CN215236175U - Adjustable aircraft engine cleaning equipment - Google Patents
Adjustable aircraft engine cleaning equipment Download PDFInfo
- Publication number
- CN215236175U CN215236175U CN202022996946.1U CN202022996946U CN215236175U CN 215236175 U CN215236175 U CN 215236175U CN 202022996946 U CN202022996946 U CN 202022996946U CN 215236175 U CN215236175 U CN 215236175U
- Authority
- CN
- China
- Prior art keywords
- wall surface
- spray head
- shell
- rotary joint
- 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.)
- Expired - Fee Related
Links
- 238000004140 cleaning Methods 0.000 title abstract description 23
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 39
- 239000007921 spray Substances 0.000 claims abstract description 25
- 238000002347 injection Methods 0.000 claims abstract description 6
- 239000007924 injection Substances 0.000 claims abstract description 6
- 238000005406 washing Methods 0.000 claims description 10
- 230000000694 effects Effects 0.000 abstract description 2
- 238000011010 flushing procedure Methods 0.000 abstract 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Images
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- Cleaning By Liquid Or Steam (AREA)
Abstract
The utility model relates to the technical field of cleaning equipment, and discloses adjustable aircraft engine cleaning equipment, a control panel is fixedly installed at the upper end of the right wall surface of a shell, a water injection hole is arranged at the front end of the upper wall surface of the shell, a water outlet hole is arranged at the lower end of the front wall surface of the shell, a water pipe is sleeved in the water outlet hole, a rotary joint is fixedly installed at the front end of the water pipe, a clamping groove is respectively arranged at one side position where the outer circular wall surfaces of the rotary joint are far away from each other, a first dislocation block is fixedly installed at the front end of the inner circular wall surface of the rotary joint, a spray head is arranged at the front end of the outer circular wall surface of the rotary joint, a clamping block is fixedly installed at the rear end of the inner circular wall surface of the spray head, a second dislocation block is fixedly installed at the rear end of the inner circular wall surface of the spray head, water flow pressure is set on the control panel, the size of the water outlet of the water pipe is adjusted through dislocation rotation of the spray head and the rotary joint, flushing pressure and flow can be adjusted according to requirements, thereby controlling the impact force, having obvious cleaning effect and greatly improving the cleaning efficiency.
Description
Technical Field
The utility model relates to a cleaning equipment technical field specifically is an aircraft engine cleaning equipment with adjustable.
Background
The aircraft engine is generally referred to as an aircraft engine, the aircraft engine is a highly complex and precise thermal machine, is used as the heart of an aircraft, is not only the power of aircraft flight, but also an important driving force for promoting the development of aviation industry, and when the engine is maintained and maintained, the water pressure regulator of the existing cleaning machine is arranged at the bottom of the machine, so that the water pressure is not convenient to regulate, and therefore, an adjustable cleaning device for the aircraft engine is needed.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
The utility model provides an aircraft engine cleaning equipment with adjustable to be not enough to prior art, the utility model provides an but possess manual regulation water pressure, improve advantages such as washing flexibility ratio, solved in the past when maintaining and maintaining the engine, current cleaning machine water pressure regulator is installed in the machine bottom, is not convenient for adjust hydraulic problem.
(II) technical scheme
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an aircraft engine cleaning equipment with adjustable, which comprises an outer shell, both sides wall all is provided with the wheel around the shell, the right wall upper end fixed mounting of shell has control panel, the right wall fixed mounting of shell has the handle, the last wall rear end of shell is provided with portable power source, the water filling hole has been seted up to the last wall front end of shell, the apopore has been seted up to the preceding wall lower extreme of shell, the water pipe has been cup jointed to the inside of apopore, the front end fixed mounting of water pipe has rotary joint, the draw-in groove has all been seted up to one side position that rotary joint's excircle wall kept away from each other, inner circular wall front end fixed mounting of rotary joint has dislocation piece one, rotary joint's excircle wall front end is provided with the shower nozzle, the inner circular wall of shower nozzle is provided with two mouths shower nozzle, inner circular wall rear end fixed mounting of shower nozzle has the fixture block, the internal face rear end fixed mounting of shower nozzle has dislocation piece two.
Preferably, the water outlet hole is sleeved with the water pipe.
Preferably, there are four of the said dislocation blocks.
Preferably, openings are formed in the front side wall surface and the rear side wall surface of the spray head, and internal threads are formed in the front end of the inner circular wall surface of the spray head.
Preferably, the rear ends of the outer circle wall surfaces of the two nozzles are provided with external threads, and the two nozzles are connected with the nozzles through threads.
Preferably, the number of the clamping blocks is two, the positions of the clamping blocks correspond to the positions of the clamping grooves, and the clamping blocks are clamped with the clamping grooves.
(III) advantageous effects
Compared with the prior art, the utility model provides an aircraft engine cleaning equipment with adjustable possesses following beneficial effect:
1. this aircraft engine cleaning equipment with adjustable through the dislocation rotation adjustment water pipe delivery port size of shower nozzle with rotary joint, can adjust washing pressure and flow as required to make the impact force grow, the cleaning performance is obvious, has improved abluent efficiency greatly.
2. This aircraft engine cleaning equipment with adjustable through the portable power source that can replace at any time, need not the access of external power to improve abluent flexibility, not restricted by the region, be convenient for wash the work anytime and anywhere.
3. This aircraft engine cleaning equipment with adjustable, through the dual spray setting of two mouth shower nozzles, can follow both sides and wash the inner wall fast, improve work efficiency.
Drawings
FIG. 1 is a perspective view of the present invention;
FIG. 2 is a schematic perspective view of a water pipe in the structure of the present invention;
fig. 3 is a schematic perspective view of the internal structure of the sprinkler head of the structure of the present invention.
In the figure: the automatic water injection device comprises a shell 1, wheels 2, a handle 3, a control panel 4, a mobile power supply 5, a water injection hole 6, a water outlet hole 7, a water pipe 8, a rotary joint 9, a spray head 10, a spray head with two nozzles 11, a clamping groove 12, a first dislocation block 13, a second dislocation block 14 and a clamping block 15.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only 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.
Referring to fig. 1-3, an adjustable aircraft engine cleaning device includes a housing 1, the housing 1 is an L-shaped hollow structure, the front and rear side walls of the housing 1 are provided with four wheels 2, the upper end of the right wall of the housing 1 is fixedly provided with a control panel 4, the control panel 4 is an existing structure, which is not described herein, the control panel 4 facilitates a worker to adjust and control water pressure at any time, the right wall of the housing 1 is fixedly provided with a handle 3, the rear end of the upper wall of the housing 1 is provided with a mobile power supply 5, the mobile power supply 5 is an existing structure, which is not described herein, the front end of the upper wall of the housing 1 is provided with a water injection hole 6, the water injection hole 6 is a circular through hole, the lower end of the front wall of the housing 1 is provided with a water outlet hole 7, the water outlet hole 7 is a circular through hole, a water pipe 8 is sleeved inside the water outlet hole 7, and the front end of the water pipe 8 is fixedly provided with a rotary joint 9, the rotary joint 9 is of a circular ring structure, the positions of one sides, away from each other, of the outer circular wall surfaces of the rotary joint 9 are provided with clamping grooves 12, the clamping grooves 12 are arc-shaped grooves, the front end of the inner circular wall surface of the rotary joint 9 is fixedly provided with a first dislocation block 13, the first dislocation block 13 is of a rectangular structure, four first dislocation blocks 13 are provided, the front end of the outer circular wall surface of the rotary joint 9 is provided with a spray head 10, the spray head 10 is of a conical hollow structure, the front side wall surface and the rear side wall surface of the spray head 10 are provided with openings, the front end of the inner circular wall surface of the spray head 10 is provided with an internal thread, the inner circular wall surface of the spray head 10 is provided with two nozzle heads 11, the two nozzle heads 11 are of an existing structure and are not described herein again, the rear ends of the outer circular wall surfaces of the two nozzle heads 11 are provided with external threads, the two nozzle heads 11 are in threaded connection with the spray head 10, the rear end of the inner circular wall surface of the spray head 10 is fixedly provided with a clamping block 15, the clamping block 15 is of a rectangular structure, and two clamping blocks 15 are arranged at positions, the position of the clamping block 15 corresponds to that of the clamping groove 12, the clamping block 15 is clamped with the clamping groove 12, a second dislocation block 14 is fixedly mounted at the rear end of the inner wall surface of the spray head 10, the second dislocation block 14 is of a rectangular structure, and the second dislocation block 14 corresponds to the first dislocation block 13 in a staggered mode.
When using, the rivers pressure has been set up on control panel 4, through shower nozzle 10 and swivel joint 9 dislocation rotation adjustment water pipe delivery port size, can adjust washing pressure and flow as required, thereby make the impact force grow, the cleaning performance is obvious, abluent efficiency has been improved greatly, whole device conveniently removes, and small in size, can work together by a plurality of devices, and the work efficiency is improved, reduce the engineering maintenance time, portable power source 5 of installation in the device can replace at any time, need not the access of external power source, thereby abluent flexibility has been improved, not restricted by the region, be convenient for carry out cleaning work anytime and anywhere, when inside washing in the cleaning process, can install two mouth shower nozzles 11 on shower nozzle 10, two mouth shower nozzles 11's double spray sets up, can follow both sides and wash the inner wall fast, and improve cleaning work efficiency.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. An adjustable aircraft engine washing device, includes shell (1), its characterized in that: the front side wall and the rear side wall of the shell (1) are provided with wheels (2), the upper end of the right wall of the shell (1) is fixedly provided with a control panel (4), the right wall of the shell (1) is fixedly provided with a handle (3), the rear end of the upper wall of the shell (1) is provided with a mobile power supply (5), the front end of the upper wall of the shell (1) is provided with a water injection hole (6), the lower end of the front wall of the shell (1) is provided with a water outlet hole (7), a water pipe (8) is sleeved inside the water outlet hole (7), the front end of the water pipe (8) is fixedly provided with a rotary joint (9), one side positions of the outer circular wall surfaces of the rotary joint (9) far away from each other are provided with clamping grooves (12), the front end of the inner circular wall surface of the rotary joint (9) is fixedly provided with a dislocation block I (13), the front end of the outer circular wall surface of the rotary joint (9) is provided with a spray head (10), and the inner circular wall surface of the spray head (10) is provided with two spray heads (11), a clamping block (15) is fixedly installed at the rear end of the inner circular wall surface of the spray head (10), and a second dislocation block (14) is fixedly installed at the rear end of the inner wall surface of the spray head (10).
2. The adjustable aircraft engine washing apparatus of claim 1, wherein: the water outlet hole (7) is sleeved with the water pipe (8).
3. The adjustable aircraft engine washing apparatus of claim 1, wherein: the number of the first dislocation blocks (13) is four.
4. The adjustable aircraft engine washing apparatus of claim 1, wherein: openings are formed in the front side wall surface and the rear side wall surface of the spray head (10), and internal threads are formed in the front end of the inner circular wall surface of the spray head (10).
5. The adjustable aircraft engine washing apparatus of claim 1, wherein: and external threads are arranged at the rear ends of the excircle wall surfaces of the two nozzles (11), and the two nozzles (11) are in threaded connection with the nozzle (10).
6. The adjustable aircraft engine washing apparatus of claim 1, wherein: the number of the clamping blocks (15) is two, the positions of the clamping blocks (15) correspond to the positions of the clamping grooves (12), and the clamping blocks (15) are clamped with the clamping grooves (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022996946.1U CN215236175U (en) | 2020-12-11 | 2020-12-11 | Adjustable aircraft engine cleaning equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022996946.1U CN215236175U (en) | 2020-12-11 | 2020-12-11 | Adjustable aircraft engine cleaning equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215236175U true CN215236175U (en) | 2021-12-21 |
Family
ID=79452508
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022996946.1U Expired - Fee Related CN215236175U (en) | 2020-12-11 | 2020-12-11 | Adjustable aircraft engine cleaning equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215236175U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115283337A (en) * | 2022-10-08 | 2022-11-04 | 南通爱月机械科技有限公司 | Rotary spraying nozzle for washing |
-
2020
- 2020-12-11 CN CN202022996946.1U patent/CN215236175U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115283337A (en) * | 2022-10-08 | 2022-11-04 | 南通爱月机械科技有限公司 | Rotary spraying nozzle for washing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211221 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |