CN204789238U - Airspace engine cleanliness factor detecting system - Google Patents
Airspace engine cleanliness factor detecting system Download PDFInfo
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- CN204789238U CN204789238U CN201520484798.1U CN201520484798U CN204789238U CN 204789238 U CN204789238 U CN 204789238U CN 201520484798 U CN201520484798 U CN 201520484798U CN 204789238 U CN204789238 U CN 204789238U
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Abstract
The utility model discloses an airspace engine cleanliness factor detecting system, including supplying liquid device, circulating device and two particle counter, supply the export of liquid device to connect the entry of airspace engine, the export of airspace engine to connect circulating device's entry, circulating device's export connects the entry that supplies the liquid device, a particle counter connects the sample connection of airspace engine entrance, and the 2nd particle counter connects the sample connection in airspace engine exit. The utility model discloses it is convenient to detect, and the security is good, can improve the cleaning efficiency, improves space flight engine wash's cleanliness factor.
Description
[technical field]
The utility model relates to airspace engine cleaning, particularly relates to a kind of airspace engine cleanliness factor detection system.
[background technology]
There is very high requirement airspace engine inside to cleanliness factor, needs to clean with absolute ethyl alcohol, the past in assembling process, and people and manual method use absolute ethyl alcohol to clean airspace engine, and detect its cleanliness factor.Absolute ethyl alcohol is inflammable, volatile dangerous chemical.Tool pungency, the steam of absolute ethyl alcohol and air can form explosive mixture, comparatively large to personal injury, manual cleaning inefficiency, danger coefficient are higher.
[summary of the invention]
The technical problems to be solved in the utility model is to provide a kind of easy to detect, and security is good, can improve the airspace engine cleanliness factor detection system of cleaning efficiency.
In order to solve the problems of the technologies described above, the technical solution adopted in the utility model is, a kind of airspace engine cleanliness factor detection system, comprise liquid feed device, circulating device and two corpuscular counters, the entrance that outlet connects the entrance of airspace engine, the outlet of airspace engine connects circulating device of liquid feed device, the outlet of circulating device connects the entrance of liquid feed device; First corpuscular counter connects the sample tap of airspace engine porch, and the second corpuscular counter connects the sample tap in airspace engine exit.
Above-described airspace engine cleanliness factor detection system, liquid feed device comprises liquid case, liquid pump, ratio adjusting valve, stop valve, filtrator and main valve, the entrance of liquid pump connects liquid case, liquid delivery side of pump connects ratio adjusting valve, filter is taken in the outlet of ratio adjusting valve, and the outlet of filtrator connects the entrance of airspace engine by main valve; The sample tap of the first corpuscular counter is between the outlet and main valve of filtrator.
Above-described airspace engine cleanliness factor detection system, circulating device comprises Ethylene recov case and ebullator, and the outlet of airspace engine connects Ethylene recov case, and the entrance of ebullator connects Ethylene recov case, and circulation delivery side of pump connects liquid case.
Above-described airspace engine cleanliness factor detection system, comprises detection main frame, and the sampled signal output terminal of the first corpuscular counter and the second corpuscular counter connects detection main frame respectively.
The utility model airspace engine cleanliness factor detection system is easy to detect, and security is good, can improve cleaning efficiency, improves the cleanliness factor of airspace engine cleaning.
[accompanying drawing explanation]
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.
Fig. 1 is the structured flowchart of the utility model embodiment airspace engine cleanliness factor detection system.
[embodiment]
As shown in Figure 1, airspace engine cleanliness factor detection system, comprises liquid feed device, circulating device, detection main frame (not shown) and two corpuscular counters to the structure of the utility model embodiment airspace engine cleanliness factor detection system.
The entrance that outlet connects the entrance of airspace engine, the outlet of airspace engine connects circulating device of liquid feed device, the outlet of circulating device connects the entrance of liquid feed device.First corpuscular counter connects the sample tap of airspace engine porch, and the second corpuscular counter connects the sample tap in airspace engine exit.The sampled signal output terminal of the first corpuscular counter and the second corpuscular counter connects detection main frame respectively.
Wherein, liquid feed device provides stable hydraulic power supply to the cleaning of airspace engine, carries out cleaning with pressure to the inner chamber of airspace engine and inner-walls of duct.Liquid feed device comprises liquid case, liquid pump, ratio adjusting valve, stop valve, filtrator and main valve, the entrance of liquid pump connects liquid case, liquid delivery side of pump connects ratio adjusting valve, and filter is taken in the outlet of ratio adjusting valve, and the outlet of filtrator connects the entrance of airspace engine by main valve.The sample tap of the first corpuscular counter is between the outlet and main valve of filtrator.
The absolute ethyl alcohol of cleaned airspace engine from Ethylene recov case pump liquid-return box, is realized the recycling of cleansing medium absolute ethyl alcohol by circulating device, reduces cleaning cost.Circulating device comprises Ethylene recov case and ebullator, and the outlet of airspace engine connects Ethylene recov case, and the entrance of ebullator connects Ethylene recov case, and circulation delivery side of pump connects liquid case.
Corpuscular counter adopts the particle detector of German import, in the cleaning process of airspace engine, both the granularity of the absolute ethyl alcohol before entering airspace engine can have been monitored at any time, also on-line monitoring granularity can be carried out to when cleaning airspace engine from its internal washing absolute ethyl alcohol out, the granule detecting data of absolute ethyl alcohol can be obtained real-time, judge the cleanliness factor that airspace engine is cleaned, complete the cleaning to airspace engine fast and efficiently, reach the requirement of cleaning code.
Claims (4)
1. an airspace engine cleanliness factor detection system, it is characterized in that, comprise liquid feed device, circulating device and two corpuscular counters, the entrance that outlet connects the entrance of airspace engine, the outlet of airspace engine connects circulating device of liquid feed device, the outlet of circulating device connects the entrance of liquid feed device; First corpuscular counter connects the sample tap of airspace engine porch, and the second corpuscular counter connects the sample tap in airspace engine exit.
2. airspace engine cleanliness factor detection system according to claim 1, it is characterized in that, liquid feed device comprises liquid case, liquid pump, ratio adjusting valve, stop valve, filtrator and main valve, the entrance of liquid pump connects liquid case, liquid delivery side of pump connects ratio adjusting valve, filter is taken in the outlet of ratio adjusting valve, and the outlet of filtrator connects the entrance of airspace engine by main valve; The sample tap of the first corpuscular counter is between the outlet and main valve of filtrator.
3. airspace engine cleanliness factor detection system according to claim 2, it is characterized in that, circulating device comprises Ethylene recov case and ebullator, and the outlet of airspace engine connects Ethylene recov case, and the entrance of ebullator connects Ethylene recov case, and circulation delivery side of pump connects liquid case.
4. airspace engine cleanliness factor detection system according to claim 1, is characterized in that, comprise detection main frame, and the sampled signal output terminal of the first corpuscular counter and the second corpuscular counter connects detection main frame respectively.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201520484798.1U CN204789238U (en) | 2015-07-07 | 2015-07-07 | Airspace engine cleanliness factor detecting system |
Applications Claiming Priority (1)
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CN201520484798.1U CN204789238U (en) | 2015-07-07 | 2015-07-07 | Airspace engine cleanliness factor detecting system |
Publications (1)
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CN204789238U true CN204789238U (en) | 2015-11-18 |
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Family Applications (1)
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CN201520484798.1U Expired - Fee Related CN204789238U (en) | 2015-07-07 | 2015-07-07 | Airspace engine cleanliness factor detecting system |
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CN (1) | CN204789238U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106841010A (en) * | 2016-12-30 | 2017-06-13 | 陕西彩虹电子玻璃有限公司 | Cleanliness factor measurement apparatus and method in a kind of cover-plate glass annealing of substrates stove |
CN109865717A (en) * | 2017-12-01 | 2019-06-11 | 北京蓝星清洗有限公司 | The cleaning device and method of hydraulic oil pipe |
-
2015
- 2015-07-07 CN CN201520484798.1U patent/CN204789238U/en not_active Expired - Fee Related
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106841010A (en) * | 2016-12-30 | 2017-06-13 | 陕西彩虹电子玻璃有限公司 | Cleanliness factor measurement apparatus and method in a kind of cover-plate glass annealing of substrates stove |
CN109865717A (en) * | 2017-12-01 | 2019-06-11 | 北京蓝星清洗有限公司 | The cleaning device and method of hydraulic oil pipe |
CN109865717B (en) * | 2017-12-01 | 2020-06-16 | 北京蓝星清洗有限公司 | Cleaning device and method for hydraulic oil pipe |
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Legal Events
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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: 20151118 Termination date: 20200707 |
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CF01 | Termination of patent right due to non-payment of annual fee |