CN205217459U - Aircraft engine ground belt cleaning device - Google Patents
Aircraft engine ground belt cleaning device Download PDFInfo
- Publication number
- CN205217459U CN205217459U CN201521000770.2U CN201521000770U CN205217459U CN 205217459 U CN205217459 U CN 205217459U CN 201521000770 U CN201521000770 U CN 201521000770U CN 205217459 U CN205217459 U CN 205217459U
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- CN
- China
- Prior art keywords
- valve
- water tank
- cleaning device
- fluid reservoir
- air accumulator
- 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
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Abstract
The utility model discloses an aircraft engine ground belt cleaning device relates to belt cleaning device technical field. An aircraft engine ground belt cleaning device, includes that the bottom sets up the moving platform of gyro wheel, moving platform's intermediate position setting pushes away the handle, the last one side tie pushing away the handle of moving platform is lain and is set up the gas holder, upright places water storage tank and liquid storage pot at the opposite side that pushes away the handle, the gas holder connects the outlet duct to lead to to water storage tank and liquid storage pot respectively, set up two one logical operating valves between gas holder and water storage tank and liquid storage pot, water storage tank and liquid storage pot all set up special purpose interface matched with water storage tank outlet pipe and the liquid storage pot outlet pipe that has with the aircraft, set up the gas holder manometer between gas supply valve and gas holder, set up the washing jar manometer of sharing between liquid storage pot and water storage tank. The utility model aims to solve the technical problem that an aircraft engine ground belt cleaning device for cleaning it is effectual is provided.
Description
Technical field
The utility model relates to cleaning device technical field, especially relates to a kind of airplane engines ground cleaning device.
Background technology
After each working flight of aircraft (mainly helicopter) terminates, its engine interior will clean, and engine has Special cleaning mouth, during internal washing, and in the press-in of its cleaning fluid band can be with easy access.This cleaning device is domestic to be produced without specialized factory, and the main import equipment that relies on meets its requirement.Therefore the cleaning device designing a kind of effectively clean aircraft engine is very necessary.
Utility model content
Technical problem to be solved in the utility model there is provided the good airplane engines ground cleaning device of a kind of cleaning effect.
For achieving the above object, the utility model provides following technical scheme: a kind of airplane engines ground cleaning device, and comprise the mobile platform that bottom arranges roller, the centre position of described mobile platform arranges push handle; Described mobile platform lies low in the side of push handle air accumulator is set, uprightly place water tank and fluid reservoir at the opposite side of push handle; Described air accumulator picks out tracheae and passes to water tank and fluid reservoir respectively, described air accumulator and arrange two one logical operating valves between water tank and fluid reservoir; Described water tank and fluid reservoir all arrange the water tank outlet pipe and fluid reservoir outlet pipe that the special purpose interface that has with aircraft matches, and on described fluid reservoir outlet pipe, the clean valve of configuration, described water tank outlet pipe configures rinsing valve; The air inlet pipe that described air accumulator has arranges steam supply valve, escape pipe arranges vent valve; Between described steam supply valve and air accumulator, air tank pressure gauge is set; Shared purge tank Pressure gauge is set between described fluid reservoir and water tank.Multiple tank body mounts by the utility model can carry out Multifunction washing to aircraft engine in identical platform simultaneously.In addition at air accumulator and arrange two one logical operating valves between water tank and fluid reservoir, can washed and rinsing aircraft engine by clean valve and arranging of rinsing valve, ensure not remaining cleaning solution in the aircraft engine after washing, ensure that the performance of aircraft engine.Between steam supply valve and air accumulator, air tank pressure gauge is set; Shared purge tank Pressure gauge is set between fluid reservoir and water tank and can ensures that the utility model carries out the adjustment of relevant pressure in washing process, avoid causing the wasting of resources.
Preferably, described air accumulator arrange pressure regulator and configure safety valve.Safety valve can to prevent in air accumulator unsafe factor in a high voltage state, ensure that the personal safety of operating personnel.
Preferably, between air accumulator and pressure regulator, internal-thread spherical valve is set.Internal-thread spherical valve flow resistance is little, and structure is simple, and volume is little, lightweight, easy to operate, and opening and closing is rapid, is convenient to remote control.Repair conveniently, sealing ring is all generally movable simultaneously, and dismounting and change is convenient.In addition when internal-thread spherical valve standard-sized sheet or full cut-off, the sealing surface of spheroid and valve seat and medium are isolated, and medium is by causing the erosion of valve sealing face.
Preferably, the check valve of one-way conduction water tank is set between pressure regulator and water tank, and configures internal thread switching ball valve.Arranging of check valve can avoid the water in water tank to reflux.
Preferably, described water tank outlet pipe arranges filter in the lower end of clean valve.Can ensure that the water that water tank passes in aircraft engine cleans by arranging filter, avoiding causing secondary pollution.
Preferably, described clean valve is internal-thread spherical valve.Internal-thread spherical valve flow resistance is little, and structure is simple, and volume is little, lightweight, easy to operate, and opening and closing is rapid, is convenient to remote control.Repair conveniently, sealing ring is all generally movable simultaneously, and dismounting and change is convenient.In addition when internal-thread spherical valve standard-sized sheet or full cut-off, the sealing surface of spheroid and valve seat and medium are isolated, and medium is by causing the erosion of valve sealing face.
Preferably, at least one group, the roller of described mobile platform is stopping wheel.By arranging stopping wheel, can ensure that mobile platform keeps inactive state in the course of the work, handled easily human users.
The invention also discloses a kind of using method of airplane engines ground cleaning device, comprise the steps:
1) the mixing cleaning agent in fluid reservoir needed for loading; Liquid needed for loading in water tank;
2) close gas storage cover, open check valve; Two one logical operating valves are opened to mixing position, opens steam supply valve air feed;
3) regulate pressure regulator to required stirring pressure, close vent valve after 2 minutes, by exert pressure in air accumulator to maximum pressure 0.86MPa;
4) open to pressing position by two one logical operating valves, adjustment pressure regulator is to required pressure;
5) open clean valve, the mixing cleaning agent in injection fluid reservoir, to engine, closes clean valve;
6) rinsing: A. closes steam supply valve; B. rinsing valve is opened; C. open water tank lid, add about 1 gallons water; D. close water tank lid and water tank vent valve, open steam supply valve; E. open clean valve, close when empty in tank; F. close steam supply valve, open air bleeding valve.
Repeatedly clean by using airplane engines ground cleaning device of the present utility model to realize, rinsing, effectively can clean aircraft engine.
Accompanying drawing explanation
Fig. 1 is the structural representation of a kind of airplane engines ground cleaning device of the utility model;
Fig. 2 is the A-A view of the structural representation of a kind of airplane engines ground cleaning device of the utility model;
Fig. 3 is the structural representation of a kind of airplane engines ground cleaning device of the utility model;
Fig. 4 is the logic chart of a kind of airplane engines ground cleaning device of the utility model;
Wherein, 1. mobile platform, 2. push handle, 3. air accumulator, 4. water tank, 5. fluid reservoir, 6. roller, 7. two one logical operating valve, 8. water tank outlet pipe, 9. fluid reservoir outlet pipes, 10. clean valve, 11. rinsing valves, 12. air inlet pipe, 13. escape pipes, 14. steam supply valves, 15. vent valves, 16. air tank pressure gauge, 17. purge tank Pressure gauges, 18. pressure regulators, 19. safety valves, 20. internal-thread spherical valves, 21. check valves, 22. filters, 23. internal threads switch ball valves.
Detailed description of the invention
In order to deepen understanding of the present utility model, below in conjunction with embodiment and accompanying drawing, the utility model is described in further detail, and this embodiment, only for explaining the utility model, does not form the restriction to the utility model protection domain.
Describe preferred embodiment of the present utility model in detail below in conjunction with accompanying drawing 1-4: a kind of airplane engines ground cleaning device, comprise the mobile platform 1 that bottom arranges roller, the centre position of described mobile platform 1 arranges push handle 2; Described mobile platform 1 lies low in the side of push handle 2 air accumulator 3 is set, uprightly place water tank 4 and fluid reservoir 5 at the opposite side of push handle; Described air accumulator 3 picks out tracheae 6 and passes to water tank 4 and fluid reservoir 5 respectively, described air accumulator 3 and arrange two one logical operating valves 7 between water tank 4 and fluid reservoir 5; Described water tank 4 and fluid reservoir 5 all arrange the water tank outlet pipe 8 and fluid reservoir outlet pipe 9 that match with the special purpose interface that aircraft has, and on described fluid reservoir outlet pipe 9, the clean valve 10 of configuration, described water tank outlet pipe 8 configures rinsing valve 11; The air inlet pipe 12 that described air accumulator 3 has arranges steam supply valve 14, escape pipe 13 is arranged vent valve 15; Between described steam supply valve 14 and air accumulator 3, air tank pressure gauge 16 is set; Between described fluid reservoir 5 and water tank 4, shared purge tank Pressure gauge 17 is set.Multiple tank body mounts by the utility model can carry out Multifunction washing to aircraft engine in identical platform simultaneously.In addition at air accumulator 3 and arrange two one logical operating valves 7 between water tank 4 and fluid reservoir 5, can washed and rinsing aircraft engine by clean valve 10 and arranging of rinsing valve 11, ensure not remaining cleaning solution in the aircraft engine after washing, ensure that the performance of aircraft engine.Air tank pressure gauge 16 is set between steam supply valve 14 and air accumulator 3; Shared purge tank Pressure gauge 17 is set between fluid reservoir 5 and water tank 4 and can ensures that the utility model carries out the adjustment of relevant pressure in washing process, avoid causing the wasting of resources.
Preferably, described air accumulator 3 arrange pressure regulator 18 and configure safety valve 19.Safety valve 19 can to prevent in air accumulator 3 unsafe factor in a high voltage state, ensure that the personal safety of operating personnel.
Preferably, between air accumulator 3 and pressure regulator 18, internal-thread spherical valve 20 is set.Internal-thread spherical valve 20 flow resistance is little, and structure is simple, and volume is little, lightweight, easy to operate, and opening and closing is rapid, is convenient to remote control.Repair conveniently, the sealing ring of internal-thread spherical valve 20 is all generally movable simultaneously, and dismounting and change is convenient.In addition when internal-thread spherical valve 20 standard-sized sheet or full cut-off, the sealing surface of spheroid and valve seat and medium are isolated, and medium is by causing the erosion of valve sealing face.
In the utility model, the check valve 21 of one-way conduction water tank is set between pressure regulator 18 and water tank 4, and configures internal thread switching ball valve 23.Arranging of check valve 18 can avoid the water in water tank to reflux.
Water tank outlet pipe 8 can also arrange filter 22 in the lower end of clean valve 11 in addition.Can ensure that the water that water tank 4 passes in aircraft engine cleans by arranging filter 22, avoiding causing secondary pollution.
Preferably, the clean valve 10 in the utility model is internal-thread spherical valve 20.Internal-thread spherical valve 20 flow resistance is little, and structure is simple, and volume is little, lightweight, easy to operate, and opening and closing is rapid, is convenient to remote control.Repair conveniently, sealing ring is all generally movable simultaneously, and dismounting and change is convenient.In addition when internal-thread spherical valve 20 standard-sized sheet or full cut-off, the sealing surface of spheroid and valve seat and medium are isolated, and medium is by causing the erosion of valve sealing face.
In the utility model, at least one group of the roller 24 of mobile platform 1 is stopping wheel.By arranging stopping wheel, can ensure that mobile platform 1 keeps inactive state in the course of the work, handled easily human users.
The invention also discloses a kind of using method of airplane engines ground cleaning device, comprise the steps:
1) the mixing cleaning agent in fluid reservoir 5 needed for loading; Liquid needed for loading in water tank 4;
2) close air accumulator 3 to cover, open check valve 21; Two one logical operating valves 7 are opened to mixing position, opens steam supply valve 14 air feed;
3) regulate pressure regulator 18 to required stirring pressure, close vent valve 15 after 2 minutes, by exert pressure in air accumulator 3 to maximum pressure 0.86MPa;
4) open to pressing position by two one logical operating valves 7, adjustment pressure regulator 18 is to required pressure;
5) open clean valve 10, the mixing cleaning agent in injection fluid reservoir 5, to engine, closes clean valve 10;
6) rinsing: A. closes steam supply valve 14; B. rinsing valve 11 is opened; C. open water tank 4 lid, add about 1 gallons water; D. close water tank 4 lid and water tank vent valve 15, open steam supply valve 14; E. open clean valve 10, close when empty in water tank tank; F. close steam supply valve 14, open air bleeding valve 15.
Repeatedly clean by using airplane engines ground cleaning device of the present utility model to realize, rinsing, effectively can clean aircraft engine.
Above-described is only preferred embodiment of the present utility model; it should be pointed out that for the person of ordinary skill of the art, under the prerequisite not departing from the utility model creation design; can also make some distortion and improvement, these all belong to protection domain of the present utility model.
Claims (7)
1. an airplane engines ground cleaning device, comprises the mobile platform that bottom arranges roller, it is characterized in that: the centre position of described mobile platform arranges push handle; Described mobile platform lies low in the side of push handle air accumulator is set, uprightly place water tank and fluid reservoir at the opposite side of push handle; Described air accumulator picks out tracheae and passes to water tank and fluid reservoir respectively, described air accumulator and arrange two one logical operating valves between water tank and fluid reservoir; Described water tank and fluid reservoir all arrange the water tank outlet pipe and fluid reservoir outlet pipe that the special purpose interface that has with aircraft matches, and on described fluid reservoir outlet pipe, the clean valve of configuration, described water tank outlet pipe configures rinsing valve; The air inlet pipe that described air accumulator has arranges steam supply valve, escape pipe arranges vent valve; Between described steam supply valve and air accumulator, air tank pressure gauge is set; Shared purge tank Pressure gauge is set between described fluid reservoir and water tank.
2. airplane engines ground cleaning device according to claim 1, is characterized in that: described air accumulator arranges pressure regulator and configures safety valve.
3. airplane engines ground cleaning device according to claim 2, is characterized in that: arrange internal-thread spherical valve between air accumulator and pressure regulator.
4. airplane engines ground cleaning device according to claim 3, is characterized in that: the check valve arranging one-way conduction water tank between pressure regulator and water tank, and configures internal thread switching ball valve.
5. the airplane engines ground cleaning device according to the arbitrary claim of claim 1-4, is characterized in that: described water tank outlet pipe arranges filter in the lower end of clean valve.
6. airplane engines ground cleaning device according to claim 5, is characterized in that: described clean valve is internal-thread spherical valve.
7. airplane engines ground cleaning device according to claim 1, is characterized in that: at least one group, the roller of described mobile platform is stopping wheel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521000770.2U CN205217459U (en) | 2015-12-07 | 2015-12-07 | Aircraft engine ground belt cleaning device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521000770.2U CN205217459U (en) | 2015-12-07 | 2015-12-07 | Aircraft engine ground belt cleaning device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205217459U true CN205217459U (en) | 2016-05-11 |
Family
ID=55892555
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521000770.2U Expired - Fee Related CN205217459U (en) | 2015-12-07 | 2015-12-07 | Aircraft engine ground belt cleaning device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205217459U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105363717A (en) * | 2015-12-07 | 2016-03-02 | 上海打捞局芜湖潜水装备厂 | Aircraft engine ground cleaning device and application method thereof |
-
2015
- 2015-12-07 CN CN201521000770.2U patent/CN205217459U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105363717A (en) * | 2015-12-07 | 2016-03-02 | 上海打捞局芜湖潜水装备厂 | Aircraft engine ground cleaning device and application method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160511 Termination date: 20181207 |