CN202358308U - Airplane ground hydraulic multifunctional device - Google Patents
Airplane ground hydraulic multifunctional device Download PDFInfo
- Publication number
- CN202358308U CN202358308U CN201120496527XU CN201120496527U CN202358308U CN 202358308 U CN202358308 U CN 202358308U CN 201120496527X U CN201120496527X U CN 201120496527XU CN 201120496527 U CN201120496527 U CN 201120496527U CN 202358308 U CN202358308 U CN 202358308U
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- Prior art keywords
- car body
- hydraulic
- control panel
- aircraft floor
- hydraulic device
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- Expired - Fee Related
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Abstract
The utility model discloses an airplane ground hydraulic multifunctional device, which comprises a vehicle body, a hydraulic system, a control panel and a high pressure hose, wherein the hydraulic system is arranged inside the vehicle body, the control panel is arranged on the surface of the vehicle body, and the high pressure hose is connected with the vehicle body. Compared with the prior art, the airplane ground hydraulic multifunctional provided by the utility model has the advantages that the three functions of testing, filling and cleaning are integrated, and the defects in the prior art can be effectively overcome.
Description
Technical field
The utility model relates to the corollary equipment field of aircraft floor hydraulic pressure, exactly is meant a kind of aircraft floor multifunctional hydraulic device.
Background technology
At present, existing aircraft floor hydraulic efficiency pressure system is the oil-feed port return opening to be connected with aircraft through high pressure hose through being fixed on ground-surface large-scale pumping source, and this large-scale pumping source comprises and is fixed on ground-surface three phase alternating current motor; Plunger pump; Fuel tank, cooling system and complicated valve control system, in this system, the driven by motor plunger pump supplies to hydraulic oil on the aircraft; Regulate desired parameters through valve control system, utilize tap water to circulate and realize heat radiation system.The major defect of existing aircraft floor hydraulic efficiency pressure system is following:
Realize to be fixed on ground-surface pumping plant form that 1, need measured piece pulled down to transport between special-purpose test during test and operate, maneuvering performance be poor, is inappropriate at the scene aircraft is tested.
2, the fixed type pumping plant is disposable has high input, and floor area is big, and dismounting is constant, not easy care.
3, the division of labor is clearer and more definite, and function ratio is more single, can carry out the function that does not possess hydraulic-oil filling of pressure parameter test; Can the annotate function that does not possess cleaning of hydraulic pressure.
The utility model content
To above-mentioned defective, the technical matters that the utility model solves is to provide a kind of aircraft floor multifunctional hydraulic device, will test, annotate, clean three kinds of integrated and one of function, can solve the shortcoming of prior art effectively.
In order to solve above technical matters; The aircraft floor multifunctional hydraulic device that the utility model provides; Comprise car body, hydraulic efficiency pressure system, control panel and high pressure hose; Said hydraulic efficiency pressure system is installed in the inside of said car body, and said control panel is arranged on the surface of said car body, and said high pressure hose is connected with said car body.
Preferably, the bottom of said car body is provided with roller.
Preferably, said control panel is arranged on the place ahead of said car body.
Preferably, said hydraulic efficiency pressure system comprises alternating current dynamo-plunger pump, hydraulic pressure valve control system, electric control operation system, pipeline system and detection alarm system.
Preferably, said hydraulic efficiency pressure system is provided with quick coupling.
The aircraft floor multifunctional hydraulic device that the utility model provides; Comprise car body, hydraulic efficiency pressure system, control panel and high pressure hose; Said hydraulic efficiency pressure system is installed in the inside of said car body, and said control panel is arranged on the surface of said car body, and said high pressure hose is connected with said car body.Compared with prior art, three kinds of integrated and one of function will be tested, annotated, clean to the aircraft floor multifunctional hydraulic device that the utility model provides, and can solve the shortcoming of prior art effectively.
Description of drawings
Fig. 1 is the structured flowchart of aircraft floor multifunctional hydraulic device in the utility model.
The specific embodiment
For the technical scheme that those skilled in the art can understand the utility model better and provided, set forth below in conjunction with specific embodiment.
See also Fig. 1, this figure is the structured flowchart of aircraft floor multifunctional hydraulic device in the utility model.
The aircraft floor multifunctional hydraulic device that the utility model provides comprises car body 1, hydraulic efficiency pressure system, control panel 2 and high pressure hose, and hydraulic efficiency pressure system is installed in the inside of car body 1, and control panel 2 is arranged on the surface of car body 1, and high pressure hose is connected with car body 1.The bottom of car body 1 is provided with roller 3, and car body is convenient to move, and maneuvering performance is good.
Hydraulic efficiency pressure system comprises alternating current dynamo-plunger pump, hydraulic pressure valve control system, electric control operation system, pipeline system and detection alarm system; Hydraulic efficiency pressure system is provided with quick coupling, can carry out hydraulic efficiency pressure system test, hydraulic efficiency pressure system hydraulic-oil filling and hydraulic efficiency pressure system to aircraft in interior outfield and clean.
Control panel is arranged on the place ahead of car body.Cleaning or oiling work when carrying out; Only need opening power on control panel, press and clean or the oiling button carries out different functions and selects, simultaneously can the adjustment pressure adjusting knob; The pilot piping oil pressure; Regulate the flow regulating knob, the Control work flow cleans the oiling technological requirement to reach to meet.The digital temperature telltale is installed on the control panel, is intuitively understood the pipeline temperature, installed the digital pressure telltale simultaneously additional, the digital flow telltale, the indication of reporting to the police is polluted in the liquid level warning indication, and is simple to operate, comes into plain view.
Compared with prior art, three kinds of integrated and one of function will be tested, annotated, clean to the aircraft floor multifunctional hydraulic device that the utility model provides, and can solve the shortcoming of prior art effectively.
To the above-mentioned explanation of the disclosed embodiments, make this area professional and technical personnel can realize or use the utility model.Multiple modification to these embodiment will be conspicuous concerning those skilled in the art, and defined General Principle can realize under the situation of spirit that does not break away from the utility model or scope in other embodiments among this paper.Therefore, the utility model will can not be restricted to these embodiment shown in this paper, but will meet and principle disclosed herein and features of novelty the wideest corresponding to scope.
Claims (5)
1. aircraft floor multifunctional hydraulic device; It is characterized in that comprise car body, hydraulic efficiency pressure system, control panel and high pressure hose, said hydraulic efficiency pressure system is installed in the inside of said car body; Said control panel is arranged on the surface of said car body, and said high pressure hose is connected with said car body.
2. aircraft floor multifunctional hydraulic device according to claim 1 is characterized in that the bottom of said car body is provided with roller.
3. aircraft floor multifunctional hydraulic device according to claim 1 is characterized in that said control panel is arranged on the place ahead of said car body.
4. aircraft floor multifunctional hydraulic device according to claim 1 is characterized in that said hydraulic efficiency pressure system comprises alternating current dynamo-plunger pump, hydraulic pressure valve control system, electric control operation system, pipeline system and detection alarm system.
5. aircraft floor multifunctional hydraulic device according to claim 1 is characterized in that said hydraulic efficiency pressure system is provided with quick coupling.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201120496527XU CN202358308U (en) | 2011-12-02 | 2011-12-02 | Airplane ground hydraulic multifunctional device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201120496527XU CN202358308U (en) | 2011-12-02 | 2011-12-02 | Airplane ground hydraulic multifunctional device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202358308U true CN202358308U (en) | 2012-08-01 |
Family
ID=46569515
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201120496527XU Expired - Fee Related CN202358308U (en) | 2011-12-02 | 2011-12-02 | Airplane ground hydraulic multifunctional device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202358308U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104859863A (en) * | 2015-05-06 | 2015-08-26 | 桂林长海发展有限责任公司 | Support equipment for aircraft maintenance |
-
2011
- 2011-12-02 CN CN201120496527XU patent/CN202358308U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104859863A (en) * | 2015-05-06 | 2015-08-26 | 桂林长海发展有限责任公司 | Support equipment for aircraft maintenance |
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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 |
Granted publication date: 20120801 Termination date: 20151202 |
|
| EXPY | Termination of patent right or utility model |