CN204817298U - Aviation spare part washing device - Google Patents
Aviation spare part washing device Download PDFInfo
- Publication number
- CN204817298U CN204817298U CN201520572647.1U CN201520572647U CN204817298U CN 204817298 U CN204817298 U CN 204817298U CN 201520572647 U CN201520572647 U CN 201520572647U CN 204817298 U CN204817298 U CN 204817298U
- Authority
- CN
- China
- Prior art keywords
- oil
- fuel tank
- feed
- service sink
- air compressor
- 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 provides an aviation spare part washing device, includes frame (1), washing pond (2), oil feed oil tank (3), and confession oil pipe (35) be connected with oil feed oil tank (3), these oil feed oil tank (3) are connected with air compressor machine (31), wash pond (2) and have an oil drain port (24), and one first oil extraction oil pipe (22) are connected with this oil drain port (24), it has a heating device (21) to wash pond (2), it has one fluid vapourizing unit (33) to supply between oil pipe (35) and oil feed oil tank (3), this vapourizing unit (33) and air compressor machine (31) intercommunication, have one transparent protection casing (4) on wasing pond (2), this protection casing (4) have two handle hole (43), and one rubber gloves (41) are connected respectively in each handle hole (43). Use this kind of washing device, can improve clean efficiency, reduce the petrol use amount simultaneously.
Description
Technical field
The utility model is specifically related to a kind of aviation parts wash mill.
Background technology
The cleaning of aviation zero gasoline is the necessary program of some aerospace partses nursing, but the cleaning efficiency that existing descaling machine comprises blind hole and the less through hole of diameter to parts is not high, not easy to operate.Simple use gasoline cleaning, by the structure of cleaning tool cleaning for structure exquisitenesses such as cleaning counterbore threads, needs large petrol just can clean out.And in the winter time prune job time, because temperature is lower, petrol molecule movement velocity slows down, cleaning parts on deposition oil stain rate reduction, also can improve the use amount of gasoline.
Summary of the invention
The purpose of this utility model is that providing a kind of can use less gasoline, can realize the aviation parts gasoline wash mill of high-efficiency cleaning.
For achieving the above object, the utility model comprises frame, service sink, oil-feed fuel tank, article one, the fuel feed pump be connected with oil-feed fuel tank, this oil-feed fuel tank is connected with air compressor machine, and service sink is with an oil drain out, and a first oil extraction oil pipe is connected with this oil drain out, described service sink is with a heater, have a fluid vapourizing unit between described fuel feed pump and oil-feed fuel tank, described service sink has a transparent shield, this protection is covered with two handle holes and is connected a rubber gloves respectively with each handle hole.
Further, first row oil pipe is connected with one end of an oil filtering device, and this oil filtering device other end is connected with oil return fuel tank, and this oil return fuel tank is connected with oil-feed fuel tank by a check valve.
Further, transparent shield is divided into symmetrical both sides half mask, is slided in frame by the guide rail of bottom side.
Further, the opposed frame contacted of two halves mask is equipped with sealing strip.
To the fluid heating in service sink, can be accelerated the speed that gasoline dissolves spot, reduce gasoline consumption by heater.By arranging vapourizing unit on fuel feed pump, using air compressor machine pressurization, the pressure-air of oil gas and air mixing can be used to clear up the details position of part, as counterbore threads etc., owing to employing pressure-air, can significantly reduce gasoline use amount.Because gasoline is easy to volatilization, suck gasoline gas to reduce popularity, also in order to make gasoline reclaim in the liquefaction of device internal condensation, be provided with protective cover, protection human-body safety, reclaims fluid, also can prevent oil gas from revealing.
Accompanying drawing explanation
Fig. 1 is the utility model schematic diagram.
1, frame, 11, guide rail, 2, service sink, 3, oil-feed fuel tank, 4, protective cover, 21, heater, 22, first row oil pipe, 23, filter, 24, oil drain out, 25, second row oil pipe, 26, oil return fuel tank, 27, check valve, 31, air compressor machine, 33, vapourizing unit, 34, oil gun, 35, fuel feed pump, 41, rubber gloves, 42, sealing strip, 43, handle hole.
Embodiment
Below in conjunction with accompanying drawing, the utility model is described in detail.
As shown in Figure 1, the utility model, comprise frame 1, service sink 2, oil-feed fuel tank 3, the air compressor machine 31 be connected with oil-feed fuel tank 3, the oil drain out 24 be connected with service sink 2 and first row oil pipe 22, and a fuel feed pump 35 be connected with oil-feed fuel tank 3, described service sink 2 is with a heater 21, a fluid vapourizing unit 33 is had between described fuel feed pump 35 and oil-feed fuel tank 3, this vapourizing unit 33 is communicated with air compressor machine 31, described service sink 2 there is a transparent shield 4, this protective cover 4 has two handle holes 43 to be connected a rubber gloves 41 respectively with each handle hole 43.
Wherein, first row oil pipe 22 is connected with one end of an oil filtering device 23, and this oil filtering device 23 other end is connected with oil return fuel tank 26, and this oil return fuel tank 26 is connected with oil-feed fuel tank 3 by a check valve 27.
Wherein, transparent shield 4 is divided into symmetrical both sides half mask, is slided in frame by the guide rail 11 of bottom side.
Wherein, the opposed frame contacted of two halves mask is equipped with sealing strip 42.
Heater to the fluid heating in service sink, can be convenient to cleaning, also can accelerate the speed that gasoline dissolves spot in the winter time.By arranging vapourizing unit on fuel feed pump, being pressurizeed by air compressor machine, the pressure-air of oil gas and air mixing can be used to clear up the details position of part, as counterbore threads etc.The protective cover arranged, can prevent human body from sucking too much gasoline boil-off gas.
Claims (4)
1. an aviation parts wash mill, comprise frame (1), service sink (2), oil-feed fuel tank (3), article one, the fuel feed pump (35) be connected with oil-feed fuel tank (3), this oil-feed fuel tank (3) is connected with air compressor machine (31), service sink (2) is with an oil drain out (24), article one, the first oil extraction oil pipe (22) is connected with this oil drain out (24), it is characterized in that, described service sink (2) is with a heater (21), a fluid vapourizing unit (33) is had between described fuel feed pump (35) and oil-feed fuel tank (3), this vapourizing unit (33) is communicated with air compressor machine (31), described service sink (2) there is a transparent shield (4), this protective cover (4) has two handle holes (43), each handle hole (43) connects a rubber gloves (41) respectively.
2. a kind of aviation parts wash mill according to claim 1, it is characterized in that, described first row oil pipe (22) is connected with one end of an oil filtering device (23), this oil filtering device (23) other end is connected with oil return fuel tank (26), and this oil return fuel tank (26) is connected with oil-feed fuel tank (3) by a check valve (27).
3. a kind of aviation parts wash mill according to claim 1, is characterized in that, described transparent shield (4) is divided into symmetrical both sides half mask, is slided in frame by the guide rail (11) of bottom side.
4. a kind of aviation parts wash mill according to claim 3, is characterized in that, the opposed frame contacted of described two halves mask is equipped with sealing strip (42).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520572647.1U CN204817298U (en) | 2015-07-31 | 2015-07-31 | Aviation spare part washing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520572647.1U CN204817298U (en) | 2015-07-31 | 2015-07-31 | Aviation spare part washing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204817298U true CN204817298U (en) | 2015-12-02 |
Family
ID=54674940
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520572647.1U Expired - Fee Related CN204817298U (en) | 2015-07-31 | 2015-07-31 | Aviation spare part washing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204817298U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114871996A (en) * | 2022-05-06 | 2022-08-09 | 中国矿业大学 | Hydraulic circuit dismounting and mounting working platform capable of preventing oil from splashing |
-
2015
- 2015-07-31 CN CN201520572647.1U patent/CN204817298U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114871996A (en) * | 2022-05-06 | 2022-08-09 | 中国矿业大学 | Hydraulic circuit dismounting and mounting working platform capable of preventing oil from splashing |
| CN114871996B (en) * | 2022-05-06 | 2023-12-12 | 中国矿业大学 | Hydraulic circuit dismounting working platform capable of preventing oil from splashing |
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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: 20151202 Termination date: 20160731 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |