CN214344987U - Fuel tanker aircraft management maintenance device - Google Patents

Fuel tanker aircraft management maintenance device Download PDF

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Publication number
CN214344987U
CN214344987U CN202120061693.0U CN202120061693U CN214344987U CN 214344987 U CN214344987 U CN 214344987U CN 202120061693 U CN202120061693 U CN 202120061693U CN 214344987 U CN214344987 U CN 214344987U
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fixed plate
fuselage
maintenance device
gear
rotating shaft
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CN202120061693.0U
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Chinese (zh)
Inventor
邹伟
杨正奇
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Individual
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Individual
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Abstract

The utility model discloses a device is maintained in fuel tanker aircraft management, including the fuselage, the inside fixed mounting of fuselage has the fixed plate, is equipped with stop gear on the fixed plate, and stop gear is connected with two splint, and the notch has been seted up to the bottom of fixed plate, and fixed plate bottom cavity position is equipped with moving mechanism, and moving mechanism's bottom is provided with meshing mechanism, and meshing mechanism is connected with the nut that is located the fuselage avris, and the top fixedly connected with motor of fixed plate, motor rotate and are connected with the washing post of surface bonding sponge, and the washing post passes the top surface of fuselage. The utility model discloses a set up the moving mechanism that cooperation meshing mechanism used, guaranteed the clamping control to splint under the user's operation, guaranteed the stability when wasing the filter core, rotate the washing post of connecting through setting up the motor, guaranteed the washing post to the abundant washing of crossing the filter core inner wall.

Description

Fuel tanker aircraft management maintenance device
Technical Field
The utility model relates to an tanker aircraft technical field specifically is a fuel tanker aircraft management maintains device.
Background
The fuel dispenser is developed along with the development of automobile and road traffic, and is a sale terminal of finished oil retail industry for sale and settlement metering equipment.
At present, in the maintenance to fuel tanker aircraft, need take off the filter core of filtering usefulness and wash, but the tubular structure inner wall of filter core washs often comparatively troublesome, if the filter core overlength will not carry out effective washing. Therefore, the management and maintenance device for the fuel dispenser is improved.
SUMMERY OF THE UTILITY MODEL
For solving the defect that prior art exists, the utility model provides a device is maintained in fuel tanker management.
In order to solve the technical problem, the utility model provides a following technical scheme:
the utility model relates to a device is maintained in fuel tanker aircraft management, the reciprocating impact tunnel drilling machine comprises a machine body, the inside fixed mounting of fuselage has the fixed plate, be equipped with stop gear on the fixed plate, stop gear is connected with two splint, the notch has been seted up to the bottom of fixed plate, the hollow position in fixed plate bottom is equipped with moving mechanism, moving mechanism's bottom is provided with meshing mechanism, meshing mechanism is connected with the nut that is located the fuselage avris, the top fixedly connected with motor of fixed plate, the motor rotates the washing post that is connected with the surface bonding sponge, the washing post passes the top surface of fuselage.
As a preferred technical scheme of the utility model, stop gear includes two draw-in grooves of seting up at the fixed plate top, the inside block of draw-in groove is connected with the block post, the top fixed mounting of block post has the connecting block.
As a preferred technical scheme of the utility model, splint pass the top fixed connection who sets up in the bottom of the spacing groove at fuselage top and splint and connecting block.
As a preferred technical scheme of the utility model, moving mechanism is including fixing the movable plate in the clamping column bottom, the bottom fixed mounting of movable plate has the rack.
As an optimal technical scheme of the utility model, the engagement mechanism is including rotating main pivot and the counter shaft of connection inside the fuselage, fixed connection master gear in the counter shaft, fixedly connected with pinion and pinion dish in the main pivot, pinion and pinion dish are connected with master gear and a rack toothing respectively, the inner wall and the nut fixed connection of fuselage are passed in the main pivot.
As an optimal technical scheme of the utility model, the nut pastes tightly on the outer wall of fuselage, the outer wall of fuselage adopts dull polish to handle.
The utility model has the advantages that: this kind of fuel tanker aircraft management maintains device through setting up the moving mechanism that the cooperation meshing mechanism used, has guaranteed the clamping control to splint under the user's operation, has guaranteed to wash the stability when crossing the filter core, rotates the washing post of connecting through setting up the motor, has guaranteed that the washing post is to crossing the abundant washing of filter core inner wall.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:
fig. 1 is a schematic structural view of a fuel dispenser management and maintenance device of the present invention;
fig. 2 is a schematic structural view of a fixing plate of the fuel dispenser management and maintenance device of the present invention;
fig. 3 is a schematic diagram of the internal structure of the fuel dispenser management and maintenance device of the present invention.
In the figure: 1. a body; 2. a fixing plate; 201. a card slot; 202. a snap post; 203. connecting blocks; 3. a splint; 4. a moving mechanism; 401. moving the plate; 402. a rack; 5. an engagement mechanism; 501. a main rotating shaft; 502. a pinion gear; 503. a main gear; 504. an auxiliary rotating shaft; 505. a pinion gear plate; 6. a motor; 7. cleaning the column; 8. a nut; 9. a limiting groove.
Detailed Description
The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are presented herein only to illustrate and explain the present invention, and not to limit the present invention.
Example (b): as shown in fig. 1, fig. 2 and fig. 3, the utility model relates to a fuel tanker management and maintenance device, including fuselage 1, the inside fixed mounting of fuselage 1 has fixed plate 2, be equipped with stop gear on the fixed plate 2, stop gear is connected with two splint 3, the notch has been seted up to the bottom of fixed plate 2, 2 bottom cavity positions of fixed plate are equipped with moving mechanism 4, moving mechanism 4's bottom is provided with meshing mechanism 5, meshing mechanism 5 is connected with the nut 8 that is located the 1 avris of fuselage, the top fixedly connected with motor 6 of fixed plate 2, motor 6 rotates the washing post 7 that is connected with the surface bonding sponge, washing post 7 passes the top surface of fuselage 1.
Wherein, stop gear includes two draw-in grooves 201 of seting up at 2 tops of fixed plate, and the inside block of draw-in groove 201 is connected with block post 202, and block post 202's top fixed mounting has connecting block 203, through setting up stop gear, has guaranteed the tight and unclamping operation of clamp plate 3 subassembly.
Wherein, splint 3 passes the top fixed connection who sets up the bottom of the spacing groove 9 and splint 3 at fuselage 1 top and connecting block 203, and splint 3 are the curved surface form and curvature radius are greater than by abluent filter core outer lane radius of circularity, through setting up the great splint 3 of curvature radius, have guaranteed the stable centre gripping to filtering the core.
Wherein, moving mechanism 4 is including fixing the movable plate 401 in the clamping column 202 bottom, and the rack 402 is installed to the bottom fixed mounting of movable plate 401, through setting up moving mechanism 4, has guaranteed the steady movement of splint 3.
The engaging mechanism 5 comprises a main rotating shaft 501 and an auxiliary rotating shaft 504 which are rotatably connected inside the machine body 1, a main gear 503 is fixedly connected to the auxiliary rotating shaft 504, an auxiliary gear 502 and an auxiliary gear disk 505 are fixedly connected to the main rotating shaft 501, the auxiliary gear 502 and the auxiliary gear disk 505 are respectively engaged with the main gear 503 and one rack 402, the main rotating shaft 501 penetrates through the inner wall of the machine body 1 and is fixedly connected with the nut 8, and the clamping of the clamping plate 3 can be controlled by a user by screwing the nut 8 through the engaging mechanism 5.
Wherein, nut 8 pastes tightly on the outer wall of fuselage 1, and the outer wall of fuselage 1 adopts dull polish to handle, has guaranteed that nut 8 can not take place easily after rotating and has rocked.
During operation, take out the inside back of crossing of tanker aircraft filter, the cover is on washing post 7, utilize crank block nut 8 and rotate, drive main pivot 501 and rotate, and then drive pinion 502, master gear 503 and pinion dish 505 rotate, and then make two movable plates 401 remove, splint 3 presss from both sides tightly crosses the filter core, can keep the spanner to avoid its removal on nut 8 this moment, water certain washing liquid to the top of washing post 7, the washing liquid is inhaled by the sponge, starting motor 6 drives and washs post 7 and rotates, the sponge on washing post 7 surface cleans the inner wall of crossing the filter core, take out after the cleanness is accomplished and cross the filter core and wash and dry and can install back filtration equipment and continue to use through the clear water.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. 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 (6)

1. The utility model provides a device is maintained in fuel tanker management, includes fuselage (1), its characterized in that, the inside fixed mounting of fuselage (1) has fixed plate (2), be equipped with stop gear on fixed plate (2), stop gear is connected with two splint (3), the notch has been seted up to the bottom of fixed plate (2), fixed plate (2) bottom cavity position is equipped with moving mechanism (4), the bottom of moving mechanism (4) is provided with meshing mechanism (5), meshing mechanism (5) are connected with nut (8) that are located fuselage (1) avris, the top fixedly connected with motor (6) of fixed plate (2), motor (6) rotate washing post (7) that are connected with the surface bonding sponge, washing post (7) pass the top surface of fuselage (1).
2. The fuel dispenser management and maintenance device as claimed in claim 1, wherein the limiting mechanism comprises two clamping grooves (201) formed in the top of the fixing plate (2), clamping columns (202) are clamped and connected in the clamping grooves (201), and connecting blocks (203) are fixedly mounted on the tops of the clamping columns (202).
3. The fuel dispenser management and maintenance device as claimed in claim 2, wherein the clamping plate (3) passes through a limiting groove (9) formed at the top of the body (1), and the bottom end of the clamping plate (3) is fixedly connected with the top end of the connecting block (203).
4. The fuel dispenser management and maintenance device as claimed in claim 1, wherein the moving mechanism (4) comprises a moving plate (401) fixed at the bottom end of the engaging column (202), and a rack (402) is fixedly mounted at the bottom end of the moving plate (401).
5. The fuel dispenser management and maintenance device as claimed in claim 4, wherein the engagement mechanism (5) comprises a main rotating shaft (501) and a secondary rotating shaft (504) which are rotatably connected inside the body (1), a main gear (503) is fixedly connected to the secondary rotating shaft (504), a secondary gear (502) and a secondary gear disk (505) are fixedly connected to the main rotating shaft (501), the secondary gear (502) and the secondary gear disk (505) are respectively engaged with the main gear (503) and a rack (402), and the main rotating shaft (501) penetrates through the inner wall of the body (1) and is fixedly connected with the nut (8).
6. The fuel dispenser management and maintenance device as claimed in claim 1, wherein the nut (8) is attached to the outer wall of the body (1), and the outer wall of the body (1) is frosted.
CN202120061693.0U 2021-01-11 2021-01-11 Fuel tanker aircraft management maintenance device Active CN214344987U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202120061693.0U CN214344987U (en) 2021-01-11 2021-01-11 Fuel tanker aircraft management maintenance device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202120061693.0U CN214344987U (en) 2021-01-11 2021-01-11 Fuel tanker aircraft management maintenance device

Publications (1)

Publication Number Publication Date
CN214344987U true CN214344987U (en) 2021-10-08

Family

ID=77954465

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202120061693.0U Active CN214344987U (en) 2021-01-11 2021-01-11 Fuel tanker aircraft management maintenance device

Country Status (1)

Country Link
CN (1) CN214344987U (en)

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