CN207899791U - A kind of aircraft engine component cleaning system - Google Patents

A kind of aircraft engine component cleaning system Download PDF

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Publication number
CN207899791U
CN207899791U CN201721760821.0U CN201721760821U CN207899791U CN 207899791 U CN207899791 U CN 207899791U CN 201721760821 U CN201721760821 U CN 201721760821U CN 207899791 U CN207899791 U CN 207899791U
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CN
China
Prior art keywords
cleaning
rack
clean room
nozzles
aircraft engine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201721760821.0U
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Chinese (zh)
Inventor
孟引根
徐薇
杨芸
李龙
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SHANGHAI CHINDT SYSTEMS AND SERVICES Co Ltd
Original Assignee
SHANGHAI CHINDT SYSTEMS AND SERVICES Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SHANGHAI CHINDT SYSTEMS AND SERVICES Co Ltd filed Critical SHANGHAI CHINDT SYSTEMS AND SERVICES Co Ltd
Priority to CN201721760821.0U priority Critical patent/CN207899791U/en
Application granted granted Critical
Publication of CN207899791U publication Critical patent/CN207899791U/en
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Abstract

The utility model discloses a kind of aircraft engine component cleaning systems,The cleaning system includes clean room,It is fixedly arranged on the rack of bottom in the clean room,The rotary electric machine being fixedly arranged in the rack,The turntable for being fixedly connected with the output shaft of the rotary electric machine and being rotated with output shaft,It is fixedly arranged on the rack for cleaning for rotating and be used to place engine components above the turntable with the turntable,The turntable is equipped with a plurality of the first nozzles sprayed water to the rack for cleaning direction,The cleaning system further includes being fixedly arranged on indoor " L " the shape spraying rack of the cleaning,The spraying rack includes the vertical tube for being set to the rack for cleaning side,And it is fixedly arranged on a plurality of second nozzles on the vertical tube,The spraying rack further includes being set to the fixed transverse tube being connected to vertical with the vertical tube top above the rack for cleaning,And it is fixedly arranged on a plurality of third nozzles on the transverse tube,Second nozzle and third nozzle are sprayed water to the rack for cleaning direction,The cleaning system further includes the head cover slidably covered at the top of the clean room.

Description

A kind of aircraft engine component cleaning system
Technical field
The utility model is related to a kind of cleaning systems, more specifically to a kind of aircraft engine component cleaning system.
Background technology
Existing cleaning device is in cleaning machinery equipment, it usually needs user cleans manually, cannot achieve automatic Cleaning to mechanical equipment causes working efficiency relatively low.
Utility model content
The technical problem to be solved by the present invention is to for the drawbacks described above of the prior art, provide a kind of aircraft hair Motivation component cleaning system.
Technical solution adopted by the utility model to solve its technical problems is:Construct a kind of aircraft engine component cleaning System, the cleaning system include clean room, are fixedly arranged on the rack of bottom in the clean room, the rotation being fixedly arranged in rack electricity Machine, the turntable for being fixedly connected with the output shaft of the rotary electric machine and being rotated with output shaft are fixedly arranged on above the turntable with the turntable The rack for cleaning of engine components is rotated and is used to place, which is equipped with a plurality of the first sprays sprayed water to the rack for cleaning direction Head, the cleaning system further include being fixedly arranged on indoor " L " the shape spraying rack of the cleaning, which includes being set to the rack for cleaning one The vertical tube of side and a plurality of second nozzles being fixedly arranged on the vertical tube, the spraying rack further include being set to above the rack for cleaning The fixed transverse tube being connected to vertical with the vertical tube top and a plurality of third nozzles being fixedly arranged on the transverse tube, second nozzle It sprays water to the rack for cleaning direction with third nozzle, which further includes the top slidably covered at the top of the clean room At least one Pneumatic extension bar for driving the head cover to move up and down above the clean room roof is covered and is set to, this is clear The system of washing further includes the high pressure being connected to simultaneously with a plurality of first nozzles, a plurality of second nozzles and a plurality of third nozzles Pump.
It is equipped with and uses in aircraft engine component cleaning system described in the utility model, between the turntable and the rack for cleaning In the fixed at least supporting rod for supporting the rack for cleaning.
In aircraft engine component cleaning system described in the utility model, the rack for cleaning be equipped with for this plurality of the A plurality of first hole for water sprayings or the first water spray gap that one nozzle top is pierced by.
In aircraft engine component cleaning system described in the utility model, which further includes being set to this clearly The pistol that chamber wash side is connected to the high-pressure pump by movable water pipe.
In aircraft engine component cleaning system described in the utility model, which is equipped with transparent observing Window.
In aircraft engine component cleaning system described in the utility model, which further includes and the clean room The sewage recovering system of connection.
In aircraft engine component cleaning system described in the utility model, which includes and the cleaning The steam condenser of ceiling end connection and the Sewage treatment case being connected to the steam condenser, the sewage recovering system also wrap The positive displacement pump being connected to the clean room bottom is included, which is connected to the Sewage treatment case.
The aircraft engine component cleaning system for implementing the utility model, has the advantages that:It is new using this practicality When the aircraft engine component cleaning system of type, aircraft engine component is positioned on rack for cleaning, starts rotary electric machine and drives Turntable and rack for cleaning rotation, the first nozzle being located on turntable carry out spraying-rinsing to engine components bottom, in turntable and clearly It washes in frame rotation process, the second nozzle on vertical tube is to engine components side spraying-rinsing, and third nozzle on transverse tube is to hair The top surface spraying-rinsing of motivation component is realized and is cleaned to the comprehensive of engine, multi-angle, improves cleaning efficiency.
Description of the drawings
Below in conjunction with accompanying drawings and embodiments, the utility model is described in further detail, in attached drawing:
Fig. 1 is the structural schematic diagram of the utility model aircraft engine component cleaning system.
Specific implementation mode
It is new to this practicality below in conjunction with attached drawing to keep the purpose of this utility model, technical solution and advantage clearer Type embodiment is described in further detail.
As shown in Figure 1, in the aircraft engine component cleaning system first embodiment of the utility model, the cleaning system 1 include clean room 2, be fixedly arranged on the rack 3 of bottom in the clean room 2, the rotary electric machine 4 being fixedly arranged in the rack 3, with the rotation The output shaft of motor 4 be fixedly connected and rotated with output shaft turntable 5, be fixedly arranged on 5 top of the turntable and be used in combination with the turntable 5 rotation In the rack for cleaning 6 for placing engine components, which is equipped with a plurality of the first nozzles 7 sprayed water to 6 direction of rack for cleaning, The cleaning system 1 further includes " L " the shape spraying rack being fixedly arranged in the clean room 2, which includes being set to the rack for cleaning 6 one The vertical tube 9 of side and a plurality of second nozzles 10 being fixedly arranged on the vertical tube 9, the spraying rack further include being set to the rack for cleaning 6 The top fixed transverse tube 11 being connected to vertical with the vertical tube top and a plurality of third nozzles 12 being fixedly arranged on the transverse tube 11, Second nozzle 10 and third nozzle 12 are sprayed water to 6 direction of rack for cleaning, which further includes slidably covering at this It the head cover 13 at the top of clean room 2 and is set to above 2 roof of clean room for driving the head cover 13 to move up and down at least One Pneumatic extension bar 14, the cleaning system 1 further include simultaneously with a plurality of first nozzles 7, a plurality of second nozzles 10 and The high-pressure pump that a plurality of third nozzles 12 are connected to.
Using the utility model aircraft engine component cleaning system 1 when, aircraft engine component is positioned over cleaning On frame 6, start rotary electric machine 4 and turntable 5 and rack for cleaning 6 is driven to rotate, is located at the first nozzle 7 on turntable 5 to engine components Bottom carries out spraying-rinsing, and in 6 rotation process of turntable 5 and rack for cleaning, the second nozzle 10 on vertical tube 9 is to engine components side Face spraying-rinsing, the third nozzle 12 on transverse tube 11 realize the full side to engine to the top surface spraying-rinsing of engine components Position, multi-angle cleaning, improve cleaning efficiency.
Specifically, being equipped between the turntable 5 and the rack for cleaning 6 for fixed at least one support for supporting the rack for cleaning 6 Bar.
The water sprayed for ease of the first nozzle 7 can be sprayed onto on engine components, the rack for cleaning 6 be equipped with for this plurality of the A plurality of first hole for water sprayings or the first water spray gap that one nozzle, 7 top is pierced by.
Further, which further includes being set to the purge chamber side with the high-pressure pump to connect by movable water pipe Logical pistol.Hand-holdable 12 less cleaning of pistol pair the first nozzle 7, the second nozzle 10 and third nozzle of user Place is cleaned.
Further, the situation in clean room 2 is observed for ease of user, which is equipped with transparent windows.
To make full use of water resource, which further includes the sewage recovering system being connected to the clean room 2.This is useless Water reclamation system includes that the steam condenser being connected to 2 top of clean room and the waste water being connected to the steam condenser are returned Case is received, which further includes the positive displacement pump being connected to 2 bottom of clean room, which connects with the Sewage treatment case It is logical.Condensing recovery is carried out to the steam in clean room 2 by steam condenser, it is preferred that in steam condenser and clean room 2 Be additionally provided with the vacuum pump steam in clean room 2 being pumped into steam condenser in connecting tube.It will be located at cleaning by positive displacement pump The waste water of 2 bottom of room is evacuated in recycling bins.
The above description is only the embodiments of the present invention, and it does not limit the scope of the patent of the present invention, every Equivalent structure or equivalent flow shift made based on the specification and figures of the utility model, is applied directly or indirectly in Other related technical areas are equally included in the patent within the scope of the utility model.

Claims (7)

1. a kind of aircraft engine component cleaning system, which is characterized in that the cleaning system includes clean room, it is described to be fixedly arranged on The rack of bottom, the rotary electric machine being fixedly arranged in the rack in clean room are fixedly connected with the output shaft of the rotary electric machine And with the turntable of output shaft rotation, be fixedly arranged on and rotated with the turntable above the turntable and be used to place the clear of engine components Frame is washed, the turntable is equipped with a plurality of the first nozzles sprayed water to the rack for cleaning direction, and the cleaning system further includes solid Set on indoor " L " the shape spraying rack of cleaning, the spraying rack includes vertical tube, the Yi Jigu for being set to the rack for cleaning side A plurality of second nozzles on the vertical tube, the spraying rack further include being set to above the rack for cleaning and the vertical tube The top vertically transverse tube of fixed connection and a plurality of third nozzles being fixedly arranged on the transverse tube, second nozzle and the Three nozzles are sprayed water to the rack for cleaning direction, and the cleaning system further includes the top slidably covered at the top of the clean room At least one Pneumatic extension bar for driving the head cover to move up and down above the clean room roof is covered and is set to, The cleaning system further includes being connected to simultaneously with a plurality of first nozzles, a plurality of second nozzles and a plurality of third nozzles High-pressure pump.
2. aircraft engine component cleaning system according to claim 1, which is characterized in that the turntable and the cleaning It is equipped between frame for the fixed at least supporting rod for supporting the rack for cleaning.
3. aircraft engine component cleaning system according to claim 2, which is characterized in that the rack for cleaning, which is equipped with, to be supplied A plurality of first hole for water sprayings or the first water spray gap that a plurality of first nozzles top is pierced by.
4. aircraft engine component cleaning system according to claim 1, which is characterized in that the cleaning system further includes It is set to the pistol that the clean room side is connected to the high-pressure pump by movable water pipe.
5. aircraft engine component cleaning system according to claim 1, which is characterized in that the clean room front is equipped with Transparent windows.
6. aircraft engine component cleaning system according to claim 1, which is characterized in that the cleaning system further includes The sewage recovering system being connected to the clean room.
7. aircraft engine component cleaning system according to claim 6, which is characterized in that the sewage recovering system packet The Sewage treatment case for including the steam condenser being connected to the clean room top and being connected to the steam condenser, it is described Sewage recovering system further includes the positive displacement pump being connected to the clean room bottom, and the positive displacement pump connects with the Sewage treatment case It is logical.
CN201721760821.0U 2017-12-17 2017-12-17 A kind of aircraft engine component cleaning system Active CN207899791U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721760821.0U CN207899791U (en) 2017-12-17 2017-12-17 A kind of aircraft engine component cleaning system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721760821.0U CN207899791U (en) 2017-12-17 2017-12-17 A kind of aircraft engine component cleaning system

Publications (1)

Publication Number Publication Date
CN207899791U true CN207899791U (en) 2018-09-25

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721760821.0U Active CN207899791U (en) 2017-12-17 2017-12-17 A kind of aircraft engine component cleaning system

Country Status (1)

Country Link
CN (1) CN207899791U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112122204A (en) * 2020-08-31 2020-12-25 江苏汤臣汽车零部件有限公司 High-pressure flushing device for automobile impeller

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112122204A (en) * 2020-08-31 2020-12-25 江苏汤臣汽车零部件有限公司 High-pressure flushing device for automobile impeller
CN112122204B (en) * 2020-08-31 2022-03-29 江苏汤臣汽车零部件有限公司 High-pressure flushing device for automobile impeller

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