WO2023024049A1 - 一种具有加热功能的航空航天用高效换气装置 - Google Patents

一种具有加热功能的航空航天用高效换气装置 Download PDF

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Publication number
WO2023024049A1
WO2023024049A1 PCT/CN2021/114863 CN2021114863W WO2023024049A1 WO 2023024049 A1 WO2023024049 A1 WO 2023024049A1 CN 2021114863 W CN2021114863 W CN 2021114863W WO 2023024049 A1 WO2023024049 A1 WO 2023024049A1
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WIPO (PCT)
Prior art keywords
fixedly installed
storage tank
water storage
aerospace
air
Prior art date
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PCT/CN2021/114863
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English (en)
French (fr)
Inventor
李明富
蔡昌勇
莫磊
朱静
王雷涛
陆海燕
Original Assignee
成都航空职业技术学院
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Application filed by 成都航空职业技术学院 filed Critical 成都航空职业技术学院
Priority to PCT/CN2021/114863 priority Critical patent/WO2023024049A1/zh
Publication of WO2023024049A1 publication Critical patent/WO2023024049A1/zh

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Classifications

    • 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, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • 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, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D13/08—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned the air being heated or cooled
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/46—Arrangements or adaptations of devices for control of environment or living conditions
    • B64G1/48—Arrangements or adaptations of devices for control of environment or living conditions for treatment of the atmosphere

Definitions

  • the invention relates to the technical field of ventilation equipment, in particular to a high-efficiency ventilation device for aerospace with a heating function.
  • Aviation refers to the navigation activities of aircraft in the earth's atmosphere
  • spaceflight refers to the navigation activities of aircraft in space outside the atmosphere. Aerospace has greatly changed the structure of transportation.
  • aerospace has become the most active and influential field of science and technology in the 21st century. The major achievements in this field indicate the high development of human civilization and also It represents the advanced level of a country's science and technology.
  • the purpose of the present invention is to solve the problem that most of the existing ventilators lack the function of heating and humidifying, resulting in poor air quality, and propose a high-efficiency ventilator for aerospace with heating function.
  • a high-efficiency ventilation device for aerospace with heating function including a box body, a support plate is fixedly installed at the bottom of the box body, and a support plate is fixedly installed at the bottom of the support plate
  • the water storage tank, the inside of the water storage tank is installed with a screw auger, the inside of the box is fixed with a suction fan and an air inlet head, the air inlet of the suction fan is connected with the air inlet head with the same air inlet pipe, and the inside of the box is
  • a swing rod is installed on the outer side to rotate, and the first round shaft is fixedly installed on the front side of the swing rod.
  • the second circular shaft is installed, and the outer movable sleeve of the second circular shaft is provided with a second horizontal frame.
  • the air outlet head, the air outlet of the suction fan and the outside of the air outlet head are connected with one end of the air outlet pipe.
  • the inside of the box is fixedly installed with a heating chamber, and the other ends of the two air outlet pipes are respectively connected to the left and right sides of the heating chamber.
  • a disc is installed on the top of the outer side of the support plate, and a water delivery ring is installed on the top of the support plate. The water outlet of the water delivery ring is connected with multiple spray heads.
  • the other end of one of the traction ropes is fixedly installed with the top of the spring, the bottom end of the spring is fixedly installed on the top of the support plate, the other end of the other traction rope is rotatably installed on the front side of the disc, and the water storage tank
  • the outside of one bevel gear in the two bevel gears is fixedly connected with one end of the auger, and the back side of the other bevel gear and the back side of the turntable are connected with the circle.
  • the rear side of the disc is all coaxially driven with sprockets, and the three sprockets are connected with the same chain, and the outer top of the water storage tank communicates with the outer side of the water delivery ring with the same water delivery pipe.
  • a filter screen is fixedly installed inside the box body, and an air inlet is provided on the outside of the box body.
  • an air inlet is provided on the outside of the box body.
  • a motor is fixedly installed on the outside of the water storage tank, and the other end of the auger extends to the outside of the water storage tank and is fixedly connected with the output shaft of the motor.
  • the synchronous rotation makes the air outlet head and the spray head swing synchronously, and can heat and humidify the air.
  • a support platform is fixedly installed on the outside of the water storage tank, the motor is fixedly installed on the top of the support platform, and the motor is provided with a certain support function through the provided support platform.
  • a hollow rod is fixedly installed on the outer top of the box, and the outer side of the connecting rod is movably abutted against the inner side of the hollow rod.
  • the provided hollow rod it plays a certain guiding role for the vertical movement of the connecting rod .
  • a through hole is opened on the top of the support plate, and the water delivery pipe is located inside the through hole and passes through the provided through hole, thereby providing a certain range of motion for the water delivery pipe.
  • a water inlet valve is connected to the top of the water storage tank, and support columns are fixedly installed on both sides of the bottom of the support plate, and the set support columns provide certain support for the entire device.
  • a rectangular plate is fixedly installed on the outside of the water storage tank, and the bevel gear is rotatably installed on the front side of the rectangular plate, and the bevel gear provides a position for rotatable installation through the provided rectangular plate.
  • the high-efficiency ventilation device for aerospace with a heating function through the set sprocket, the work of the motor makes the auger rotate, so that the bevel gear rotates to drive the three sprockets to rotate synchronously,
  • the turntable and the disc rotate synchronously, and the rotation of the turntable makes the air outlet head swing, which can increase the ventilation range of the internal environment.
  • the rotation of the disc and the swing of the spray head can increase the range of humidification, thereby improving the air quality.
  • the internal air quality of the unit through the set sprocket, the work of the motor makes the auger rotate, so that the bevel gear rotates to drive the three sprockets to rotate synchronously,
  • the turntable and the disc rotate synchronously, and the rotation of the turntable makes the air outlet head swing, which can increase the ventilation range of the internal environment.
  • the rotation of the disc and the swing of the spray head can increase the range of humidification, thereby improving the air quality.
  • the internal air quality of the unit
  • the design of the invention is reasonable, and the spray head and the air outlet pipe can be oscillated synchronously through the set turntable and disc, so that the range of heating and humidifying the air can be increased, and the quality of the air inside the aviation device can be guaranteed.
  • Fig. 1 is a schematic structural view of a high-efficiency ventilation device for aerospace with a heating function proposed by the present invention.
  • Fig. 2 is a rear view of a high-efficiency ventilation device for aerospace with heating function proposed by the present invention.
  • Fig. 3 is a structural schematic diagram of part A of a high-efficiency ventilation device for aerospace with a heating function proposed by the present invention.
  • Fig. 4 is a schematic structural view of part B of a high-efficiency ventilation device for aerospace with a heating function proposed by the present invention.
  • Fig. 5 is a structural schematic diagram of part C of a high-efficiency ventilation device for aerospace with heating function proposed by the present invention.
  • a high-efficiency ventilation device for aerospace with heating function includes a box body 1, a support plate 2 is fixedly installed at the bottom of the box body 1, and a water storage tank 3 is fixedly installed at the bottom of the support plate 2, The inside of the water storage tank 3 is rotatably equipped with an auger 21, and the inside of the box body 1 is fixedly installed with a suction fan 4 and an air intake head 6.
  • the outer side of the box body 1 is rotatably equipped with a swing lever 8, the front side of the swing lever 8 is fixedly installed with a first round shaft 10, and the outer side of the first round shaft 10 is movable cover with a first horizontal frame 11, the outer side of the box body 1
  • the top is rotatably equipped with a turntable 12, and the front side of the turntable 12 is fixedly equipped with a second round shaft 13, and the outer side of the second round shaft 13 is movably provided with a second horizontal frame 14, and the top of the first horizontal frame 11 is connected to the second horizontal frame.
  • the same connecting rod 15 is fixedly installed at the bottom of 14, and an air outlet head 9 is fixedly installed at one end of the swing rod 8.
  • the air outlet of the suction fan 4 and the outside of the air outlet head 9 are connected with one end of the air outlet pipe 7, and the inside of the box body 1
  • a heating chamber 28 is fixedly installed, and the other ends of the two air outlet pipes 7 are respectively connected to the left and right sides of the heating chamber 28.
  • the outer top of the box body 1 is rotatably installed with a disc 16, and the top of the support plate 2 is rotatably installed with a water delivery ring. 18.
  • the water outlet of the water transfer ring 18 is connected with a plurality of spray heads 19, and the top and bottom of the water transfer ring 18 are fixedly equipped with one end of a traction rope 17, and the other end of one of the two traction ropes 17 is fixed.
  • the top end of the spring 20 is installed, the bottom end of the spring 20 is fixedly installed on the top of the support plate 2, the other end of the other traction rope 17 is rotatably installed on the front side of the disc 16, and the outer side of the water storage tank 3 is rotatably installed with two Bevel gear 22, two bevel gears 22 mesh with each other, the outside of one bevel gear 22 in the two bevel gears 22 is fixedly connected with one end of the screw auger 21, the rear side of the other bevel gear 22, the rear side of the rotating disk 12 and The rear side of the disk 16 is coaxially driven with a sprocket 23, and the three sprockets 23 are connected with the same chain 24, and the outer top of the water storage tank 3 is connected with the outer side of the water delivery ring 18 with the same water delivery pipe 27 .
  • a filter screen 26 is fixedly installed inside the box body 1, and an air inlet is provided on the outside of the box body 1. Through the filter screen 26 provided, a certain filtering work can be performed on the sucked air, thereby ensuring that the aviation device Internal air quality.
  • the outside of water storage tank 3 is fixedly installed with motor 25, and the other end of screw auger 21 extends to the outside of water storage tank 3 and is fixedly connected with the output shaft of motor 25, by the motor 25 that is set, the motor 25
  • the work makes the disk 16 and the turntable 12 rotate synchronously, so that the air outlet head 9 and the spray head 19 swing synchronously, and the work of heating and humidifying the air can be performed.
  • a support platform is fixedly installed on the outside of the water storage tank 3, and the motor 25 is fixedly installed on the top of the support platform, and the motor 25 is provided with a certain support function through the provided support platform.
  • a hollow rod is fixedly installed on the top of the outer side of the box body 1, and the outer side of the connecting rod 15 is movable against the inner side of the hollow rod. role.
  • a through hole is opened on the top of the support plate 2 , and the water delivery pipe 27 is located inside the through hole, and passes through the provided through hole, thereby providing a certain range of motion for the water delivery pipe 27 .
  • a water inlet valve is connected to the top of the water storage tank 3, and support columns are fixedly installed on both sides of the bottom of the support plate 2, and a certain supporting effect is provided for the whole device through the set support columns.
  • a rectangular plate is fixedly installed on the outside of the water storage tank 3, and the bevel gear 22 is rotatably installed on the front side of the rectangular plate, and the bevel gear 22 is provided with a position for rotatable installation through the provided rectangular plate.
  • the working principle of this ventilation device is as follows: drive the suction fan 4, thereby making the outside air enter the inside of the air outlet pipe 7, through the heating work of the heating chamber 28, thereby being ejected by the air outlet head 9, and the internal air of the aviation device can be discharged.
  • the work of the motor 25 makes the auger 21 rotate, so that the water inside the water storage tank 3 can enter the inside of the water delivery ring 18, and then be sprayed out by a plurality of spray nozzles 19, thereby The internal environment is humidified.
  • the rotation of the screw auger 21 makes the two bevel gears 22 rotate, thereby driving the three sprockets 23 to rotate synchronously, so that the turntable 12 and the disc 16 rotate synchronously.
  • the rotation of the turntable 12 makes the second The circular shaft 13 rotates, so that the second horizontal frame 14 obtains vertical movement, and the first horizontal frame 11 obtains the same vertical reciprocating motion through the provided connecting rod 15, thereby pushing the first circular shaft 10 to swing, Therefore, the swing rod 8 is reciprocally oscillating, so that the air outlet head 9 is oscillating, so that the range of ventilation to the internal environment can be increased.
  • the rotation of the disc 16 makes the traction rope 17 work, so that the water delivery ring 18 Swing, thereby driving a plurality of spray heads 19 to swing, can increase the range of humidification, secondly, the hot air output by the air outlet head 9 can blow the water mist sprayed by the spray heads 19 to a farther position, thereby improving the internal air of the aviation device. quality.

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  • Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pulmonology (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Biodiversity & Conservation Biology (AREA)
  • Environmental & Geological Engineering (AREA)
  • Environmental Sciences (AREA)
  • Toxicology (AREA)
  • Remote Sensing (AREA)
  • Air Humidification (AREA)

Abstract

发明属于换气设备技术领域，尤其为一种具有加热功能的航空航天用高效换气装置，针对现有的换气装置大多缺少加热加湿的功能，从而造成空气质量不佳的问题，现提出如下方案，其包括箱体，箱体的底部固定安装有支撑板，支撑板的底部固定安装有储水罐，储水罐的内部转动安装有螺旋绞龙，箱体的内部固定安装有吸风机与进气头，吸风机的进气口与进气头连通有同一个进气管，箱体的外侧转动安装有摆动杆，摆动杆的前侧固定安装有第一圆轴，第一圆轴的外侧活动套设有第一水平框。本发明设计合理，通过设置的转盘与圆盘，使得喷雾头与出气管能够同步的进行摆动工作，能够增大对空气的加热与加湿的范围，保证航空装置内部空气的质量。

Description

一种具有加热功能的航空航天用高效换气装置 技术领域
本发明涉及换气设备技术领域，尤其涉及一种具有加热功能的航空航天用高效换气装置。
 背景技术
航空指飞行器在地球大气层内的航行活动，航天指飞行器在大气层外宇宙空间的航行活动。航空航天大大改变了交通运输的结构，经过近百年来的快速发展，航空航天已经成为21世纪最活跃和最有影响的科学技术领域，该领域取得的重大成就标志着人类文明的高度发展，也表征着一个国家科学技术的先进水平。
现有的换气装置大多缺少加热加湿的功能，从而造成空气质量不佳的缺点，因此我们提出了一种具有加热功能的航空航天用高效换气装置用于解决上述问题。
 技术问题
本发明的目的是为了解决现有的换气装置大多缺少加热加湿的功能，从而造成空气质量不佳的缺点，而提出的一种具有加热功能的航空航天用高效换气装置。
 技术解决方案
为了实现上述目的，本发明采用了如下技术方案：一种具有加热功能的航空航天用高效换气装置，包括箱体，所述箱体的底部固定安装有支撑板，支撑板的底部固定安装有储水罐，储水罐的内部转动安装有螺旋绞龙，箱体的内部固定安装有吸风机与进气头，吸风机的进气口与进气头连通有同一个进气管，箱体的外侧转动安装有摆动杆，摆动杆的前侧固定安装有第一圆轴，第一圆轴的外侧活动套设有第一水平框，箱体的外侧顶部转动安装有转盘，转盘的前侧固定安装有第二圆轴，第二圆轴的外侧活动套设有第二水平框，第一水平框的顶部与第二水平框的底部固定安装有同一个连接杆，摆动杆的一端固定安装有出气头，吸风机的出气口与出气头的外侧均连通有出气管的一端，箱体的内部固定安装有加热室，两个出气管的另一端分别连通在加热室的左右两侧，箱体的外侧顶部转动安装有圆盘，支撑板的顶部转动安装有输水环，输水环的出水口连通有多个喷雾头，输水环的顶部与底部均固定安装有牵引绳的一端，两个牵引绳中的一个牵引绳的另一端固定安装有弹簧的顶端，弹簧的底端固定安装在支撑板的顶部，另一个牵引绳的另一端转动安装在圆盘的前侧，储水罐的外侧转动安装有两个锥齿轮，两个锥齿轮相互啮合，两个锥齿轮中的一个锥齿轮的外侧与螺旋绞龙的一端固定连接，另一个锥齿轮的后侧、转盘的后侧与圆盘的后侧均同轴传动有链轮，三个链轮上传动连接有同一个链条，储水罐的外侧顶部与输水环的外侧连通有同一个输水管。
 有益效果
优选的，所述箱体的内部固定安装有过滤网，箱体的外侧开设有进风口，通过设置的过滤网，从而能够对吸入的空气进行一定的过滤的工作，从而保证航空装置内部的空气质量。
优选的，所述储水罐的外侧固定安装有电机，螺旋绞龙的另一端延伸至储水罐的外侧并与电机的输出轴固定连接，通过设置的电机，电机的工作使得圆盘与转盘同步转动，从而使得出气头头与喷雾头同步摆动，能够对空气进行加热加湿的工作。
优选的，所述储水罐的外侧固定安装有支撑台，电机固定安装在支撑台的顶部，通过设置的支撑台，从而为电机提供一定的支撑作用。
优选的，所述箱体的外侧顶部固定安装有中空杆，连接杆的外侧活动抵接在中空杆的内侧，通过设置的中空杆，从而为连接杆的竖直运动起到一定的导向的作用。
优选的，所述支撑板的顶部开设有通孔，输水管的位于通孔的内部，通过设置的通孔，从而为输水管提供一定的活动范围。
优选的，所述储水罐的顶部连通有进水阀，支撑板的底部两侧均固定安装有支撑柱，通过设置的支撑柱，从而为整个装置提供一定的支撑作用。
优选的，所述储水罐的外侧固定安装有矩形板，锥齿轮转动安装在矩形板的前侧，通过设置的矩形板，从而为锥齿轮提供转动安装的位置。
本发明中，所述的一种具有加热功能的航空航天用高效换气装置，通过设置的链轮，电机的工作使得螺旋绞龙转动，使得锥齿轮通过转动，带动三个链轮同步转动，使得转盘与圆盘同步转动，转盘的转动使得出气头得到摆动工作，从而能够增大对内部环境的换气范围，其次圆盘的转动喷雾头摆动，能够增大加湿的范围，从而能够改善航空装置的内部空气质量。
本发明设计合理，通过设置的转盘与圆盘，从而使得喷雾头与出气管能够同步的进行摆动工作，从而能够增大对空气的加热与加湿的范围，保证航空装置的内部空气的质量。
 附图说明
图1为本发明提出的一种具有加热功能的航空航天用高效换气装置的结构示意图。
图2为本发明提出的一种具有加热功能的航空航天用高效换气装置的后视图。
图3为本发明提出的一种具有加热功能的航空航天用高效换气装置的A部分的结构示意图。
图4为本发明提出的一种具有加热功能的航空航天用高效换气装置的B部分的结构示意图。
图5为本发明提出的一种具有加热功能的航空航天用高效换气装置的C部分的结构示意图。
图中：1、箱体；2、支撑板；3、储水罐；4、吸风机；5、进气管；6、进气头；7、出气管；8、摆动杆；9、出气头；10、第一圆轴；11、第一水平框；12、转盘；13、第二圆轴；14、第二水平框；15、连接杆；16、圆盘；17、牵引绳；18、输水环；19、喷雾头；20、弹簧；21、螺旋绞龙；22、锥齿轮；23、链轮；24、链条；25、电机；26、过滤网；27、输水管；28、加热室。
 本发明的实施方式
下面将结合本发明实施例中的附图，对本发明实施例中的技术方案进行清楚、完整地描述，显然，所描述的实施例仅仅是本发明一部分实施例，而不是全部的实施例。
参照图1-5，一种具有加热功能的航空航天用高效换气装置，包括箱体1，箱体1的底部固定安装有支撑板2，支撑板2的底部固定安装有储水罐3，储水罐3的内部转动安装有螺旋绞龙21，箱体1的内部固定安装有吸风机4与进气头6，吸风机4的进气口与进气头6连通有同一个进气管5，箱体1的外侧转动安装有摆动杆8，摆动杆8的前侧固定安装有第一圆轴10，第一圆轴10的外侧活动套设有第一水平框11，箱体1的外侧顶部转动安装有转盘12，转盘12的前侧固定安装有第二圆轴13，第二圆轴13的外侧活动套设有第二水平框14，第一水平框11的顶部与第二水平框14的底部固定安装有同一个连接杆15，摆动杆8的一端固定安装有出气头9，吸风机4的出气口与出气头9的外侧均连通有出气管7的一端，箱体1的内部固定安装有加热室28，两个出气管7的另一端分别连通在加热室28的左右两侧，箱体1的外侧顶部转动安装有圆盘16，支撑板2的顶部转动安装有输水环18，输水环18的出水口连通有多个喷雾头19，输水环18的顶部与底部均固定安装有牵引绳17的一端，两个牵引绳17中的一个牵引绳17的另一端固定安装有弹簧20的顶端，弹簧20的底端固定安装在支撑板2的顶部，另一个牵引绳17的另一端转动安装在圆盘16的前侧，储水罐3的外侧转动安装有两个锥齿轮22，两个锥齿轮22相互啮合，两个锥齿轮22中的一个锥齿轮22的外侧与螺旋绞龙21的一端固定连接，另一个锥齿轮22的后侧、转盘12的后侧与圆盘16的后侧均同轴传动有链轮23，三个链轮23上传动连接有同一个链条24，储水罐3的外侧顶部与输水环18的外侧连通有同一个输水管27。
本发明中，箱体1的内部固定安装有过滤网26，箱体1的外侧开设有进风口，通过设置的过滤网26，从而能够对吸入的空气进行一定的过滤的工作，从而保证航空装置内部的空气质量。
本发明中，储水罐3的外侧固定安装有电机25，螺旋绞龙21的另一端延伸至储水罐3的外侧并与电机25的输出轴固定连接，通过设置的电机25，电机25的工作使得圆盘16与转盘12同步转动，从而使得出气头9与喷雾头19同步摆动，能够对空气进行加热加湿的工作。
本发明中，储水罐3的外侧固定安装有支撑台，电机25固定安装在支撑台的顶部，通过设置的支撑台，从而为电机25提供一定的支撑作用。
本发明中，箱体1的外侧顶部固定安装有中空杆，连接杆15的外侧活动抵接在中空杆的内侧，通过设置的中空杆，从而为连接杆15的竖直运动起到一定的导向的作用。
本发明中，支撑板2的顶部开设有通孔，输水管27的位于通孔的内部，通过设置的通孔，从而为输水管27提供一定的活动范围。
本发明中，储水罐3的顶部连通有进水阀，支撑板2的底部两侧均固定安装有支撑柱，通过设置的支撑柱，从而为整个装置提供一定的支撑作用。
本发明中，储水罐3的外侧固定安装有矩形板，锥齿轮22转动安装在矩形板的前侧，通过设置的矩形板，从而为锥齿轮22提供转动安装的位置。
该换气装置的工作原理如下：驱动吸风机4，从而使得外界的空气进入到出气管7的内部，经过加热室28的加热工作，从而由出气头9喷出，能够对航空装置的内部空气进行改善，接着驱动电机25，电机25的工作使得螺旋绞龙21转动，从而使得储水罐3内部的水能够进入到输水环18的内部，从而由多个喷雾头19喷出，从而对内部环境进行加湿工作，其次螺旋绞龙21的转动使得两个锥齿轮22通过转动，从而带动三个链轮23同步转动，从而使得转盘12与圆盘16同步转动，转盘12的转动使得第二圆轴13转动，从而使得第二水平框14得到竖直方向的运动，通过设置的连接杆15，从而使得第一水平框11得到同样的竖直往复运动，从而推动第一圆轴10摆动，从而使得摆动杆8得到往复的摆动工作，从而使得出气头9得到摆动工作，从而能够增大对内部环境的换气范围，其次圆盘16的转动使得牵引绳17运作，从而使得输水环18摆动，从而带动多个喷雾头19摆动，能够增大加湿的范围，其次出气头9输出的热风能够将喷雾头19喷出的水雾吹向更远的位置，从而能够改善航空装置的内部空气质量。

Claims (1)

  1. 一种具有加热功能的航空航天用高效换气装置，包括箱体（1），其特征在于，所述箱体（1）的底部固定安装有支撑板（2），支撑板（2）的底部固定安装有储水罐（3），储水罐（3）的内部转动安装有螺旋绞龙（21），箱体（1）的内部固定安装有吸风机（4）与进气头（6），吸风机（4）的进气口与进气头（6）连通有同一个进气管（5），箱体（1）的外侧转动安装有摆动杆（8），摆动杆（8）的前侧固定安装有第一圆轴（10），第一圆轴（10）的外侧活动套设有第一水平框（11），箱体（1）的外侧顶部转动安装有转盘（12），转盘（12）的前侧固定安装有第二圆轴（13），第二圆轴（13）的外侧活动套设有第二水平框（14），第一水平框（11）的顶部与第二水平框（14）的底部固定安装有同一个连接杆（15），摆动杆（8）的一端固定安装有出气头（9），吸风机（4）的出气口与出气头（9）的外侧均连通有出气管（7）的一端，箱体（1）的内部固定安装有加热室（28），两个出气管（7）的另一端分别连通在加热室（28）的左右两侧，箱体（1）的外侧顶部转动安装有圆盘（16），支撑板（2）的顶部转动安装有输水环（18），输水环（18）的出水口连通有多个喷雾头（19），输水环（18）的顶部与底部均固定安装有牵引绳（17）的一端，两个牵引绳（17）中的一个牵引绳（17）的另一端固定安装有弹簧（20）的顶端，弹簧（20）的底端固定安装在支撑板（2）的顶部，另一个牵引绳（17）的另一端转动安装在圆盘（16）的前侧，储水罐（3）的外侧转动安装有两个锥齿轮（22），两个锥齿轮（22）相互啮合，两个锥齿轮（22）中的一个锥齿轮（22）的外侧与螺旋绞龙（21）的一端固定连接，另一个锥齿轮（22）的后侧、转盘（12）的后侧与圆盘（16）的后侧均同轴传动有链轮（23），三个链轮（23）上传动连接有同一个链条（24），储水罐（3）的外侧顶部与输水环（18）的外侧连通有同一个输水管（27）。
    2、根据权利要求1所述的一种具有加热功能的航空航天用高效换气装置，其特征在于，所述箱体（1）的内部固定安装有过滤网（26），箱体（1）的外侧开设有进风口。
    3、根据权利要求1所述的一种具有加热功能的航空航天用高效换气装置，其特征在于，所述储水罐（3）的外侧固定安装有电机（25），螺旋绞龙（21）的另一端延伸至储水罐（3）的外侧并与电机（25）的输出轴固定连接。
    4、根据权利要求1所述的一种具有加热功能的航空航天用高效换气装置，其特征在于，所述储水罐（3）的外侧固定安装有支撑台，电机（25）固定安装在支撑台的顶部。
    5、根据权利要求1所述的一种具有加热功能的航空航天用高效换气装置，其特征在于，所述箱体（1）的外侧顶部固定安装有中空杆，连接杆（15）的外侧活动抵接在中空杆的内侧。
    6、根据权利要求1所述的一种具有加热功能的航空航天用高效换气装置，其特征在于，所述支撑板（2）的顶部开设有通孔，输水管（27）的位于通孔的内部。
    7、根据权利要求1所述的一种具有加热功能的航空航天用高效换气装置，其特征在于，所述储水罐（3）的顶部连通有进水阀，支撑板（2）的底部两侧均固定安装有支撑柱。
    8、根据权利要求1所述的一种具有加热功能的航空航天用高效换气装置，其特征在于，所述储水罐（3）的外侧固定安装有矩形板，锥齿轮（22）转动安装在矩形板的前侧。
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116808444A (zh) * 2023-06-27 2023-09-29 江苏侎医特信息科技有限公司 一种健康照明光疗装置

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN209757572U (zh) * 2019-02-12 2019-12-10 景宁畲族自治县宏晨金属制品厂 一种节能型航天航空高效换气装置
CN110844085A (zh) * 2019-11-05 2020-02-28 芜湖市极星航空科技有限公司 一种具有加热功能的航空航天用高效换气装置
CN112414782A (zh) * 2020-12-23 2021-02-26 彭莎 一种水文地质勘察水源取样检测装置
CN112643557A (zh) * 2020-12-21 2021-04-13 铜陵青铜时代雕塑有限公司 一种高效的铜雕生产加工用喷砂装置

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN209757572U (zh) * 2019-02-12 2019-12-10 景宁畲族自治县宏晨金属制品厂 一种节能型航天航空高效换气装置
CN110844085A (zh) * 2019-11-05 2020-02-28 芜湖市极星航空科技有限公司 一种具有加热功能的航空航天用高效换气装置
CN112643557A (zh) * 2020-12-21 2021-04-13 铜陵青铜时代雕塑有限公司 一种高效的铜雕生产加工用喷砂装置
CN112414782A (zh) * 2020-12-23 2021-02-26 彭莎 一种水文地质勘察水源取样检测装置

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116808444A (zh) * 2023-06-27 2023-09-29 江苏侎医特信息科技有限公司 一种健康照明光疗装置
CN116808444B (zh) * 2023-06-27 2024-01-12 江苏侎医特信息科技有限公司 一种健康照明光疗装置

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