CN212654545U - Special cleaning rod for cleaning and waxing outside airplane - Google Patents

Special cleaning rod for cleaning and waxing outside airplane Download PDF

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Publication number
CN212654545U
CN212654545U CN202021421939.2U CN202021421939U CN212654545U CN 212654545 U CN212654545 U CN 212654545U CN 202021421939 U CN202021421939 U CN 202021421939U CN 212654545 U CN212654545 U CN 212654545U
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China
Prior art keywords
rod
cleaning
waxing
exterior
clean
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Active
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CN202021421939.2U
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Chinese (zh)
Inventor
徐强清
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Hangzhou Tianwei Aviation Technology Service Co Ltd
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Hangzhou Tianwei Aviation Technology Service Co Ltd
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Priority to CN202021421939.2U priority Critical patent/CN212654545U/en
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Abstract

The utility model provides a special clean pole of waxing of aircraft outside cleanness belongs to burnisher technical field. This special clean pole of waxing of aircraft outside cleanness includes clean mechanism and body of rod mechanism, clean mechanism includes pedestal, motor, bull stick and rotating assembly, rotating assembly includes circle box, spacing ring, cleaning brush, thread bush and threaded rod, the motor connect in the pedestal inner wall, the bull stick install in the output shaft of motor, the thread bush connect in bull stick one end. The utility model discloses a third bracing piece, pull rod, non slipping spur, stay cord, drum, first bracing piece, axostylus axostyle, second bracing piece, pedestal, spring, motor, bull stick, thread bush, threaded rod and cleaning brush's effect to reached the purpose that clean efficient, improved the clean inefficiency of current cleaning rod, the outside shape of aircraft is irregular, people are parallel with clean department with the difficult adjustment of angle when using cleaning rod, clean not good problem of effect.

Description

Special cleaning rod for cleaning and waxing outside airplane
Technical Field
The utility model relates to a burnisher field particularly, relates to the clean special clean pole of waxing of aircraft outside.
Background
Because the aircraft is very big, need clean waxing with the cleaning rod when the aircraft is clean in some places, and the clean inefficiency of current cleaning rod, the outside shape of aircraft is irregular, and the angle is difficult for adjusting when people use the cleaning rod to be parallel with clean department, and clean effect is not good.
SUMMERY OF THE UTILITY MODEL
In order to compensate the above deficiency, the utility model provides a special clean pole of waxing of aircraft outside cleanness aims at improving the problem of clean inefficiency.
The utility model discloses a realize like this:
the utility model provides a special clean pole of aircraft outside clean waxing, including clean mechanism and body of rod mechanism.
The cleaning mechanism comprises a base, a motor, a rotating rod and a rotating assembly, the rotating assembly comprises a round box, a limiting ring, a cleaning brush, a threaded sleeve and a threaded rod, the motor is connected to the inner wall of the base, the rotating rod is installed on an output shaft of the motor, the threaded sleeve is connected to one end of the rotating rod, the threaded rod is in threaded connection with the threaded sleeve, the round box is installed at one end of the threaded rod, the limiting ring is connected to the inner wall of the round box, the cleaning brush is filled in an inner cavity of the round box, the limiting ring can clamp the cleaning brush, the rod body mechanism comprises an air drying assembly, a rotating assembly and an adjusting assembly, the air drying assembly comprises a cylinder, the rotating assembly comprises a first supporting rod, a shaft rod and a second supporting rod, the adjusting assembly comprises a third supporting rod, a pull rope, a pull ring, a spring, an, the second support rods are connected to one side of the seat body, the number of the second support rods is two, the shaft lever is rotatably connected to the inner side of the second support rods, the first support rod is arranged at one end of the shaft rod, the cylinder is connected with one end of the first support rod, the third supporting rod is arranged at one end of the cylinder, a through groove is arranged on the third supporting rod, the spring is connected to the inner wall of the through groove, the anti-skid block is arranged at one end of the spring, the pull rod is connected with two sides of the anti-skid block and penetrates through the third supporting rod in a sliding manner, the pull rings are arranged on one side of the seat body, the number of the pull rings is two, two ends of the pull rope are respectively connected with the pull rings, the pull rope penetrates through the through groove, the anti-skid block can press the pull rope tightly, and the third supporting rod is provided with a control switch.
In the embodiment of the utility model, the cleaning brush is a brush or a sponge.
The utility model discloses a special clean pole embodiment of waxing of aircraft outside cleanness, the spout has been seted up to third bracing piece both sides, the pull rod slide run through in the spout.
The utility model discloses an in the special clean pole embodiment of the outside clean waxing of aircraft, air-dry the subassembly and still include reinforcing plate, the mouth that charges, battery case and fan, the battery case connect in the drum inner wall, the battery install in battery case inner wall, the mouth that charges set up in battery case one side, the fan connect in the drum inner wall, the reinforcing plate install in the drum inner wall, reinforcing plate one side with the battery case is connected.
The utility model discloses an in the special clean pole embodiment of waxing of aircraft outside cleanness, the air-out end of fan runs through the pipeline drum and pedestal intercommunication.
The utility model discloses an in the special clean pole embodiment of the outside clean waxing of aircraft, the third through-hole has been seted up to the drum, third through-hole inner chamber fixedly connected with filter screen.
In the embodiment of the utility model discloses a clean pole embodiment of special use of waxing of aircraft outside, the mouth that charges runs through and extends to the drum is outside.
The utility model discloses an in the special clean pole embodiment of the outside clean waxing of aircraft, the wind chamber has been seted up to the pedestal internal surface, the second through-hole has been seted up to pedestal one side, the second through-hole with wind chamber intercommunication.
The utility model discloses an in the special clean pole embodiment of the outside clean waxing of aircraft, pedestal inner wall fixedly connected with baffle, first through-hole has been seted up to the baffle, the bull stick with first through-hole clearance fit.
The utility model discloses an in the special clean pole embodiment of aircraft outside cleaning waxing, antiskid cover has been cup jointed to third bracing piece one end.
The utility model has the advantages that: the utility model obtains the special cleaning rod for cleaning and waxing the exterior of the airplane through the design, when in use, people hold the third support rod to enable the pull rod to move downwards, the pull rod can drive the anti-skid block to move downwards, at the moment, the stay cord can move in the through groove, the cylinder can rotate with the seat body through the first support rod, the shaft rod and the second support rod, according to the inclination angle of the part to be cleaned outside the airplane, the stay cord is pulled, the stay cord can drive the seat body to rotate around the shaft rod, the seat body and the third support rod form different angles, thereby the seat body and the exterior of the airplane form different angles, the seat body is parallel to the part to be cleaned of the airplane, the pull rod is released, the elastic force of the spring can drive the anti-skid block to move upwards, the stay cord is fixed by the anti-skid block and the third support rod, the inclination angle of the, the bull stick can drive the thread bush and rotate, the thread bush can drive the threaded rod and rotate, the threaded rod can drive the cleaning brush and rotate, remove the cleaning position with the cleaning brush, the cleaning brush is rotatory, self-cleaning, it is effectual to clean, and can be as required clear intensity, it cleans to change brush or sponge, thereby the purpose that cleaning efficiency is high has been reached, the clean inefficiency of current cleaning rod has been improved, the outside shape of aircraft is irregular, people are parallel with clean department with the difficult adjustment of angle when using the cleaning rod, clean not good problem of effect.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings that are required to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present invention, and therefore should not be considered as limiting the scope, and for those skilled in the art, other related drawings can be obtained according to the drawings without inventive efforts.
Fig. 1 is a schematic structural view of a cleaning rod special for cleaning and waxing the exterior of an airplane according to an embodiment of the present invention;
fig. 2 is a schematic structural view of a cleaning mechanism according to an embodiment of the present invention at a first viewing angle;
fig. 3 is a schematic structural view of a cleaning mechanism according to an embodiment of the present invention at a second viewing angle;
fig. 4 is a schematic structural diagram of a rotating assembly according to an embodiment of the present invention;
fig. 5 is a schematic structural view of a rod mechanism according to an embodiment of the present invention;
fig. 6 is a schematic structural view of an air drying assembly according to an embodiment of the present invention;
fig. 7 is a schematic structural view of a rotating assembly according to an embodiment of the present invention;
fig. 8 is a schematic structural diagram of an adjusting assembly according to an embodiment of the present invention.
In the figure: 10-a cleaning mechanism; 110-a seat body; 120-a motor; 130-a first via; 140-a rotating rod; 150-a rotating assembly; 151-round box; 152-a stop collar; 153-cleaning brush; 154-thread bush; 155-threaded rod; 160-a second via; 170-a separator; 180-air chamber; 20-a rod body mechanism; 210-air drying the component; 211-cylinder; 212-a filter screen; 213-a reinforcing plate; 214-a charging port; 215-a battery; 216-a battery compartment; 217-third via; 218-a fan; 220-a rotating assembly; 221-a first support bar; 222-a shaft; 223-a second support bar; 230-an adjustment assembly; 231-a third support bar; 232-pulling rope; 233-a tab; 234-a spring; 235-anti-skid blocks; 236-a pull rod; 237-chute; 238-through grooves; 240-anti-slip sleeve.
Detailed Description
To make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the drawings of the embodiments of the present invention are combined to clearly and completely describe the technical solutions of the embodiments of the present invention, and obviously, the described embodiments are some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and to simplify the description, but do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore should not be construed as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically limited otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
In the present disclosure, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact between the first and second features, or may comprise contact between the first and second features not directly. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
Examples
Referring to fig. 1, the present invention provides a cleaning rod for cleaning and waxing the exterior of an aircraft, including a cleaning mechanism 10 and a rod mechanism 20.
The rod mechanism 20 is fixedly installed on the cleaning mechanism 10, the cleaning mechanism 10 is used for cleaning the exterior of the airplane, and the rod mechanism 20 is used for adjusting the angle of the cleaning mechanism 10, so that the cleaning mechanism 10 is parallel to the portion, needing to be cleaned, of the exterior of the airplane, and the cleaning effect is good.
Referring to fig. 1, 2 and 4, the cleaning mechanism 10 includes a base 110, a motor 120, a rotating rod 140 and a rotating assembly 150, the rotating assembly 150 includes a round box 151, a limiting ring 152, a cleaning brush 153, a threaded sleeve 154 and a threaded rod 155, the motor 120 is connected to an inner wall of the base 110, specifically, the motor 120 is fixedly connected to an inner wall of the base 110 by welding, the rotating rod 140 is installed on an output shaft of the motor 120, specifically, the rotating rod 140 is fixedly installed on an output shaft of the motor 120 by welding, the threaded sleeve 154 is connected to one end of the rotating rod 140, specifically, the threaded sleeve 154 is fixedly connected to one end of the rotating rod 140 by welding, the threaded rod 155 is fixedly connected to the threaded sleeve 154, the round box 151 is installed on one end of the threaded rod 155, specifically, the round box 151 is fixedly installed on one end of the threaded rod 155 by welding, the limiting ring 152 is connected to an inner, the cleaning brush 153 is filled in the inner cavity of the round box 151, the limiting ring 152 can clamp the cleaning brush 153, the motor 120, the rotating rod 140 and the round box 151 are used for driving the cleaning brush 153 to rotate, so that the cleaning effect is good, and the cleaning brush 153 can be conveniently replaced through the round box 151, the limiting ring 152, the threaded sleeve 154 and the threaded rod 155.
In some specific embodiments, the cleaning brush 153 is a brush or a sponge.
Referring to fig. 1, 5, 6, 7, and 8, the rod mechanism 20 includes an air drying component 210, a rotating component 220, and an adjusting component 230, the air drying component 210 includes a cylinder 211, the rotating component 220 includes a first support rod 221, a shaft rod 222, and a second support rod 223, the adjusting component 230 includes a third support rod 231, a pull rope 232, a pull ring 233, a spring 234, an anti-slip block 235, and a pull rod 236, the second support rod 223 is connected to one side of the base 110, specifically, the second support rod 223 is fixedly connected to one side of the base 110 by welding, the two second support rods 223 are provided, the shaft rod 222 is rotatably connected to the inner side of the second support rod 223, specifically, the shaft rod 222 is rotatably connected to the inner side of the second support rod 223 by a bearing, the first support rod 221 is installed at one end of the shaft rod 222, specifically, the first support rod 221 is fixedly installed at one end of the, specifically, the cylinder 211 is fixedly connected to one end of the first support rod 221 by welding, the third support rod 231 is installed at one end of the cylinder 211, specifically, the third support rod 231 is fixedly installed at one end of the cylinder 211 by welding, the third support rod 231 is provided with a through groove 238, the spring 234 is connected to the inner wall of the through groove 238, specifically, the spring 234 is fixedly connected to the inner wall of the through groove 238 by welding, the anti-slip block 235 is installed at one end of the spring 234, specifically, the anti-slip block 235 is installed at one end of the spring 234 by welding, the pull rod 236 is connected to two sides of the anti-slip block 235, specifically, the pull rod 236 is fixedly connected to two sides of the anti-slip block 235 by welding, the pull rod 236 slidably penetrates through the third support rod 231, the pull ring 233 is installed at one side of the seat 110, specifically, the pull ring 233 is fixedly installed, the anti-slip block 235 can compress the pull rope 232, the third support bar 231 is provided with a control switch, the cylinder 211 and the seat body 110 can rotate to different angles through the first support bar 221, the shaft bar 222 and the second support bar 223, and the rotation angle of the cylinder 211 and the seat body 110 can be controlled through the pull rope 232, the pull ring 233, the spring 234, the anti-slip block 235 and the pull rod 236.
In some specific embodiments, sliding grooves 237 are formed on both sides of the third support rod 231, the pull rod 236 slidably penetrates through the sliding grooves 237, the air drying assembly 210 further includes a reinforcing plate 213, a charging port 214, a storage battery 215, a battery box 216 and a blower 218, the battery box 216 is connected to the inner wall of the cylinder 211, specifically, the battery box 216 is fixedly connected to the inner wall of the cylinder 211 by welding, the storage battery 215 is mounted to the inner wall of the battery box 216, the charging port 214 is disposed on one side of the battery box 216, the blower 218 is connected to the inner wall of the cylinder 211 by welding, the reinforcing plate 213 is mounted to the inner wall of the cylinder 211, specifically, the reinforcing plate 213 is fixedly mounted to the inner wall of the cylinder 211 by welding, one side of the reinforcing plate 213 is connected to the battery box 216, specifically, one side of the reinforcing plate 213 is fixedly connected to the battery box 216 by welding, third through hole 217 has been seted up to drum 211, third through hole 217 inner chamber fixedly connected with filter screen 212, it is specific, third through hole 217 inner chamber is through welded fastening connected with filter screen 212, it runs through and extends to the drum 211 outside to charge mouthful 214, antiskid cover 240 has been cup jointed to third bracing piece 231 one end, fan 218 and third through hole 217 are used for blowing wind to the outside clean department of aircraft, air-dry with higher speed, filter screen 212 is arranged in the dust of filtered air, reinforcing plate 213 is arranged in improving the stability of battery case 216, battery 215 is used for fan 218 and the power supply of motor 120.
Referring to fig. 2 and 3, an air cavity 180 is formed in the inner surface of the seat body 110, a second through hole 160 is formed in one side of the seat body 110, the second through hole 160 is communicated with the air cavity 180, a partition plate 170 is fixedly connected to the inner wall of the seat body 110, a first through hole 130 is formed in the partition plate 170, the rotating rod 140 is in clearance fit with the first through hole 130, the air cavity 180 and the second through hole 160 are used for blowing air generated by the fan 218 to an aircraft surface cleaning place, and the partition plate 170 is used for protecting the motor 120 and reducing water or dust from entering the motor 120.
The working principle of the special cleaning rod for cleaning and waxing the exterior of the airplane is as follows: when the airplane cleaning device is used, a user holds the third support rod 231 by hand, so that the pull rod 236 moves downwards, the pull rod 236 drives the anti-slip block 235 to move downwards, the pull rope 232 can move in the through groove 238 at the moment, the cylinder 211 can rotate with the seat body 110 through the first support rod 221, the shaft rod 222 and the second support rod 223, according to the inclination angle of the part to be cleaned outside the airplane, the pull rope 232 is pulled, the pull rope 232 can drive the seat body 110 to rotate around the shaft rod 222, the seat body 110 and the third support rod 231 form different angles, so that the seat body 110 and the outside of the airplane form different angles, the seat body 110 is parallel to the part to be cleaned of the airplane, the pull rod 236 is released, the elastic force of the spring 234 can drive the anti-slip block 235 to move upwards, the anti-slip block 235 and the third support rod 231 fix the pull rope 232, so that the inclination angles of the seat body 110 and the, the bull stick 140 can drive thread bush 154 and rotate, thread bush 154 can drive threaded rod 155 and rotate, threaded rod 155 can drive cleaning brush 153 and rotate, brush 153 will be cleaned and remove clean position, cleaning brush 153 is rotatory, self-cleaning, it is clean effectual, and can be as required clear intensity, it cleans to change brush or sponge, thereby reached the purpose that clean efficient, it is low to have improved the clean inefficiency of current cleaning rod, the outside shape irregularity of aircraft, people are parallel with clean department with the difficult adjustment of angle when using cleaning rod, the problem that clean effect is not good.
It should be noted that the specific model specifications of the storage battery 215, the motor 120, and the fan 218 need to be determined by model selection according to the actual specification of the device, and the specific model selection calculation method adopts the prior art in the field, so detailed description is omitted.
The power supply of the battery 215 to the motor 120 and the fan 218 and the principle thereof will be clear to those skilled in the art and will not be described in detail herein.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (10)

1. The special cleaning rod for cleaning and waxing the exterior of the airplane is characterized by comprising
The cleaning mechanism (10), the cleaning mechanism (10) comprises a base body (110), a motor (120), a rotating rod (140) and a rotating component (150), the rotating component (150) comprises a round box (151), a limiting ring (152), a cleaning brush (153), a threaded sleeve (154) and a threaded rod (155), the motor (120) is connected to the inner wall of the seat body (110), the rotating rod (140) is arranged on the output shaft of the motor (120), the threaded sleeve (154) is connected to one end of the rotating rod (140), the threaded rod (155) is in threaded connection with the threaded sleeve (154), the round box (151) is arranged at one end of the threaded rod (155), the limit ring (152) is connected with the inner wall of the round box (151), the cleaning brush (153) is filled in the inner cavity of the round box (151), and the limiting ring (152) can clamp the cleaning brush (153);
the rod body mechanism (20), the rod body mechanism (20) comprises an air drying component (210), a rotating component (220) and an adjusting component (230), the air drying component (210) comprises a cylinder (211), the rotating component (220) comprises a first supporting rod (221), a shaft rod (222) and a second supporting rod (223), the adjusting component (230) comprises a third supporting rod (231), a pull rope (232), a pull ring (233), a spring (234), an anti-slip block (235) and a pull rod (236), the second supporting rod (223) is connected to one side of the base body (110), the number of the second supporting rods (223) is two, the shaft rod (222) is rotatably connected to the inner side of the second supporting rod (223), the first supporting rod (221) is installed at one end of the shaft rod (222), the cylinder (211) is connected to one end of the first supporting rod (221), and the third supporting rod (231) is installed at one end of the cylinder (211), a through groove (238) is formed in the third support rod (231), the spring (234) is connected to the inner wall of the through groove (238), the anti-slip block (235) is installed at one end of the spring (234), the pull rod (236) is connected to two sides of the anti-slip block (235), the pull rod (236) penetrates through the third support rod (231) in a sliding manner, the pull rings (233) are installed at one side of the seat body (110), the number of the pull rings (233) is two, two ends of the pull rope (232) are respectively connected to the pull rings (233), the pull rope (232) penetrates through the through groove (238), the anti-slip block (235) can compress the pull rope (232), and a control switch is arranged on the third support rod (231).
2. The special cleaning rod for cleaning and waxing the exterior of an airplane according to claim 1, wherein the cleaning brush (153) is a brush or a sponge.
3. The special cleaning rod for cleaning and waxing the exterior of an airplane according to claim 1, wherein sliding grooves (237) are formed in two sides of the third supporting rod (231), and the pull rod (236) penetrates through the sliding grooves (237) in a sliding manner.
4. The cleaning rod special for cleaning and waxing the exterior of an airplane according to claim 1, wherein the air drying assembly (210) further comprises a reinforcing plate (213), a charging port (214), a storage battery (215), a battery box (216) and a fan (218), the battery box (216) is connected to the inner wall of the cylinder (211), the storage battery (215) is mounted on the inner wall of the battery box (216), the charging port (214) is arranged on one side of the battery box (216), the fan (218) is connected to the inner wall of the cylinder (211), the reinforcing plate (213) is mounted on the inner wall of the cylinder (211), and one side of the reinforcing plate (213) is connected with the battery box (216).
5. The special cleaning rod for cleaning and waxing the exterior of an airplane according to claim 4, wherein the air outlet end of the fan (218) is communicated with the seat body (110) through the cylinder (211) by a pipeline.
6. The special cleaning rod for cleaning and waxing the exterior of an airplane according to claim 4, wherein a third through hole (217) is formed in the cylinder (211), and a filter screen (212) is fixedly connected to an inner cavity of the third through hole (217).
7. The aircraft exterior cleaning and waxing dedicated cleaning pole according to claim 4, wherein said charging port (214) extends through to the exterior of said cylinder (211).
8. The special cleaning rod for cleaning and waxing the exterior of an airplane according to claim 1, wherein an air cavity (180) is formed on the inner surface of the seat body (110), a second through hole (160) is formed on one side of the seat body (110), and the second through hole (160) is communicated with the air cavity (180).
9. The special cleaning rod for cleaning and waxing the exterior of an airplane according to claim 1, wherein a partition plate (170) is fixedly connected to the inner wall of the seat body (110), a first through hole (130) is formed in the partition plate (170), and the rotating rod (140) is in clearance fit with the first through hole (130).
10. The special cleaning rod for cleaning and waxing the exterior of an airplane according to claim 1, wherein an anti-slip sleeve (240) is sleeved at one end of the third supporting rod (231).
CN202021421939.2U 2020-07-17 2020-07-17 Special cleaning rod for cleaning and waxing outside airplane Active CN212654545U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202021421939.2U CN212654545U (en) 2020-07-17 2020-07-17 Special cleaning rod for cleaning and waxing outside airplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202021421939.2U CN212654545U (en) 2020-07-17 2020-07-17 Special cleaning rod for cleaning and waxing outside airplane

Publications (1)

Publication Number Publication Date
CN212654545U true CN212654545U (en) 2021-03-05

Family

ID=74769775

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202021421939.2U Active CN212654545U (en) 2020-07-17 2020-07-17 Special cleaning rod for cleaning and waxing outside airplane

Country Status (1)

Country Link
CN (1) CN212654545U (en)

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