阅读说明：本技术 空气清净机 (Air cleaner ) 是由 坪井和树 平野信介 辰己良昭 罗莉 于 2018-12-13 设计创作，主要内容包括：本发明提供一种空气清净机,可高效率地将更宽范围的空气多量地吸入至集尘器内,而且轻量且容易进行维护。空气清净机(1-1)具备飞行器(2)和集尘器(4)。飞行器(2)具有本体部(20)与安装于框架(25至28)的前端的螺旋桨(21至24)。集尘器(4)具有放电电极(41至44)和集尘电极(45)。放电电极(41至44)连接于中央室(40)内的升压部(33)。升压部(33)电性连接于本体部(20)内的控制部(30)。使集尘电极(45)与放电电极(41至44)之间的空气放电,使空气中的尘埃粒子带电而通过集尘电极(45)来捕集。(The invention provides an air cleaner which can efficiently suck a large amount of air in a wider range into a dust collector, and is light and easy to maintain. An air cleaner (1-1) is provided with an aircraft (2) and a dust collector (4). The aircraft (2) has a body portion (20) and propellers (21 to 24) mounted to the front end of frames (25 to 28). The dust collector (4) has discharge electrodes (41 to 44) and a dust collecting electrode (45). The discharge electrodes (41 to 44) are connected to a voltage boosting section (33) in the center chamber (40). The boosting part (33) is electrically connected to the control part (30) in the main body part (20). Air between the dust collecting electrode (45) and the discharge electrodes (41 to 44) is discharged, and dust particles in the air are charged and collected by the dust collecting electrode (45).)

1. An air cleaner is provided with:

an aircraft in which a plurality of propellers for sucking air from above and discharging the air downward are arranged around a main body having a control unit for controlling a flight operation, and the plurality of propellers are floated as a propulsive force; and

a dust collector having a cylindrical dust collecting electrode opened upward and downward and a discharge electrode arranged at a substantially central portion of the dust collecting electrode, wherein a high voltage is applied between the dust collecting electrode and the discharge electrode to discharge at a tip portion of the discharge electrode, thereby electrically charging and collecting dust particles in air flowing into the dust collecting electrode; wherein

Mounting the dust collector to the aircraft such that the discharge electrode is positioned substantially at the center of the upper portion of the aircraft;

the arrangement position of the dust collecting electrode of the dust collector is set so that the center position of the height direction of the dust collecting electrode is equal to or more than the position of the rotating surface of the screw propeller, and the lower end position of the dust collecting electrode is equal to or less than the position near the upper part of the rotating surface of the screw propeller, so that air can be sucked into the dust collecting electrode by the rotating force of the screw propeller.

2. An air cleaner is provided with:

an aircraft in which a plurality of propellers for sucking air from above and discharging the air downward are arranged around a main body having a control unit for controlling a flight operation, and the plurality of propellers are floated as a propulsive force; and

a dust collector having a cylindrical dust collecting electrode opened upward and downward and a discharge electrode arranged at a substantially central portion of the dust collecting electrode, wherein a high voltage is applied between the dust collecting electrode and the discharge electrode to discharge at a tip portion of the discharge electrode, thereby electrically charging and collecting dust particles in air flowing into the dust collecting electrode; wherein

At least one or more propellers among the plurality of propellers, the dust collectors being disposed respectively;

mounting each dust collector to each propeller in such a manner that each discharge electrode is positioned substantially at the center of the upper portion of each propeller of the aircraft;

the arrangement position of the dust collecting electrodes of each dust collector is set so that the height direction center position of each dust collecting electrode is equal to or more than the position of the rotating surface of each screw and the lower end position of the dust collecting electrode is equal to or less than the position near the upper side of the rotating surface of the screw, and air can be sucked into the dust collecting electrodes by the rotating force of the screw.

3. The air cleaner according to claim 1 or 2, wherein the dust collecting electrode of the dust collector has a plurality of holes for inflow of ambient air.

4. The air cleaner according to any one of claims 1 to 3, wherein an upper opening of the dust collecting electrode of the dust collector is set to have a larger diameter than a lower opening.

5. The air cleaner according to any one of claims 1 to 4, wherein the dust collector is detachably attached to the aircraft.

6. The air cleaner according to any one of claims 1 to 5, wherein a maximum diameter of the dust collecting electrode of the dust collector is set to 10cm or more, and a height of the dust collecting electrode is set to 2.5cm or more.

7. The air cleaner according to any one of claims 1 to 6, wherein the dust collector has an aluminum-plated film or a vinyl chloride sheet on an inner surface side of a dust collecting electrode.

Technical Field

The present invention relates to an air cleaner which floats in the air and can capture dust in the air.

Background

Conventionally, such air cleaners have been disclosed in, for example, patent document 1 and patent document 2.

The air cleaner described in patent document 1 includes: a dust collector for adsorbing dust in the air; a flying means for floating the dust collector in the air by a propeller; and a control device for controlling the flight means.

According to this structure, when the flying means is driven to float the air cleaner indoors, the floating air cleaner adsorbs the dust floating in the air by the fixed electronic nonwoven fabric on the surface of the dust catcher. Dust attached to the ceiling surface of furniture or a shelf placed indoors is wound in the air by a propeller and is adsorbed to the fixed electronic nonwoven fabric.

On the other hand, the air cleaner disclosed in patent document 2 includes: a flying body composed of a balloon propelled by a propeller; and a dust collector attached to the flying body. The dust collector is formed by a container having an air inlet and an air outlet which can be charged in opposite polarities to each other.

According to this configuration, when the flying object moves in the air by the propulsive force of the propeller, air flows into the dust collector through the air supply port. Accordingly, dust charged in the air is collected in the vicinity of the air supply port, the inside, the exhaust port, and the like of the dust collector.

[ Prior art documents ]

[ patent document ]

Patent document 1: japanese laid-open patent publication No. H08-131883

Patent document 2: japanese patent laid-open No. 2014-515086.

Disclosure of Invention

(problems to be solved by the invention)

However, the above known air cleaner has the following problems.

The air cleaners disclosed in patent documents 1 and 2 are configured to move a flying body by thrust of a propeller and to collect dust by bringing the dust into contact with a dust collector. Therefore, the dust collection rate per unit time depends on the speed and route of the flying object. Therefore, when the speed of the flying object is low and the range of the flying object circling is small, the dust collection rate is low. That is, these air cleaners have a low dust collecting capacity.

In particular, in the case of a configuration in which the air inlet and the air outlet of the dust collector have different charges, as in the air cleaner disclosed in patent document 2, when a high voltage is applied to charge the dust, it is necessary to provide a structure in which the air inlet and the air outlet are separated from each other by a distance between electrodes of the air inlet and the air outlet for insulation.

When the dust collector having such a structure is attached to a position that affects the airflow of the propulsion mechanism of the flying object, the propulsive force of the flying object is greatly affected. In addition, since the dust collector is enlarged, the center of gravity of the air cleaner as a whole moves according to the installation position of the dust collector. Therefore, control of the flight vehicle becomes very difficult.

The present invention has been made to solve the above problems, and an object of the present invention is to provide an air cleaner which can efficiently suck a large amount of air in a wider range into a dust collector, and which is lightweight and easy to maintain.

(means for solving the problems)

In order to solve the above problem, a first aspect of the present invention provides an air cleaner, including: an aircraft in which a plurality of propellers for sucking air from above and discharging the air downward are arranged around a main body having a control unit for controlling a flight operation, and the plurality of propellers are floated as a propulsive force; and a dust collector having a cylindrical dust collecting electrode opened upward and downward and a discharge electrode disposed at a substantially central portion of the dust collecting electrode, wherein a high voltage is applied between the dust collecting electrode and the discharge electrode to discharge at a tip portion of the discharge electrode, thereby charging and collecting dust particles in air flowing into the dust collecting electrode; wherein the air cleaning mechanism comprises: mounting a dust collector to the aircraft in such a manner that the discharge electrode is located substantially centrally in the upper part of the aircraft; the position of the dust collecting electrode of the dust collector is set so that the center position of the dust collecting electrode in the height direction is equal to or more than the position of the rotating surface of the screw and the lower end position of the dust collecting electrode is equal to or less than the position near the upper side of the rotating surface of the screw, and air can be sucked into the dust collecting electrode by the rotating force of the screw.

With this configuration, the plurality of propellers can be controlled by the control unit to float the aircraft. When the dust collector is operated in a floating state of the aircraft and a high voltage is applied between the dust collecting electrode and the discharge electrode, electric discharge occurs at the tip of the discharge electrode, and air ions are generated in the vicinity of the discharge electrode. In this way, air ions having the same polarity as the polarity of the discharge electrode are attracted to the dust collecting electrode, and while the air ions reach the dust collecting electrode, the dust particles in the air flowing into the dust collecting electrode are charged to have the same polarity. Accordingly, the charged dust particles are attracted to the dust collecting electrode and collected by the dust collecting electrode.

In other words, according to the air cleaner of the present invention, the air ions move in the wide space between the discharge electrode and the dust collecting electrode, and the large amount of dust particles flowing into the wide space are charged, whereby the charged large amount of dust particles can be collected.

In addition, the speed of air sucked in from above by the propeller of the aircraft is much slower than the speed of air discharged downwards. Therefore, the air sucked from above by the propeller is ionized, and a larger amount of dust particles can be collected than the air exhausted from below.

In view of this, in the air cleaner of the present invention, the dust collector is attached to the main body of the aircraft such that the discharge electrode is positioned substantially at the center of the upper portion of the aircraft, and the center position of the dust collecting electrode in the height direction is set to be equal to or higher than the position of the rotation surface of the propeller. Accordingly, the air on the air suction side can be mainly ionized among the air flowing into the dust collecting electrode of the dust collector.

However, if the height of the dust collector is too high than the propeller, sufficient air cannot be sucked into the dust collecting electrode.

Therefore, in the air cleaner of the present invention, the lower end position of the dust collecting electrode is set to be equal to or lower than the position near the upper side of the rotating surface of the propeller, so that a desired amount of air can be sucked into the dust collecting electrode.

A second aspect of the present invention provides an air cleaner, including: an aircraft in which a plurality of propellers for sucking air from above and discharging the air downward are arranged around a main body having a control unit for controlling a flight operation, and the plurality of propellers are floated as a propulsive force; and a dust collector for collecting dust particles in the air flowing into the dust collecting electrode from the upper opening by discharging at the tip of the discharge electrode when a high voltage is applied between the cylindrical dust collecting electrode opened upward and downward and the discharge electrode arranged at the substantially central portion of the dust collecting electrode; wherein the air cleaning mechanism comprises: at least more than one screw propeller in the plurality of screw propellers are respectively provided with a dust collector; mounting each dust collector to each propeller in such a manner that each discharge electrode is located substantially centrally above each propeller of the aircraft; the arrangement position of the dust collecting electrodes of each dust collector is set so that the height direction center position of each dust collecting electrode is equal to or more than the position of the rotating surface of each screw and the lower end position of the dust collecting electrode is equal to or less than the position near the upper side of the rotating surface of the screw, and air can be sucked into the dust collecting electrodes by the rotating force of the screw.

With this configuration, when the dust collectors are operated in a floating state of the aircraft and a high voltage is applied between the dust collecting electrodes and the discharge electrodes in each dust collector, dust particles in the air flowing into each dust collecting electrode are charged and collected by the dust collecting electrodes.

Further, since the arrangement position of the dust collecting electrodes of the respective dust collectors is set so that the center position in the height direction of the respective dust collecting electrodes becomes equal to or more than the position of the rotation surface of the respective propellers and the lower end position of the dust collecting electrodes becomes equal to or less than the position in the vicinity above the rotation surface of the propellers, it is possible to mainly ionize the air on the suction side among the air flowing into the dust collecting electrodes of the respective dust collectors and to suck a desired amount of air into the respective dust collecting electrodes.

A third aspect of the invention is the air cleaner according to the first or second aspect, wherein the dust collecting electrode formed as the dust collector has a plurality of holes into which ambient air flows.

With this configuration, air can flow into the dust collecting electrode from the upper opening and also from the plurality of holes, so that the air can flow smoothly without being obstructed by the dust collecting electrode. As a result, the aircraft can perform stable flight.

A fourth aspect of the invention is the air cleaner according to any one of the first to third aspects, wherein: the upper opening of the dust collecting electrode of the dust collector is set to have a larger diameter than the lower opening.

With this configuration, a large amount of air can smoothly flow into the dust collecting electrode from the large-diameter upper opening, and the aircraft can stably fly.

A fifth aspect of the invention is the air cleaner according to any one of the first to fourth aspects, wherein the dust collector is detachably attached to the aircraft.

With this configuration, the dust collector can be easily attached to and detached from the aircraft, and as a result, repair and maintenance of the dust collector can be easily performed.

A sixth aspect of the invention is the air cleaner according to any one of the first to fifth aspects, wherein a maximum diameter of the dust collecting electrode of the dust collector is set to 10cm or more, and a height of the dust collecting electrode is set to 2.5cm or more.

A seventh aspect of the invention provides the air cleaner as recited in any one of the first to sixth aspects, wherein the dust collector has a structure having any one of an aluminum-plated film and a vinyl chloride sheet on an inner surface side of a dust collecting electrode of the dust collector.

(effect of the invention)

As described above in detail, according to the air cleaner of the present invention, since the air ions can be moved in the wide space between the discharge electrode and the dust collecting electrode, and a large amount of dust particles flowing into the wide space can be collected, the air cleaner has an excellent effect of having a very high dust collecting capability.

Further, the height position of the dust collector is set to a position where the air flowing into the dust collecting electrode can be ionized mainly on the air suction side and a desired amount of air can be surely flowed into the dust collecting electrode, so that the dust collecting capability can be further improved.

In addition, the dust collector is composed of one dust collecting electrode and one discharge electrode, so that the dust collector is light and smooth in air flow, and the dust collector can be maintained by brushing the surface of one dust collecting electrode without disassembling the dust collecting electrode.

In particular, according to the third aspect of the invention, the air can smoothly flow without being blocked by the dust collecting electrode, and the weight of the dust collector can be reduced.

In addition, according to the invention of the fourth aspect, a large amount of air can smoothly flow into the dust collecting electrode.

In addition, according to the fifth aspect of the invention, the dust collector can be easily repaired and maintained.

Drawings

Fig. 1 is an exploded perspective view showing an air cleaner according to a first embodiment of the present invention.

FIG. 2 is a schematic sectional view of an air cleaner.

Fig. 3 is a plan view of the aircraft.

Fig. 4 is a side view of the dust collector.

Fig. 5 is a plan view showing the upper face side of the dust collector.

Fig. 6 is a plan view showing the lower face side of the dust collector.

Fig. 7 is a schematic sectional view for explaining a method of loading and unloading the dust collector to and from the aircraft.

Fig. 8 is a schematic view for explaining a control system of an aircraft and a dust collector.

Fig. 9 is a schematic sectional view showing a state where the dust collector is mounted at the lowermost position.

Fig. 10 is a schematic sectional view showing a state where the dust collector is mounted at the uppermost position.

Fig. 11 is a schematic cross-sectional view showing an electric field concentration state.

Fig. 12 is a schematic partial cross-sectional view showing a state where air ions are generated.

Fig. 13 is a schematic partial sectional view showing the flow of air ions.

Fig. 14 is a schematic cross-sectional view showing an inflow state of air containing dust.

Fig. 15 is a schematic cross-sectional view showing a moving state of charged dust.

Fig. 16 is a schematic view showing an apparatus of the first experiment.

Fig. 17 is a graph showing set values of the sizes of ten kinds of dust collecting electrodes.

Fig. 18 is a graph showing the results of the first experiment.

Fig. 19 is a schematic view showing an apparatus for the second experiment.

Fig. 20 is a graph showing the results of the second experiment.

Fig. 21 is a schematic sectional view showing a modification of the first embodiment.

Fig. 22 is a side view of a dust collector of a main part of the second embodiment of the present invention.

Fig. 23 is a schematic partial sectional view showing the flow of air.

FIG. 24 is a schematic view showing two types of air cleaners used in the experiment.

Fig. 25 is a graph showing the results of the experiment.

Fig. 26 is a side view showing a modification of the second embodiment.

Fig. 27 is a schematic cross-sectional view showing an air cleaner according to a third embodiment of the present invention.

Fig. 28 is a schematic cross-sectional view showing an air cleaner according to a fourth embodiment of the present invention.

Fig. 29 is a perspective view showing an air cleaner according to a fifth embodiment of the present invention.

Fig. 30 is a schematic sectional view showing a state where the dust collector is mounted at the lowermost position.

Fig. 31 is a schematic sectional view showing a state where the dust collector is mounted at the uppermost position.

Fig. 32 is a schematic cross-sectional view showing an air cleaner according to a sixth embodiment of the present invention.

Fig. 33 is a schematic sectional view showing a modification of the sixth embodiment.

Detailed Description

Hereinafter, preferred embodiments of the present invention will be described with reference to the drawings.

(example 1)

Fig. 1 is an exploded perspective view showing an air cleaner according to a first embodiment of the present invention, and fig. 2 is a schematic cross-sectional view of the air cleaner.

As shown in fig. 1 and 2, the air cleaner 1-1 of this embodiment is configured such that one dust collector 4 is mounted on the aircraft 2.

The aircraft 2 is a rotary wing type aircraft that can float vertically and horizontally with a propeller as a propulsive force. As the rotary-wing type aircraft, there are aircraft provided with various types of rotors, such as a triple rotor having three propellers, a quad rotor having four propellers, a five rotor having five propellers, a six rotor having six propellers, and an eight rotor having eight propellers. In this embodiment, a four-rotor aircraft is used as the aircraft 2.

Fig. 3 is a plan view of the aircraft 2.

As shown in fig. 3, this aircraft 2 has: a body portion 20; and four propellers 21 to 24 arranged around the body portion 20.

The propellers 21 to 24 are attached to the front end portions of four frames 25 to 28 extending crosswise from the main body 20. Specifically, the motors 21a (22a to 24a) are mounted on the upper front ends of the respective frames 25(26 to 28), and the respective propellers 21(22 to 24) are fixed to the rotary shafts 21b (22b to 24b) of the respective motors 21a (22a to 24 a).

Accordingly, the propellers 21(22 to 24) rotate integrally with the rotary shafts 21b (22b to 24b) by driving the motors 21a (22a to 24a), and suck air from above and discharge air downward. In other words, the propellers 21(22 to 24) provide upward propulsion to the aircraft 2.

In fig. 1 and 2, the dust collector 4 is a device for collecting dust in the air by electric discharge, and includes four discharge electrodes 41 to 44 and a dust collecting electrode 45.

Fig. 4 is a side view of the dust container 4, fig. 5 is a plan view showing the upper surface side of the dust container 4, and fig. 6 is a plan view showing the lower surface side of the dust container 4.

The discharge electrodes 41 to 44 are conductive carbon brushes, and are attached to a peripheral surface 40a of the center chamber 40 provided on the upper surface of the dust collecting electrode 45, as shown in fig. 4.

Specifically, as shown in fig. 5, the discharge electrodes 41 to 44 are mounted on the peripheral surface 40a of the center chamber 40 with their distal end portions exposed at 90 ° intervals, and the rear end portions of the discharge electrodes 41 to 44 are connected to the pressure increasing portion 33 inside the center chamber 40. The center chamber 40 is mounted on a center chamber mounting portion 47a of the dust collecting electrode 45, which will be described later.

The dust collecting electrode 45 is an electrode for electrostatically attracting and collecting charged dust, and is composed of a rectangular tubular dust collecting electrode body 46 having an upward and downward opening, and a plurality of ribs 47 supporting the dust collecting electrode body 46 and the center chamber 40.

Specifically, as shown in fig. 6, the plurality of ribs 47 extend from the upper edge of the collecting electrode body 46 toward the center of the collecting electrode body 46, and are connected to an annular center chamber mounting portion 47a provided at the center. The plurality of ribs 47, the center chamber mounting portion 47a, and the dust collecting electrode body 46 are integrally formed by a conductive member.

Fig. 7 is a schematic cross-sectional view for explaining a method of loading and unloading the dust collector 4 to and from the aircraft 2.

As shown in fig. 2, the air cleaner 1-1 includes a mounting/demounting mechanism 5 that can mount and demount the dust collector 4 to and from the aircraft 2. The attachment/detachment mechanism 5 is constituted by four support posts 51 to 54 provided on the aircraft 2 and four mount portions 56 to 59 provided on the dust collector 4.

As shown in fig. 1 and 3, the struts 51 to 54 are erected around the main body 20 of the aircraft 2 at equal angular intervals, and a magnet piece 51a (52a to 54a) is attached to an upper end of each strut 51(52 to 54).

On the other hand, as shown in fig. 2 and 6, the mounting portions 56 to 59 are provided on the lower surface of the central chamber mounting portion 47a of the dust collector 4. The mounting portions 56 to 59 hang down at equal angular intervals at positions corresponding to the support posts 51 to 54, and the magnet pieces 56a (57a to 59a) are attached to the lower ends of the respective mounting portions 56(57 to 59).

Accordingly, as shown in fig. 7, the dust collector 4 is positioned above the aircraft 2, and after the central chamber 40 of the dust collector 4 is aligned with the main body portion 20 positioned at the substantially center of the aircraft 2, the dust collector 4 is lowered to the aircraft 2 side, whereby the magnet pieces 56a to 59a of the placement portions 56 to 59 of the dust collector 4 can be loaded on the magnet pieces 51a to 54a of the support posts 51 to 54 of the aircraft 2. As a result, the dust collector 4 is fixed to the aircraft 2 by the magnetic force of the magnet pieces 56a to 59a and the magnet pieces 51a to 54 a.

In addition, the dust container 4 is lifted against the magnetic force of the magnet pieces 56a to 59a and the magnet pieces 51a to 54a, whereby the dust container 4 can be easily detached from the aircraft 2.

In other words, according to the air cleaner 1-1 of this embodiment, since the dust collector 4 can be easily detached from the aircraft 2, repair or maintenance of the dust collector 4 can be easily performed.

In addition, as described above, since the dust container 4 is mounted above the propellers 21 to 24, the dust container 4 constituted by the dust collecting electrode body 46 and the ribs 47 functions as a propeller guard for the propellers 21 to 24.

The control of the aircraft 2 and the dust collector 4 is performed by the body part 20 of the aircraft 2.

Fig. 8 is a schematic view for explaining a control system of the aircraft 2 and the dust collector 4.

As shown in fig. 8, the control section 30 having the memory 30a, the power supply section 31, the receiving section 34, and the antenna 35 are housed in the main body section 20 of the aircraft 2, and the pressure-increasing section 33 is housed in the central chamber 40 of the dust collector 4.

The power supply unit 31, the receiving unit 34, and the antenna 35 are connected to the control unit 30, and the number of rotations of the motors 21a (22a to 24a) of the propellers 21(22 to 24) is controlled by the control unit 30. Here, the power supply unit 31 is, for example, a lithium battery having a direct current voltage of 11.1 volts (V).

The wirings 30b and 30c are wirings for transmitting a power supply voltage and a control signal to the booster 33, and these wirings 30b and 30c are led from the controller 30 into the support columns 51 and 53 and connected to the magnet pieces 51a and 53a, respectively.

On the other hand, wires 33b and 33c are provided on the dust collector 4 side. These wires 33b and 33c are wires for receiving a power supply voltage and a control signal from the control unit 30, and are connected between the input end of the voltage boosting unit 33 and the magnet pieces 56a and 58a of the mounting units 56 and 58.

The output end of the voltage boosting unit 33 is connected to wires 33d and 33e, and the wires 33d and 33e are connected to the discharge electrodes 41 to 44 and the central chamber mounting portion 47a of the dust collecting electrode 45, respectively. The booster 33 is a high-voltage booster circuit that boosts a dc voltage of 5V to 6kV, for example. In this embodiment, the insulation type DC/DC converter 36 is provided between the wirings 33b and 33c of the boosting unit 33 and the boosting unit 33. This insulation type DC/DC converter 36 has the following functions: the dc voltage 11.1V from the power supply unit 31 sent through the wires 33b and 33c is converted into a dc voltage 5V, and the stabilized dc voltage 5V is input to the voltage step-up unit 33.

In other words, as shown in fig. 7, when the dust collector 4 is mounted on the aircraft 2, the control unit 30 of the main body 20 and the voltage boosting unit 33 of the center chamber 40 are electrically connected by the wires 30b and 30c, the magnet pieces 51a and 53a, the magnet pieces 56a and 58a, the wires 33b and 33c, and the insulation type DC/DC converter 36. As a result, the direct-current voltage 11.1V of the power supply unit 31 is input from the control unit 30 to the insulation type DC/DC converter 36, and is converted into a stable direct-current voltage of 5V. Then, the DC voltage of 5V is inputted to the voltage boosting section 33, boosted to a high voltage of 6kV, and applied between the discharge electrodes 41 to 44 and the dust collecting electrode body 46.

In this embodiment, the discharge electrodes 41 to 44 are set to negative electrodes, and the dust collecting electrode 45 is set to positive electrodes. In addition, the dust collector 4 is substantially completely insulated from the aircraft 2. Specifically, the dust collector 4 is mounted on the aircraft 2 in such a manner that the ribs 47 and the dust collecting electrode body 46 do not contact the frames 25 to 28 of the aircraft 2. The aircraft 2 and the dust collector 4 are in contact only by the struts 51 to 54 and the mount portions 56 to 59. The support posts 51 to 54 and the placement portions 56 to 59 are formed of an insulating material except for the portions of the magnet pieces 51a to 54a and 56a to 59a and the portions of the wires 33b and 33 c. The central chamber 40 of the dust collector 4 is also made of an insulating material.

In addition, the control flight of the aircraft 2 can be roughly classified into an automatic control flight and an operation control flight. The flight form of the automatic control flight is as follows: for example, 3D (three-dimensional) map data of a clean object space created in advance is stored in the control unit 30, and the control unit 30 causes the aircraft 2 to fly to a desired position in the space based on the 3D map data and the control program. On the other hand, the flight pattern of the operation control flight is as follows: the aircraft 2 is manually operated from a short distance or a long distance using a dedicated operation machine, a portable operation machine, a smart phone, a Global Positioning System (GPS), or the like. Both control flights enable the aircraft 2 to fly in full space, or they may be restricted to a given location or a given altitude.

These systems for automatically controlling and operating the control flight are known systems, whichever control system is applicable to the aircraft 2.

In this embodiment, both automatic flight control and operational flight control systems are used. That is, the control section 30 can control the propellers 21 to 24 according to the control program, the 3D drawing, and the like stored in the memory 30 a. The control unit 30 receives a command radio wave from the outside or a radio wave from the GPS via the antenna 35 at the receiving unit 34, and controls the propellers 21 to 24, the booster unit 33, and the like in accordance with the received radio wave.

Fig. 9 is a schematic sectional view showing a state where the dust collector 4 is mounted at the lowermost position, and fig. 10 is a schematic sectional view showing a state where the dust collector 4 is mounted at the uppermost position.

As shown in fig. 7, when the mount portions 56 to 59 of the dust collector 4 are mounted on the supports 51 to 54 of the aircraft 2, the dust collector can be mounted on the body portion of the aircraft such that the central chamber 40 having the discharge electrodes 41 to 44 is located directly above the body portion 20, the body portion 20 being located substantially centrally in the upper portion of the aircraft 2. At this time, as shown in fig. 9 and 10, the height position of the dust collector 4 with respect to the aircraft 2 depends on the length of the mount portions 56 to 59 of the dust collector 4.

When the propellers 21 to 24 of the aircraft 2 shown in fig. 9 are rotated, the propellers 21 to 24 suck air from above the rotating surface S of the propellers 21 to 24 and discharge the air to below the rotating surface S. At this time, the flow velocity of the air flowing from above to the rotating surface S side is much slower than the flow velocity of the air flowing from below. Accordingly, when the air above the rotating surface S of the propellers 21 to 24 is discharged and ionized, a larger amount of dust particles can be charged than when the air below the rotating surface S is discharged and ionized.

In view of this point, in this embodiment, as shown in fig. 9, it is set that: when the center position M in the height direction of the dust collecting electrode 45 coincides with the rotation surface S of the propellers 21 to 24, the dust collector 4 is positioned at the lowermost position.

However, if the height of the dust collector 4 is excessively higher than the propellers 21 to 24, sufficient air cannot be sucked into the dust collecting electrode 45. It is necessary to set the dust container 4 at a height position where a necessary minimum amount of air can be sucked by the rotational force of the propellers 21 to 24.

In view of this point, in this embodiment, as shown in fig. 10, when the lower end position U of the dust collecting electrode 45 is located in the vicinity of the upper side of the rotation surface S of the propellers 21 to 24, the dust collector 4 is set to the uppermost position.

That is, in this embodiment, the dust collector 4 is mounted on the aircraft 2 such that the center position M of the dust collecting electrode 45 is above the rotation surface S of the propellers 21 to 24 and the lower end position U of the dust collecting electrode 45 is below a position near above the rotation surface S of the propellers 21 to 24.

Next, the operation and effect of the air cleaner 1-1 of this embodiment will be described.

Fig. 11 is a schematic sectional view showing a state in which an electric field is concentrated, fig. 12 is a schematic partial sectional view showing a state in which air ions are generated, and fig. 13 is a schematic partial sectional view showing a flow of the air ions.

As shown in fig. 2, when the propellers 21 to 24 are rotated at a desired rotation speed by the control of the control unit 30 (see fig. 8) in a state where the dust collector 4 is mounted on the upper portion of the aircraft 2, an upward thrust is generated, and the air cleaner 1-1 floats.

Then, when a predetermined dc voltage is inputted from the power supply unit 31 to the voltage boosting unit 33 by the control of the control unit 30 shown in fig. 8 in the floating state of the air cleaner 1-1, the dc voltage is boosted to a high voltage in the voltage boosting unit 33, and the high voltage is applied between the discharge electrodes 41 to 44 and the dust collecting electrode main body 46.

Accordingly, as shown in fig. 11, an electric field E is generated between the discharge electrodes 41 to 44 of the negative electrode and the dust collecting electrode body 46 of the positive electrode, and the electric field E is concentrated on the front end portions of the discharge electrodes 41 to 44 as indicated by the surrounding dotted line C.

As a result, discharge such as corona discharge occurs, and as shown in fig. 12, a large number of positive air ions a are generated near the tips of the discharge electrodes 41 to 44⁺With negative air ions A^-. Then, as shown in FIG. 13, positive air ions A⁺Will be captured by the discharge electrodes 41 to 44 of the negative electrode, and the negative air ions A^-Will move toward the positive collecting electrode body 46.

Fig. 14 is a schematic cross-sectional view showing an inflow state of air a containing dust P, and fig. 15 is a schematic cross-sectional view showing a moving state of charged dust P.

As shown in fig. 14, in the negative air ion a^-In a state where the dust collecting electrode body 46 facing the positive electrode is moved, the air a containing the dust P flows into the dust collecting electrode body 46 from the upper opening 45A.

Thus, air ion A^-The dust P collides with the negative electrode, and a negatively charged dust P is generated in the negative electrode as shown in FIG. 15^-. Accordingly, the charged dust P^-Moves to the positive electrode side of the collecting electrode body 46 and is captured by the collecting electrode body 46.

As described above, according to the air cleaner 1-1 of this embodiment, as shown in FIG. 14, the air ions A are made to be air ions A^-And moves in the wide space D between the discharge electrodes 41 to 44 and the dust collecting electrode body 46, and a large amount of air A can flow into the wide space D, so that a large amount of dust P can be collected at one time.

Further, as shown in FIG. 1, since the dust collector 4 of the air cleaner 1-1 is composed of one dust collecting electrode 45 and the discharge electrodes 41 to 44, the weight of the dust collector 4 can be reduced and the air can smoothly flow into the dust collecting electrode body 46. Further, with this configuration, the dust collector 4 can be maintained by brushing the surface of one dust collecting electrode 45 without disassembling the dust collector 4.

The inventors performed two experiments.

The first experiment is an experiment for confirming the relationship between the size of the dust collecting electrode of the dust collector and the dust collecting rate.

Fig. 16 is a schematic view showing the apparatus in the first experiment, and fig. 17 is a graph showing set values of sizes of ten kinds of dust collecting electrodes.

As shown in FIG. 16, in this experiment, the dust collector 100-1(100-2 to 100-10) was disposed in a volume of 2.744m with its upper side facing upward³The concentration of the particles of the string incense in the chamber 110 is measured, and the dust collection rate of each dust collector 100-1(100-2 to 100-10) is determined based on the measured concentration.

Specifically, the following configuration is adopted: each dust collector 100-1(100-2 to 100-10) is formed by a dust collecting electrode 101 and a carbon brush-shaped discharge electrode 10 disposed at the center of the dust collecting electrode 101, and a DC voltage of 6kV is applied between the dust collecting electrode 101 and the discharge electrode 102 from a booster circuit 103 to operate each dust collector 100-1(100-2 to 100-10).

Further, when the chamber 110 is filled with not-shown joss stick smoke and the joss stick smoke is stabilized, a propeller of an aircraft (not shown) disposed below the dust collector 100-1(100-2 to 100-10) is rotated at a predetermined rotational speed, so that air having a wind speed of 1.5m/s flows into the dust collector 100-1(100-2 to 100-10) from above.

In this experiment, as shown in FIG. 17, ten sizes of dust collectors 100-1(100-2 to 100-10) were used. That is, the combinations (L, R) of the height L (cm) and the diameter R (cm) of the dust collecting electrodes 101 are ten kinds of dust collectors 100-1 to 100-10 of (1.25, 10), (2.5, 10), (5, 10), (2.5, 20), (5, 20), (10, 20), (2.5, 5), (5, 5), (10, 10), (1.25, 5), respectively.

In the experiment, each dust collector 100-1(100-2 to 100-10) was disposed in the chamber 110 and operated, and the particle concentration of the incense stick at that time was measured between 10 minutes. Further, the experiment was performed twice for each dust collector 100-1(100-2 to 100-10) with varying time intervals, and the dust collection rate of each dust collector 100-1(100-2 to 100-10) was determined from the average particle concentration value of the two times. Further, the dust collectors 100-3 and 100-5 were performed four times with different times.

Fig. 18 is a graph showing the results of the first experiment.

FIG. 18 shows the attenuation ratio λ (1/min), the natural attenuation λ (min) with respect to each dust collector 100-1(100-2 to 100-10)₀(1/min) clean air Release Rate (m)³Min: clean Air Delivery Rate; CADR), and dust collection rate. Herein, the CADR is a value obtained by multiplying a difference between the attenuation rate and the natural attenuation by the volume of the chamber 100, that is, (λ - λ ^ λ)₀) × V, the dust collection ratio is a value obtained by dividing CADR by the amount of air Q passing through the dust collection electrode 101, i.e., CADR/Q.

As shown in FIG. 18, it was confirmed from the experiment that when the electrode height L and the diameter R are both large, the attenuation ratio and CADR are large, and the dust collection ratio is high when the diameter R is small.

The second experiment was an experiment for confirming the relationship between the size of the dust collecting electrode of the dust collector and the number of diffused ions.

Fig. 19 is a schematic view showing an apparatus for the second experiment.

In this experiment, as shown in fig. 19, the dust collector 100-1(100-2 to 100-10) was disposed laterally in the chamber 110, and the circulator 200 was disposed at the right side of 10cm from the dust collector. At this time, two honeycomb meshes 201 and 202 having different mesh sizes are arranged in a state of being overlapped on the front surface of the circulator 200 so that the distribution of the wind speed by the circulator 200 becomes uniform. Then, the ion number measuring instrument 210 was disposed at the left side of 50cm from the dust collector 100-1(100-2 to 100-10).

When the dust collector 100-1(100-2 to 100-10) is operated, negative ions (air ions A in FIG. 2)^-) Generated at the tip of the discharge electrode 102, these negative ions are directed toward the dust collecting electrode 101. However, when the wind from the circulator 200 flows into the dust collecting electrode 101 of the dust collector 100-1(100-2 to 100-10), the negative ions are diffused out of the dust collecting electrode 101.

The number of ions is measured by measuring the diffused negative ions by the ion number measuring instrument 210, and the concentration of the negative ions is determined.

Specifically, the air speed is changed while the humidity in the chamber 110 is confirmed, and the air is sent from the circulator 200 to the dust collectors 100-1(100-2 to 100-10) in the operating state.

The wind speed of the circulator 200 is set to four kinds a to D. When A is set, the average wind speed v1 flowing from the center of the front surface of the circulator 200 to the region within a radius of 5cm is 1.5m/s, the average wind speed v2 flowing from the center to the region within a radius of 10cm is 1.55m/s, and the average wind speed v3 flowing from the center to the region within a radius of 20cm is 1.38 m/s. When B, C, D was set, the average wind speeds (v1, v2, v3) were (0.90m/s, 0.79m/s), (0.65m/s, 0.63m/s, 0.60m/s), (0.50m/s, 0.49m/s, 0.47m/s), respectively.

In the experiment, the air speed of the circulator 200 was changed from the setting a to the setting D, and the air was blown to each dust collector 100-1(100-2 to 100-10), and the concentration of negative ions was determined based on the number of negative ions measured by the ion number measuring instrument 210 at each air speed setting. At this time, the experiments on the dust collectors 100-1, 100-3, 100-4, 100-6 to 100-10 were performed twice, and the experiments on the dust collectors 100-2, 100-5 were performed three times.

Fig. 20 is a graph showing the results of the second experiment.

As shown in fig. 20, it was confirmed that the number of diffused ions was large in the case of the dust collector having the large diameter R of the dust collecting electrode 10, and the number of diffused ions was large in the case of the dust collector having the small height L of the dust collecting electrode 101. In addition, the dust collector in which the ratio of the diameter R to the height L of the dust collecting electrode 101 was the same was similar in characteristics, and in the case where the diameter R was 5cm, it was confirmed that the ions were not diffused.

It is considered that the negative ions are not diffused to the outside of the dust collector and remain in the dust collector, and the charged dust particles are not escaped and can be collected, and the dust collector has a high dust collection rate. Further, when the first and second experimental results were compared, it was found that "a sample having a high dust collection rate" and "a sample not diffusing negative ions" corresponded to each other, and it was confirmed that this was confirmed. Thus, the dust collector having a large electrode height L and a small diameter R has a high dust collection efficiency. However, the dust collecting capacity CADR which eventually becomes a problem is proportional to the processable air volume Q. The air volume Q is roughly proportional to the cross-sectional area of the dust collector through which the air passes, and is estimated to be proportional to the square of the diameter R. From the first experimental results, it was confirmed that the dust collecting capacity CADR of the dust collector having the large electrode height L and the large diameter R was large.

(modification 1)

Fig. 21 is a schematic sectional view showing a modification of the first embodiment.

Although the discharge electrodes 41 to 44 are attached to the circumferential surface 40a of the center chamber 40 in the first embodiment, the discharge electrodes 41 to 44 may be attached to the lower surface 40b of the center chamber 40 so as to protrude toward the lower side of the center chamber 40, as shown in fig. 21.

(example 2)

Next, a second embodiment of the present invention will be described.

Fig. 22 is a side view of a dust collector of a main part of the second embodiment of the present invention, and fig. 23 is a schematic partial sectional view showing a flow of air a.

As shown in fig. 22, the air cleaner 1-2 of this embodiment is different from the first embodiment in that the dust collecting electrode body 46 of the dust collector 4 has a plurality of holes 46 a.

That is, a plurality of circular or oval holes 46a penetrating the collecting electrode body 46 are bored in the collecting electrode body 46, and thus, as shown in fig. 23, when the screw 21(22 to 24) is rotated, the air a flows not only from the upper opening 45A of the collecting electrode body 46 but also from the plurality of holes 46a into the collecting electrode body 46.

Therefore, according to the air cleaner 1-2 of this embodiment, the hollowing out by the plurality of holes 46a makes it possible to reduce the weight of the air cleaner and to smooth the flow of the air a, thereby stabilizing the flight of the aircraft 2.

That is, when the periphery of the screw 21(22 to 24) is surrounded by the dust collecting electrode body 46, the air a is not sucked to the screw 21(22 to 24) side, so that the air pressure on the suction side of the screw 21(22 to 24) is lowered. In this way, since an excessive load is applied to the propellers 21(22 to 24) and noise is generated from the propellers 21(22 to 24), a large amount of electric power is required for driving the propellers 21(22 to 24), and the aircraft 2 cannot fly even in some cases.

In contrast, in the embodiment, by providing the plurality of holes 46a in the dust collecting electrode body 46 of the dust collecting electrode 45, the air a can flow into the dust collecting electrode body 46 from the plurality of holes 46a as well as from the upper opening 45A. As a result, the air a can smoothly flow into the propeller 21(22 to 24) side without being obstructed by the dust collecting electrode body 46, and the aircraft 2 can stably fly.

In addition, when the plurality of holes 46a are provided in the dust collecting electrode body 46 of the dust collector 4, the electrode area of the dust collecting electrode body 46 is reduced, and there is a possibility that the dust collecting ability of the dust collector 4 is affected.

In contrast, the inventors performed a comparative experiment of the dust collecting capability of the dust collector 4 provided with the holes 46a and the dust collector 4 not provided with the holes 46 a.

FIG. 24 is a schematic view showing two types of air cleaners used in the experiment.

The air cleaner 10-1 shown in FIG. 24 has substantially the same structure as the air cleaner 1-1 of the first embodiment, and the dust collecting electrode body 46 does not have the hole 46 a. On the other hand, the air cleaner 10-3 shown in FIG. 24 has substantially the same structure as the air cleaner 1-2 of the second embodiment, and has a hole 46a in the dust collecting electrode body 46. The air cleaners 10-1 and 10-3 are the same in size.

The experiment was performed in the same manner as the experiment of the dust collection rate shown in FIG. 16, in which each air cleaner 10-1(10-3) was disposed in the chamber 110, and the attenuation rate and CADR of each air cleaner 10-1(10-3) were determined by measuring the particle concentration of the linear fragrance in the chamber 110.

That is, the chamber 110 is filled with a stick of incense not shown, and the air cleaner 10-1(10-3) is operated at a time point when the stick of incense has stabilized, and the particle concentration of the stick of incense is measured for 10 minutes. Further, the experiment was performed twice in each air cleaner 10-1(10-3), and the attenuation rate and CADR of each air cleaner 10-1(10-3) were determined from the average particle concentration values of the two times.

Fig. 25 is a graph showing the results of the experiment.

FIG. 25 shows the attenuation ratios λ (1/min) and CADR (m) of the respective air cleaners 10-1(10-3)³Min), and dust collection rate.

As shown in FIG. 25, the attenuation ratios and CADRs of the two air cleaners 10-1 and 10-3 were substantially the same. The difference between the air cleaners 10-1 and 10-3 is within the range of experimental error, and it can be judged that almost no difference occurs.

In other words, it was confirmed through this experiment that there is no difference in the dust collecting capacity of the air cleaner having the plurality of holes 46a from the dust collecting capacity of the air cleaner not having the holes 46a, and there is little concern about the influence on the dust collecting capacity of the dust collector 4 even if the electrode area of the dust collecting electrode body 46 is reduced by the holes 46 a.

Since other configurations, operations, and functions are the same as those of the first embodiment, the description thereof is omitted.

(modification 2)

Fig. 26 is a side view showing a modification of the second embodiment.

In the second embodiment, the example in which the dust collecting electrode body 46 is provided with the circular or elliptical hole 46a is shown.

However, the hole is not limited to a circular or elliptical shape. As shown in fig. 26, the longitudinal slit-like holes 46b penetrating the dust collecting electrode body 46 may be provided at regular intervals in the circumferential direction of the dust collecting electrode body 46.

(example 3)

Next, a third embodiment of the present invention will be described.

Fig. 27 is a schematic cross-sectional view showing an air cleaner according to a third embodiment of the present invention.

As shown in FIG. 27, the dust collecting electrode body 46 of the dust collector 4 of the air cleaner 1-3 applied to this embodiment is tapered in cross section.

That is, the upper half portion of the collecting electrode body 46 is tapered, and the opening diameter of the upper opening 45A is larger than that of the lower opening 45B.

With this configuration, a large amount of air is smoothly sucked into the dust collecting electrode body 46 from the upper opening 45A having a large diameter by the rotation of the screw 21(22 to 24), and is forcibly discharged from the lower opening 45B.

Since other configurations, operations, and functions are the same as those of the first and second embodiments, the description thereof is omitted.

(example 4)

Next, a fourth embodiment of the present invention will be described.

Fig. 28 is a schematic cross-sectional view showing an air cleaner according to a fourth embodiment of the present invention.

As shown in fig. 28, the air cleaner 1-4 of this embodiment is configured such that the dust collecting electrode 45 of the dust collector 4 is mounted on the aircraft 2 in the reverse direction.

Specifically, the dust collecting electrode 45 illustrated in the above embodiment is directed upward, the center chamber 40 is disposed in the dust collecting electrode 45, and the center chamber 40 is attached to the center chamber attachment portion 47a of the rib 47.

The lower end position U of the dust collecting electrode 45 is set to a position near above the rotating surface S of the propellers 21 to 24 so that the propellers 21 to 24 can suck sufficient air into the dust collecting electrode 45.

Since other configurations, actions, and functions are the same as those of the first to third embodiments, their description is omitted.

(example 5)

Next, a fifth embodiment of the present invention will be described.

Fig. 29 is a perspective view showing an air cleaner according to a fifth embodiment of the present invention.

As shown in fig. 29, the air cleaner 1-5 of this embodiment is different from the air cleaners 1-1 to 1-4 of the first to fourth embodiments described above in that a small dust collector 4' is attached to all of the propellers 21 to 24 of the aircraft 2.

Each dust collector 4 'is constituted by discharge electrodes 41 to 44 and a dust collecting electrode 45' substantially in the same manner as the dust collector 4 described above.

That is, the dust collecting electrode 45 'is composed of a cylindrical dust collecting electrode body 46' opened upward and downward, and a plurality of ribs 47 'supporting the dust collecting electrode body 46' and the center chamber 40.

These dust collectors 4 'are mounted on the propellers 21(22 to 24) by means of an unillustrated mount, and the boost portions 33 of the dust collectors 4' are connected to the control portion 30 in the main body 20 by unillustrated wiring.

Fig. 30 is a schematic sectional view showing a state where the dust collector 4 'is mounted at the lowermost position, and fig. 31 is a schematic sectional view showing a state where the dust collector 4' is mounted at the uppermost position.

As shown in fig. 30 and 31, in each dust collector 4', similarly to the dust collector 4 of the above-described embodiment, each dust collector 4' is attached to each screw 21(22 to 24) such that the center position M of each dust collecting electrode 45 'is equal to or more than the rotation surface S of each screw 21(22 to 24), and the lower end position U of each dust collecting electrode 45' is equal to or less than the position in the vicinity of the upper side of the rotation surface S of each screw 21(22 to 24).

With this configuration, by operating the four dust collectors 4' in the floating state of the aircraft 2, the dust particles in the air flowing into the respective dust collecting electrodes 45 ' can be collected by the dust collecting electrode main bodies 46 '.

Further, since the dust collector 4' is attached to each of the propellers 21(22 to 24) so that the center position M of each of the dust collecting electrodes 45 ' becomes equal to or more than the rotation surface S of each of the propellers 21(22 to 24) and the lower end position U of each of the dust collecting electrodes 45 ' becomes equal to or less than the position near the upper side of the rotation surface S, high dust collecting capability can be exhibited as in the above-described embodiment.

Since other configurations, actions, and effects are the same as those of the first to fourth embodiments, the description thereof is omitted.

(example 6)

Next, a sixth embodiment of the present invention will be described.

Fig. 32 is a schematic cross-sectional view showing an air cleaner according to a sixth embodiment of the present invention.

The air cleaner 1-6 of this embodiment is different from the first to fifth embodiments described above in that the dust collecting electrode body 46 of the dust collector 4 has an aluminum-plated film.

In general, it is considered that the dust collecting effect is higher when a material having an appropriate volume resistivity close to an insulator but not a complete insulator is disposed on the surface of the conductive member than the dust collecting effect of the conductive member serving as the dust collecting electrode alone.

This embodiment is completed with this point in mind. Specifically, as shown in fig. 32, the dust collecting electrode body 46 is configured by forming an aluminum-plated film 48a on the inner surface of a support frame 48b formed of polyethylene terephthalate (PET) having high strength and high insulation. The dust collecting electrode body 46 is attached to the rib 47 so that the aluminum-plated film 48a is electrically connected to the rib 47 having conductivity.

Accordingly, when a high voltage is applied between the conductive aluminum plated film 48a and the discharge electrodes 41 to 44, dust is trapped on the aluminum plated film 48a side, but the aluminum oxide film generated on the surface of the aluminum plated film 48a is a material having an appropriate volume resistivity close to an insulator but not a complete insulator, and therefore the dust collection rate of the dust collection electrode body 46 can be further improved by the effect of the aluminum oxide film.

Since other configurations, operations, and effects are the same as those of the first to fifth embodiments, the description thereof is omitted.

(modification 3)

Fig. 33 is a schematic sectional view showing a modification of the sixth embodiment.

From the same viewpoint as that of the sixth embodiment, the dust collecting electrode body 46 shown in fig. 33 can be also presented.

That is, the dust collecting electrode body 46 is configured by disposing a conductive carbon ink (carbon ink)49a on the inner surface of the support frame 48b and attaching a vinyl chloride sheet 49b to the surface of the carbon film 49 a.

Accordingly, when a high voltage is applied between the conductive carbon ink 49a and the discharge electrodes 41 to 44, dust is trapped on the carbon ink 49a side, but since the vinyl chloride sheet 49b provided on the surface of the carbon ink 49a is a material having an appropriate volume resistivity, the dust collection rate of the dust collecting electrode main body 46 can be further improved by the influence of the vinyl chloride sheet 49 b.

The present invention is not limited to the above-described embodiments, and various changes and modifications can be made within the scope of the gist of the present invention.

For example, although the discharge electrodes 41 to 44 are set as negative electrodes and the dust collecting electrode bodies 46 and 46 'are set as positive electrodes in the above embodiment, an air cleaner in which the discharge electrodes 41 to 44 are set as positive electrodes and the dust collecting electrode bodies 46 and 46' are set as negative electrodes is also included in the scope of the present invention.

In addition, although the discharge electrodes 41 to 44 using carbon brushes have been exemplified in the above embodiment, an air cleaner having a discharge electrode using a needle-like or sharp conductor piece instead of a brush-like one is also within the scope of the present invention.

Further, in the fifth embodiment, the dust collector 4 'is mounted on all of the four propellers 21 to 24, but the dust collector 4' may be mounted on at least one of the four propellers 21 to 24. An air cleaner in which the dust collector 4' is mounted only on one of the propellers 21 to 24 is also included in the scope of the present invention.

Description of the reference numerals

1-1 to 1-6, 10-1 to 10-4 air cleaner

2 aircraft

4. 4', 100-1 to 100-10 dust collector

5 Loading and unloading mechanism

20 body part

21 to 24 propeller

21a to 24a motor

21b to 24b rotation axis

25 to 28 frame

30 control part

30a memory

30b, 30c, 33b to 33e wiring

31 power supply unit

33. 103 boost part

34 receiving part

35 antenna

36 insulation type DC/DC converter

40 center chamber

40a peripheral surface

40b lower surface

40c upper surface

41-44, 102 discharge electrode

45. 45', 101 dust collecting electrode

45A upper opening

45B lower opening

46. 46' dust collecting electrode body

46a, 46b holes

47. 47' Rib

47a center chamber mounting part

48a aluminum plating film

48b support frame

49a carbon ink

49b vinyl chloride sheet

51 to 54 support post

51a to 54a magnet sheet

56 to 59 placing parts

56a to 59a magnet pieces

110 chamber

200 circulator

201. 202 honeycomb sieve pore

210 ion number measuring device

A air

A⁺、A^-Air ion

D space

E electric field

M central position

P dust

P-charged dust

S surface of revolution

U lower extreme position.