multi-rotor plant protection aircraft for installing an electronic governor and a motor.
- the electric motor mounting base includes a mounting base 10 and a connecting pipe 20 disposed at a side of the mounting base 10, wherein the mounting base 10 has a motor mounting position formed on the top surface.
- the connecting pipe 20 includes a first semicircular pipe 200 and a second semicircular pipe 201 opposite to the first semicircular pipe 200, the first semicircular pipe A gap 202 is formed between the 200 and the second semicircular tube 201, and a first fastening portion 203 is formed at an end of the first semicircular tube 200, and a corresponding portion is formed at an end of the second semicircular tube 201.
- the second fastening portion 204 of the first fastening portion 203 is fastened to the first fastening portion 203 and the second fastening portion 204 by using a fastener 205 such as a screw or the like, by the fastener
- the first semicircular tube 200 and the second semicircular tube 201 are tightened so that the electric motor mount can be fixedly mounted at a target position, such as at the arm of the multi-rotor plant protection aircraft.
- the mounting base 10 includes a receiving base 102 and a cover plate 103.
- the receiving base 102 is enclosed by the top plate 1020 and the surrounding side plates 1021, thereby forming a
- the housing 103 can be used to receive the accommodating space 101 of the ESC, and the cover plate 103 is closed to the opening of the accommodating seat 102, so that the accommodating seat 102 is formed with a closed accommodating space 101 to avoid spraying on the multi-rotor plant protection aircraft.
- the liquid splashed on the ESC causing damage to the ESC.
- the first fastening portion 203 includes a first protrusion 2030 formed on two sides of the end of the first semicircular tube 200, and the first protrusion 2030 is formed with an internally threaded hole 2031.
- the second fastening portion 204 includes a second protrusion 2040 formed on two sides of the end of the second semicircular tube 201.
- the second protrusion 2040 is formed with a position of the internal thread hole 2031 of the first protrusion 2030.
- Corresponding circular holes are screwed into the circular holes and screwed into the internally threaded holes 2031, and the first semicircular tube 200 and the second semicircular tube 201 can be tightened, and the electric The motor mount is clamped and fixed to the arm of the multi-rotor plant protection aircraft. It is to be noted that in other embodiments, a circular hole may be disposed on the first protrusion 2030, and an internal threaded hole is disposed on the second protrusion 2040, or the first protrusion 2030 and the second protrusion are disposed on the second protrusion 2040.
- An internal threaded hole is formed in each of the blocks 2040, and the upper semicircular tube 200 and the lower semicircular tube 201 are tightened by screwing of the screws, thereby fastening the electric motor mounting seat to the target position.
- a circular hole may be provided on the first bump 2030 and the second bump 2040 without providing an internally threaded hole, and a bolt is used to achieve clamping of the two.
- a radially through locking hole 206 is formed at the proximal end of the connecting tube 20, and the first fastening portion 203 and the second fastening portion 204 are pierced by the fastener 205 to fix the connecting tube 20 to the plant protection.
- the locking bolt is further used to lock through the locking hole 205 (of course, a radial through hole is formed at the corresponding position on the carbon tube of the arm), thus preventing When the fastener 205 is loose, the electric motor mount is turned over and affects the flight stability of the plant protection aircraft.
- a plurality of oblong holes 104 are formed in the top plate 1020 of the mount 10 corresponding to the motor mounting position 100.
- the motor provided at the motor mounting position 100 can be locked by screwing through the oblong hole 104.
- the ribs 105 are formed in the accommodating space 101 of the mounting seat 10 corresponding to the motor mounting position 100.
- the wall thickness of the accommodating seat 102 can be reduced, and sufficient structural strength is ensured.
- the weight of the ESC mount can be minimized and the performance of the plant protection aircraft can be improved.
- the ESC is provided with a metal heat sink 105.
- the metal heat sink 105 is disposed to perform electrical adjustment on the inside of the mount 10. Cooling.
- the electric motor mount is made of a suitable material to meet various performance requirements.
- the receptacle 102 is made of an aluminum alloy material
- the connecting tube 20 is also made of an aluminum alloy material.
- the cover plate 103 can be made of a carbon fiber material.
- the connecting pipe 20 is first inserted into the carbon tube of the arm of the plant protection aircraft, and the first semicircular pipe 200 and the second semicircular pipe 201 of the connecting pipe 20 are tightened by using the fastener 205 to initially realize the installation of the electric motor.
- Fixing the seat after horizontally aligning the mounting seat, use the locking bolt to pass through the locking hole 206 to further lock the electric motor mounting seat; and place the motor in the motor mounting position at the top surface of the mounting base 10.
- 100 and using screws to lock and fix through the oblong hole 103; the metal heat sink 106 of the electronic governor is embedded in the cover plate 103, and then the cover plate 103 is closed to the receiving seat 102, thereby completing the electric motor
- the installation process of the mount is first inserted into the carbon tube of the arm of the plant protection aircraft, and the first semicircular pipe 200 and the second semicircular pipe 201 of the connecting pipe 20 are tightened by using the fastener 205 to initially realize the installation of the electric motor.
- Fixing the seat
- the electric motor mounting seat disclosed by the utility model comprises a mounting seat for mounting an electric adjusting motor and a connecting pipe for fixing the electric adjusting motor mounting seat to the plant protection aircraft, and mounting the electric adjusting device to the mounting seat. In the space, it is fixed on the carbon tube of the plant protection aircraft through the connecting pipe. This not only facilitates the disassembly and maintenance of the ESC, but also avoids the damage caused by the splashing of the liquid on the ESC during the spraying operation of the plant protection aircraft. .
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Motor Or Generator Frames (AREA)
Abstract
一种用于多旋翼植保飞行器的电调电机安装座，其包括有一安装座（10）和一连接管（20），所述安装座（10）在顶面处形成有电机安装位（100），而在内部形成有用于安装电调的容置空间（101）；所述连接管（20）设于所述安装座（10）一侧处，包括有一第一半圆管（200）及一与所述第一半圆管相对的第二半圆管（201），所述第一半圆管（200）与第二半圆管（201）之间形成有间隙（202），于所述第一半圆管（200）的末端处形成有第一紧固部（203），于所述第二半圆管（201）的末端处形成有对应于所述第一紧固部的第二紧固部（204），使用紧固件（205）穿接所述第一紧固部（203）和第二紧固部（204），而藉由所述紧固件（205）以拉紧所述第一半圆管（200）和第二半圆管（201）。本装置具有利于电调的拆装维护和保护的有益技术效果。
Description
技术领域
本实用新型涉及多旋翼植保飞行器，尤其涉及一种用于多旋翼植保飞行器的电调电机安装座。
背景技术
植保飞行器是用于农林植物保护作业的无人驾驶飞机，通过外部控制来实现喷洒作业，例如喷洒药剂、种子、粉剂等。电调作为控制直流电机运行的关键器件，其安装固定方式直接影响到植保飞行器的安全运行。现有技术的多旋翼植保飞行器，其电调一般安装在飞行器的中心板内部，不利于电调的拆装维护。抑或将电调直接裸露安装在机臂外侧，如此则使得电调完全暴露在外部环境，造成产品外观大打折扣，甚至影响到飞行器的产品品质和运行安全。
发明内容
本实用新型所要解决的技术问题在于提供一种利于电调的拆装维护和保护的用于多旋翼植保飞行器的电调电机安装座。
为解决上述技术问题，本实用新型采用如下所述的技术方案：一种用于多旋翼植保飞行器的电调电机安装座，其包括有一安装座和一连接管，所述安装座在顶面处形成有电机安装位，而在内部形成有用于安装电调的容置空间；所述连接管设于所述安装座一侧处，包括有一第一半圆管及一与所述第一半圆管相对的第二半圆管，所述第一半圆管与第二半圆管之间形成有间隙，于所述第一半圆管的末端处形成有第一紧固部，于所述第二半圆管的末端处形成有对应于所述第一紧固部的第二紧固部，使用紧固件穿接所述第一紧固部和第二紧固部，而藉由所述紧固件以拉紧所述第一半圆管和第二半圆管。
上述电调电机安装座中，所述安装座包括有一容置座及一盖板，所述容置座由顶板及四周侧板围合而成，所述盖板盖合于所述容置座的开口处。
上述电调电机安装座中，所述安装座的顶板上对应于所述电机安装位处形成有若干长圆孔。
上述电调电机安装座中，所述安装座的容置空间内对应于所述电机安装位处形成有加强筋。
上述电调电机安装座中，所述第一紧固部包括有形成于所述第一半圆管末端两侧的第一凸块，所述第二紧固部包括有形成于所述第二半圆管末端两侧的第二凸块，所述第一凸块和第二凸块两者之中，其中一者形成内螺纹孔，另一者形成有于内螺纹孔位置相对应的圆形孔。
上述电调电机安装座中，所述第一紧固部包括有形成于所述第一半圆管末端两侧的第一凸块，所述第二紧固部包括有形成于所述第二半圆管末端两侧的第二凸块，所述第一凸块和第二凸块之上均形成有内螺纹孔。
上述电调电机安装座中，所述第一紧固部包括有形成于所述第一半圆管末端两侧的第一凸块，所述第二紧固部包括有形成于所述第二半圆管末端两侧的第二凸块，所述第一凸块和第二凸块之上均形成有圆形孔。
上述电调电机安装座中，所述连接管近末端处形成有一径向贯通的锁紧孔。
上述电调电机安装座中，电调自带有一金属散热板，所述金属散热板嵌设于所述盖板。
上述电调电机安装座中，所述容置座为铝合金容置座，所述连接管为铝合金连接管，所述盖板为碳纤维盖板。
本实用新型的有益技术效果在于：电调电机安装座包括有一用于安装电调和电机的安装座和一用于将电调电机安装座固定于植保飞行器的连接管，将电调安装于安装座的容置空间内，再通过连接管固定于植保飞行器的机臂碳管上，如此，不仅便于电调的拆装维护，而且可避免在植保飞行器的喷洒作业过程中药液溅落在电调上而造成损害。
附图说明
图1为电调电机安装座的分解结构示意图。
图2为电调电机安装座的侧视结构示意图。
图3为电调电机安装座的仰视结构示意图。
具体实施方式
为使本领域的普通技术人员更加清楚地理解本实用新型的目的、技术方案和优点，以下结合附图和实施例对本实用新型做进一步的阐述。
本实用新型所公开的电调电机安装座作为多旋翼植保飞行器的组成部件，以供于安装电子调速器和电机。参阅附图1~3所示，该电调电机安装座包括一安装座10及一设于该安装座10一侧处的连接管20，其中，该安装座10在顶面形成有电机安装位100，而在内部形成有用于安装电调的容置空间101，该连接管20包括有一第一半圆管200及一与该第一半圆管200相对的第二半圆管201，该第一半圆管200与第二半圆管201两者之间形成有间隙202，于该第一半圆管200的末端处形成有第一紧固部203，于该第二半圆管201的末端处形成有对应于该第一紧固部203的第二紧固部204，使用诸如螺丝等之类的紧固件205穿接该第一紧固部203和第二紧固部204，藉由该紧固件以拉紧该第一半圆管200和第二半圆管201，从而可将电调电机安装座固定安装于目标位置处，例如多旋翼植保飞行器的机臂处。
如附图所示，在一些优选实施例中，该安装座10包括有一容置座102及一盖板103，该容置座102由顶板1020及四周侧板1021围合而成，从而构成一可以用于收纳电调的容置空间101，而盖板103则盖合于该容置座102的开口，从而使得容置座102形成有封闭的容置空间101，避免在多旋翼植保飞行器喷洒作业过程中药液溅落于电调上，而造成电调的损害。
在附图所示的实施例中，该第一紧固部203包括有形成于该第一半圆管200末端两侧的第一凸块2030，该第一凸块2030上形成有内螺纹孔2031，该第二紧固部204包括有形成于该第二半圆管201末端两侧的第二凸块2040，该第二凸块2040上形成有与该第一凸块2030的内螺纹孔2031位置相对应的圆形孔（图中没有示出），使用螺丝穿过圆形孔而螺合于内螺纹孔2031，可拉紧该第一半圆管200和第二半圆管201，而将该电调电机安装座夹紧固定于多旋翼植保飞行器的机臂处。诚然，在其他的实施例中，也可于该第一凸块2030上设置圆形孔，而于该第二凸块2040上设置内螺纹孔，或者于该第一凸块2030和第二凸块2040上均形成内螺纹孔，通过螺丝的螺合来拉紧该上半圆管200和下半圆管201，从而将电调电机安装座紧固于目标位置上。而在另外的实施例中，也可于该第一凸块2030和第二凸块2040上设置圆形孔，而不设置内螺纹孔，使用螺栓以实现两者的夹紧。
优选地，于该连接管20近末端处形成有一径向贯通的锁紧孔206，使用紧固件205穿设第一紧固部203、第二紧固部204而将连接管20固定于植保飞行器的机臂碳管后，再进一步使用锁紧螺栓穿过锁紧孔205进行锁紧（当然，机臂碳管上在相应的位置处也形成有径向通孔），如此，可防止在紧固件205发生松动的情况下出现电调电机安装座翻转而影响植保飞行器的飞行稳定性。
参阅图1和图2所示，该安装座10的顶板1020上对应于电机安装位100处形成有若干长圆孔104。安装电机时，可使用螺丝穿过该长圆孔104而将设于电机安装位100的电机锁紧固定。
优选地，该安装座10的容置空间101内对应于电机安装位100处形成有加强筋105，通过加强筋105的设置，可减小容置座102的壁厚，在保证足够结构强度的同时可最大限度地减去电调电机安装座的重量，提升植保飞行器的性能。
参阅图1所示，在本实用新型的一些优选实施例中，电调自带有一金属散热板105，藉由该金属散热板105的设置，可对安装于该安装座10内部的电调进行散热。
该电调电机安装座选用合适的材质制备，以满足其各种性能的需求，在一些优选实施例中，该容置座102采用铝合金材料制备，连接管20也采用铝合金材料制备，而盖板103则可采用碳纤维材料制备。
安装时，先将连接管20插接于植保飞行器的机臂碳管上，使用紧固件205拉紧该连接管20的第一半圆管200和第二半圆管201而初步实现电调电机安装座的固定，在对安装座进行水平校准后，使用锁紧螺栓穿过锁紧孔206而进一步将电调电机安装座锁紧；将电机置放于该安装座10顶面处的电机安装位100上，并使用螺丝通过长圆孔103进行锁紧固定；将电子调速器的金属散热板106嵌设于盖板103，再将盖板103盖合于容置座102，从而完成电调电机安装座的安装过程。
本实用新型所公开的电调电机安装座包括有一用于安装电调和电机的安装座和一用于将电调电机安装座固定于植保飞行器的连接管，将电调安装于安装座的容置空间内，再通过连接管固定于植保飞行器的机臂碳管上，如此，不仅便于电调的拆装维护，而且可避免在植保飞行器的喷洒作业过程中药液溅落在电调上而造成损害。
以上所述仅为本实用新型的优选实施例，而非对本实用新型做任何形式上的限制。本领域的技术人员可在上述实施例的基础上施以各种等同的更改和改进，凡在权利要求范围内所做的等同变化或修饰，均应落入本实用新型的保护范围之内。
Claims (10)
- 一种用于多旋翼植保飞行器的电调电机安装座，其特征在于，所述电调电机安装座包括有：一安装座，其在顶面处形成有电机安装位，而在内部形成有用于安装电调的容置空间；一设于所述安装座一侧处的连接管，其包括有一第一半圆管及一与所述第一半圆管相对的第二半圆管，所述第一半圆管与第二半圆管之间形成有间隙，于所述第一半圆管的末端处形成有第一紧固部，于所述第二半圆管的末端处形成有对应于所述第一紧固部的第二紧固部，使用紧固件穿接所述第一紧固部和第二紧固部，而藉由所述紧固件以拉紧所述第一半圆管和第二半圆管。
- 如权利要求1所述的电调电机安装座，其特征在于，所述安装座包括有一容置座及一盖板，所述容置座由顶板及四周侧板围合而成，所述盖板盖合于所述容置座的开口处。
- 如权利要求2所述的电调电机安装座，其特征在于，所述安装座的顶板上对应于所述电机安装位处形成有若干长圆孔。
- 如权利要求2所述的电调电机安装座，其特征在于，所述安装座的容置空间内对应于所述电机安装位处形成有加强筋。
- 如权利要求1所述的电调电机安装座，其特征在于，所述第一紧固部包括有形成于所述第一半圆管末端两侧的第一凸块，所述第二紧固部包括有形成于所述第二半圆管末端两侧的第二凸块，所述第一凸块和第二凸块两者之中，其中一者形成内螺纹孔，另一者形成有于内螺纹孔位置相对应的圆形孔。
- 如权利要求1所述的电调电机安装座，其特征在于，所述第一紧固部包括有形成于所述第一半圆管末端两侧的第一凸块，所述第二紧固部包括有形成于所述第二半圆管末端两侧的第二凸块，所述第一凸块和第二凸块之上均形成有内螺纹孔。
- 如权利要求1所述的电调电机安装座，其特征在于，所述第一紧固部包括有形成于所述第一半圆管末端两侧的第一凸块，所述第二紧固部包括有形成于所述第二半圆管末端两侧的第二凸块，所述第一凸块和第二凸块之上均形成有圆形孔。
- 如权利要求1所述的电调电机安装座，其特征在于，所述连接管近末端处形成有一径向贯通的锁紧孔。
- 如权利要求2所述的电调电机安装座，其特征在于，电调自带有一金属散热板，所述金属散热板嵌设于所述盖板。
- 如权利要求2所述的电调电机安装座，其特征在于，所述容置座为铝合金容置座，所述连接管为铝合金连接管，所述盖板为碳纤维盖板。
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| CN206528630U (zh) * | 2017-02-24 | 2017-09-29 | 深圳市大疆创新科技有限公司 | 动力套装及无人飞行器 |
| CN110876266A (zh) * | 2018-12-03 | 2020-03-10 | 深圳市大疆创新科技有限公司 | 电子调速器、动力装置及无人飞行器 |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3979087A (en) * | 1975-07-02 | 1976-09-07 | United Technologies Corporation | Engine mount |
| CN205113725U (zh) * | 2015-09-01 | 2016-03-30 | 金龙 | 一种无人机电机座 |
| CN105599895A (zh) * | 2016-01-29 | 2016-05-25 | 浙江智天科技有限公司 | 多轴飞行器 |
| CN205872489U (zh) * | 2016-07-29 | 2017-01-11 | 深圳亿天航科技有限公司 | 用于多旋翼植保飞行器的电调电机安装座 |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3979087A (en) * | 1975-07-02 | 1976-09-07 | United Technologies Corporation | Engine mount |
| CN205113725U (zh) * | 2015-09-01 | 2016-03-30 | 金龙 | 一种无人机电机座 |
| CN105599895A (zh) * | 2016-01-29 | 2016-05-25 | 浙江智天科技有限公司 | 多轴飞行器 |
| CN205872489U (zh) * | 2016-07-29 | 2017-01-11 | 深圳亿天航科技有限公司 | 用于多旋翼植保飞行器的电调电机安装座 |
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