CN203199194U - Water tank for airplane sewage car - Google Patents

Water tank for airplane sewage car Download PDF

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Publication number
CN203199194U
CN203199194U CN2013200685921U CN201320068592U CN203199194U CN 203199194 U CN203199194 U CN 203199194U CN 2013200685921 U CN2013200685921 U CN 2013200685921U CN 201320068592 U CN201320068592 U CN 201320068592U CN 203199194 U CN203199194 U CN 203199194U
Authority
CN
China
Prior art keywords
sewage
clear water
aircraft
water
storehouse
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
Application number
CN2013200685921U
Other languages
Chinese (zh)
Inventor
傅新国
张韶伟
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SHANGHAI SHENGHUANG AIRCRAFT GROUND EQUIPMENTS Co
Original Assignee
SHANGHAI SHENGHUANG AIRCRAFT GROUND EQUIPMENTS Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by SHANGHAI SHENGHUANG AIRCRAFT GROUND EQUIPMENTS Co filed Critical SHANGHAI SHENGHUANG AIRCRAFT GROUND EQUIPMENTS Co
Priority to CN2013200685921U priority Critical patent/CN203199194U/en
Application granted granted Critical
Publication of CN203199194U publication Critical patent/CN203199194U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a water tank for an airplane sewage car. The water tank for the airplane sewage car comprises a water tank body fixed on a chassis of the sewage car. The water tank for the airplane sewage car is characterized in that an inner cavity of the water tank body is divided into a clear water bin and a sewage bin through a partition board, a clear water inlet is formed in the top of the clear water bin, a clear water outlet which is communicated with an airplane clear water port through a water pump set and a water pipe is formed in the bottom of the clear water bin, a sewage inlet which is communicated with an airplane sewage draining port through a sewage draining pipe is formed in the top of the sewage bin, and a sewage outlet is formed in the bottom of the sewage bin. The partition board divides the water tank body into the clear water bin and the sewage bin, the two bins are integrated, the occupied space of the water tank body is saved, the clear water bin and the sewage bin can independently work, and therefore airplane sewage can be effectively collected and airplane clear water can be effectively replaced.

Description

A kind of water tank for the aircraft gulley emptier
Technical field
The utility model relates to aircraft gulley emptier apparatus field, particularly a kind of water tank for the aircraft gulley emptier.
Background technology
On the airport, every airplane all can produce the sewage that some need be cleared up after transporting the passenger, needs again simultaneously to replenish clean clear water to the aircraft that continues flight, therefore, need use the vehicle that transports clear water and sewage on the airport.Filtered water tank and the foul water tank of existing gulley emptier are separated, and volume is also bigger, are not suitable for some sanitary accomodation Sewage outlet aspect ratios lower secondary-line-aircraft or blimp, the operation inconvenience.
The utility model content
Technical problem to be solved in the utility model is at the deficiencies in the prior art and defective, provides a kind of Ji Qingshuicang and sewage storehouse in one and can effectively collect aircraft sewage and the water tank of transfer to flight clear water more, to solve the above problems.
The technical matters that the utility model solves can realize by the following technical solutions:
A kind of water tank for the aircraft gulley emptier, comprise the tank box that is fixed on the gulley emptier chassis, it is characterized in that, described tank box inner chamber is divided into clear water storehouse and sewage storehouse by dividing plate, top, described clear water storehouse is provided with the clear water import, bottom, described clear water storehouse is provided with the clear water output that is communicated with the aircraft clean water outlet by water pump assembly and water pipe, and top, described sewage storehouse is provided with the sewage import that is communicated with the aircraft sewage draining exit by blow-off pipe, and bottom, described sewage storehouse is provided with sewage outlet.
In a preferred embodiment of the present utility model, described tank box is that two ends are that semisphere, middle part are columniform goalpost shape casings.
In a preferred embodiment of the present utility model, described clear water storehouse inwall is provided with heat-insulation layer.
In a preferred embodiment of the present utility model, described sewage storehouse inwall is provided with preservative coat.
In a preferred embodiment of the present utility model, described tank box bottom is further fixing by brace panel and gulley emptier chassis.
In a preferred embodiment of the present utility model, described sewage outlet is provided with foul valve, and the blowdown handle of described foul valve extends outside the gulley emptier chassis.
In a preferred embodiment of the present utility model, described clear water storehouse outer wall is provided with liquidometer, and the top is provided with manhole.
In a preferred embodiment of the present utility model, top, described sewage storehouse is provided with ventilation mouth and visor.
Owing to adopted technical scheme as above, dividing plate of the present utility model is divided into clear water storehouse and sewage storehouse with tank box, make two sump integrated, saved the floor area of tank box, work independently of one another in clear water storehouse and sewage storehouse, can effectively collect aircraft sewage and transfer to flight clear water more, the casing of goalpost shape makes the sewage storehouse more thorough when sewage effluent, does not have the draining dead angle.
Description of drawings
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, to do to introduce simply to the accompanying drawing of required use in embodiment or the description of the Prior Art below, apparently, accompanying drawing in describing below only is embodiment more of the present utility model, for those of ordinary skills, under the prerequisite of not paying creative work, can also obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is the structural representation of a kind of specific embodiment of the utility model.
Fig. 2 is the right elevation of Fig. 1.
The specific embodiment
For technological means, creation characteristic that the utility model is realized, reach purpose and effect is easy to understand, below in conjunction with concrete diagram, further set forth the utility model.
Referring to illustrated in figures 1 and 2, a kind of water tank for the aircraft gulley emptier comprises the tank box 100 that is fixed on the gulley emptier chassis 200, for further fixedly tank box 100, bottom at tank box 100 is further fixing by brace panel 123 and gulley emptier chassis 200, tank box 100 inner chambers are divided into clear water storehouse 120 and sewage storehouse 110 by dividing plate 101, tank box 100 is that semisphere, middle part are columniform goalpost shape casings for two ends, and such shape and structure makes clear water storehouse 120 and sewage storehouse 110 not have the draining dead angle.
100 tops, clear water storehouse are provided with clear water import 121, manhole 123, and the bottom is provided with clear water output 122, and clear water output 122 is communicated with the aircraft clean water outlet by water pump assembly and water pipe, provides clean clear water to aircraft; Liquidometer 124 is installed, convenient liquid level of observing 100 inside, clear water storehouse on the outer wall in clear water storehouse 100; Lay heat-insulation layer 125 on the inwall in clear water storehouse 100, guarantee that the clear water in the clear water storehouse 100 are in a normal temperature, when outdoor temperature was low, the clear water temperature that prevents from entering aircraft was crossed low and is caused infringement and the distortion of aircraft water storing bin.
110 tops, sewage storehouse offer sewage import 111, ventilation mouth 113 and observe the visor 114 of sewage storehouse 110 inner cases, be rotary with ventilative cap on the ventilation mouth 113, the periphery of sewage import 111 is thread groove 111a, conveniently be connected with blow-off pipe one end, the other end of blow-off pipe is communicated with the aircraft sewage draining exit, and the sewage on the aircraft is transported to sewage storehouse 110 by blow-off pipe; Bottom, sewage storehouse offers sewage outlet 112, sewage outlet 112 is controlled its keying by a foul valve 112a, the staff opens foul valve 112a for convenience, the blowdown handle 112b of foul valve 112a extends outside the gulley emptier chassis 200, only need downward switching can open foul valve 112a for 90 °, carry out sewage discharge; Be equipped with preservative coat 115 on the inwall in sewage storehouse 110, guarantee that sewage storehouse 110 is not corroded by the corrosive materials in the sewage, increases the service life.
More than show and described groundwork of the present utility model and principal character and advantage of the present utility model.The technical personnel of the industry should be understood; the utility model is not restricted to the described embodiments; that describes in above-described embodiment and the specification sheets just illustrates principle of the present utility model; under the prerequisite that does not break away from the utility model spirit and scope; the utility model also has various changes and modifications, and these changes and improvements all fall in claimed the utility model scope.The claimed scope of the utility model is defined by appending claims and equivalent thereof.

Claims (8)

1. water tank that is used for the aircraft gulley emptier, comprise the tank box that is fixed on the gulley emptier chassis, it is characterized in that, described tank box inner chamber is divided into clear water storehouse and sewage storehouse by dividing plate, top, described clear water storehouse is provided with the clear water import, bottom, described clear water storehouse is provided with the clear water output that is communicated with the aircraft clean water outlet by water pump assembly and water pipe, and top, described sewage storehouse is provided with the sewage import that is communicated with the aircraft sewage draining exit by blow-off pipe, and bottom, described sewage storehouse is provided with sewage outlet.
2. a kind of water tank for the aircraft gulley emptier as claimed in claim 1 is characterized in that, described tank box is that two ends are that semisphere, middle part are columniform goalpost shape casings.
3. a kind of water tank for the aircraft gulley emptier as claimed in claim 1 is characterized in that, described clear water storehouse inwall is provided with heat-insulation layer.
4. a kind of water tank for the aircraft gulley emptier as claimed in claim 1 is characterized in that, described sewage storehouse inwall is provided with preservative coat.
5. as each described a kind of water tank for the aircraft gulley emptier in claim 1 or 2, it is characterized in that described tank box bottom is further fixing by brace panel and gulley emptier chassis.
6. a kind of water tank for the aircraft gulley emptier as claimed in claim 1 is characterized in that described sewage outlet is provided with foul valve, and the blowdown handle of described foul valve extends outside the gulley emptier chassis.
7. a kind of water tank for the aircraft gulley emptier as claimed in claim 1 is characterized in that, described clear water storehouse outer wall is provided with liquidometer, and the top is provided with manhole.
8. a kind of water tank for the aircraft gulley emptier as claimed in claim 1 is characterized in that, top, described sewage storehouse is provided with ventilation mouth and visor.
CN2013200685921U 2013-02-05 2013-02-05 Water tank for airplane sewage car Expired - Fee Related CN203199194U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2013200685921U CN203199194U (en) 2013-02-05 2013-02-05 Water tank for airplane sewage car

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2013200685921U CN203199194U (en) 2013-02-05 2013-02-05 Water tank for airplane sewage car

Publications (1)

Publication Number Publication Date
CN203199194U true CN203199194U (en) 2013-09-18

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN2013200685921U Expired - Fee Related CN203199194U (en) 2013-02-05 2013-02-05 Water tank for airplane sewage car

Country Status (1)

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CN (1) CN203199194U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106985767A (en) * 2017-04-10 2017-07-28 无锡申联专用汽车有限公司 A kind of automobile-used Flexible intumescent binary Integral type water tank
CN109955773A (en) * 2017-12-25 2019-07-02 北方爆破科技有限公司 A kind of used oil recovery vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106985767A (en) * 2017-04-10 2017-07-28 无锡申联专用汽车有限公司 A kind of automobile-used Flexible intumescent binary Integral type water tank
CN109955773A (en) * 2017-12-25 2019-07-02 北方爆破科技有限公司 A kind of used oil recovery vehicle

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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: 20130918

Termination date: 20150205

EXPY Termination of patent right or utility model