CN2597335Y - Filter for aircraft clear water car - Google Patents
Filter for aircraft clear water car Download PDFInfo
- Publication number
- CN2597335Y CN2597335Y CNU032230206U CN03223020U CN2597335Y CN 2597335 Y CN2597335 Y CN 2597335Y CN U032230206 U CNU032230206 U CN U032230206U CN 03223020 U CN03223020 U CN 03223020U CN 2597335 Y CN2597335 Y CN 2597335Y
- Authority
- CN
- China
- Prior art keywords
- clear water
- utility
- filter
- model
- urceolus
- 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 - Lifetime
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Abstract
A plane rinsing truck filter is provided, which belongs to a water cleaning and filtering device, in particular to water filter used for the plane rinsing truck. The utility model is characterized in that: the utility model comprises an outer tank, an inner tank, a water discharging pipe and a filtering bag; the inner tank is arranged in the outer tank, the filtering bag is arranged in the inner tank; the water discharging pipe is arranged on the tank wall of the lower part of the outer tank, a filter cover is arranged on the tank body. The utility model is proportionally used with the plane rinsing truck, which can filter the various impurities in tap water used for the plane. The filter part of the utility model has a high filtering precision, can completely reach the drinking water standard; and the filtering bag can be washed and replaced, the replace is convenient and easy. Therefore, the utility model completely ensures the water supply quality for plane with the advantages of safety, economy, reliability and practicality.
Description
Technical field:
The utility model relates to a kind of aircraft clear water car filtering installation, and it belongs to a kind of cleaning and filtering installation of water, particularly a kind of water filtering device that is used on the aircraft clear water car.
Technical background:
The aircraft clear water driving skills art comparative maturity that use at present on the airport, but filtering installation generally all is not set, after such device uses a period of time.Can partly get rusty in solder joint place in the stainless steel water tank, also need every day in addition and clean water tank, if unclean, some impurity will occur in the water tank, influences quality of water supply, do not meet the requirement of health and epidemic prevention supervisory management zone.And clear water filtering installation commonly used is generally fixed mode, and volume is big, complex structure, and incompatibility is installed on the clear water car and uses.Therefore there is the quality of water supply problem all the time in existing clear water car.
Technology contents:
The purpose of this utility model is to provide a kind of aircraft clear water car filtering installation that can guarantee aircraft with water quality.
The purpose of this utility model is achieved in that
A kind of aircraft clear water car filtering installation is characterized in that it comprises urceolus, inner core, outlet conduit and a filter bag; Described inner core places urceolus, and described filter bag places inner core; Described outlet conduit is arranged on the barrel of bottom of described urceolus.
On described cylindrical shell, be provided with a strainer cover.
Described strainer cover is by being bolted to the last end face of urceolus.
Outlet at described outlet conduit is provided with attachment flange.
Between the upper surface of described urceolus and strainer cover, also be provided with packing ring.
Edge in the lower surface of described urceolus is provided with fixedly ear.
The utility model and aircraft clear water car are used, can filter out the various impurity that contained in the tap water that enters aircraft, filtration fraction filtering accuracy height of the present utility model, can reach standard-required fully about drinking-water, and filter bag can clean, and also can change, and it is easily convenient to change, the utility model has guaranteed the quality of water supply of aircraft fully, and has accomplished safe, economical, reliable, economical and practical.
Description of drawings:
Accompanying drawing 1 is a structural representation of the present utility model
Accompanying drawing 2 is the birds-eye view of accompanying drawing 1
Accompanying drawing 3 is the left view of accompanying drawing 1 of the present utility model
The specific embodiment:
Basic comprising of the present utility model comprises a urceolus 2, inner core 3, an outlet conduit 5 and a filter bag 4; Described urceolus 3 places urceolus 2, and described filter bag places inner core 3; Described outlet conduit 5 is arranged on the barrel of bottom of described urceolus 2.Be provided with a strainer cover 1 on described cylindrical shell, water inlet is located on the described strainer cover 1; Described strainer cover 1 is fixed on the last end face of urceolus 2 by bolt 6.In order to guarantee the sealing effectiveness between lid of the present utility model and cylindrical shell, between the upper surface of described urceolus 2 and strainer cover 1, also be provided with packing ring 8.This packing ring 8 is " O " type packing ring.Outlet at described outlet conduit 5 is provided with attachment flange 7, can fix the water pipe that is connected with inlet channel 5 with this flange 7.For the utility model well being fixed on the existing aircraft clear water car, be provided with fixedly ear 9 at the edge of the lower surface 10 of described urceolus 2, can the utility model be fixed by captive nut, dismantle and keep in repair all more convenient like this.Filter bag 4 can be selected existing general-duty water filtration material for use, and changes the filter bag that can not re-use at any time.Can in described filter bag 4, filter core be set.Urceolus of the present utility model and interior bucket can be metallo-s, also can be rigid plastic.
Tap water at first enters in the utility model by the strainer cover 1 that is located on the utility model filtration barrel body, pass through the filtration of filter bag 4 then after, through outlet conduit 5 output.
Claims (7)
1, a kind of aircraft clear water car filtering installation is characterized in that it comprises a urceolus (2), inner core (3), outlet conduit (5) and filter bag (4); Described urceolus (3) places urceolus (2), and described filter bag places inner core (3); Described outlet conduit (5) is arranged on the barrel of bottom of described urceolus (2).
2, the aircraft clear water car filtering installation described in claim 1 is characterized in that being provided with a strainer cover (1) on described cylindrical shell.
3, the aircraft clear water car filtering installation described in claim 2 is characterized in that described strainer cover (1) is fixed on the last end face of urceolus (2) by bolt (6).
4, the aircraft clear water car filtering installation described in claim 1 is characterized in that being provided with attachment flange (7) in the outlet of described outlet conduit (5).
5, the aircraft clear water car filtering installation described in claim 1 is characterized in that also being provided with packing ring (8) between the upper surface of described urceolus (2) and strainer cover (1).
6, the aircraft clear water car filtering installation described in claim 1 is characterized in that being provided with fixedly ear (9) at the edge of the lower surface (10) of described urceolus (2).
7, the aircraft clear water car filtering installation described in claim 1 is characterized in that being provided with filter core in described filter bag (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU032230206U CN2597335Y (en) | 2003-01-17 | 2003-01-17 | Filter for aircraft clear water car |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU032230206U CN2597335Y (en) | 2003-01-17 | 2003-01-17 | Filter for aircraft clear water car |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2597335Y true CN2597335Y (en) | 2004-01-07 |
Family
ID=34162518
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU032230206U Expired - Lifetime CN2597335Y (en) | 2003-01-17 | 2003-01-17 | Filter for aircraft clear water car |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2597335Y (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9376932B2 (en) | 2004-06-14 | 2016-06-28 | Ecoservices, Llc | Turboengine water wash system |
-
2003
- 2003-01-17 CN CNU032230206U patent/CN2597335Y/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9376932B2 (en) | 2004-06-14 | 2016-06-28 | Ecoservices, Llc | Turboengine water wash system |
| US9708928B2 (en) | 2004-06-14 | 2017-07-18 | Ecoservices, Llc | Turboengine water wash system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20090313 Address after: Room 9A, 9 floor, Jin Yun Century Towers, No. 6033, Shennan Road, Futian District, Guangdong, Shenzhen, Che Kung Temple: 518053 Patentee after: Shenzhen Jiajie Technology Development Co. Ltd. Address before: 4, three floor, industrial zone, east of overseas Chinese, Nanshan District, Guangdong, Shenzhen Province, China: 518053 Patentee before: Dahang Science and Technology Co. Ltd., Shenzhen City |
|
| ASS | Succession or assignment of patent right |
Owner name: SHENZHEN CITY JIAJIE SCIENCE DEVELOPMENT CO., LTD. Free format text: FORMER OWNER: SHENZHEN CITY DAHANG SCIENCE CO., LTD. Effective date: 20090313 |
|
| C17 | Cessation of patent right | ||
| CX01 | Expiry of patent term |
Expiration termination date: 20130117 Granted publication date: 20040107 |