CN2592584Y - Tail lifting mechanism of sewage vehicle for aircraft - Google Patents

Tail lifting mechanism of sewage vehicle for aircraft Download PDF

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Publication number
CN2592584Y
CN2592584Y CN 02293114 CN02293114U CN2592584Y CN 2592584 Y CN2592584 Y CN 2592584Y CN 02293114 CN02293114 CN 02293114 CN 02293114 U CN02293114 U CN 02293114U CN 2592584 Y CN2592584 Y CN 2592584Y
Authority
CN
China
Prior art keywords
inner frame
slide block
frame
water tank
outside
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
CN 02293114
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Chinese (zh)
Inventor
唐永伟
尤志宏
钱元齐
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.)
Wuxi Ximei Special Automobiles Co ltd
Original Assignee
Wuxi Ximei Special Automobiles Co ltd
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 Wuxi Ximei Special Automobiles Co ltd filed Critical Wuxi Ximei Special Automobiles Co ltd
Priority to CN 02293114 priority Critical patent/CN2592584Y/en
Application granted granted Critical
Publication of CN2592584Y publication Critical patent/CN2592584Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model belongs to a novel conveyance, particularly a sewage vehicle which is especially used for airfields. The utility model has the main technical proposal that an inner frame which can lift and lower is arranged in an outer frame; a lower fulcrum of a lifting and lowering oil cylinder is connected with the bottom of the outer frame; a piston rod of the lifting and lowering oil cylinder is connected with the upper part of the inner frame; a slide block which can lift and lower is arranged in the inner frame; the slide block is connected with the upper part of the inner frame through a driving belt; the upper part of the inner frame is provided with a chain wheel; one end of the driving belt is connected with the upper part of the lifting and lowering oil cylinder, and the other end of the driving belt is connected with the slide block; a slide slot is arranged on the inside of the outer frame; the outside of the inner frame is provided with a rolling wheel; the inner frame is embedded in the slide slot through the rolling wheel and is arranged in the outer frame. After the device is used, the utility model is capable of enlarging range of use of the sewage vehicle and improves stability of the whole device.

Description

The afterbody lifting mechanism of aircraft gulley emptier
Technical field
The utility model belongs to a kind of transportation means, refers in particular to a kind of gulley emptier that is exclusively used in the airport.
Background technology
In the air transportation process, need the sewage of aircraft bus attendant and passenger's generation be removed on the airport, for some large-scale transport airliners, the airport has special-purpose gulley emptier usually and transports these sewage, for some small-sized feeder liner, the device that does not also have at present to be suitable for is carried sewage, and this has brought sizable difficulty for the sewage disposal of branch line blimp.In addition, existing gulley emptier is because the problem of structure design still can not satisfy operating needs on stability.
Summary of the invention
The purpose of this utility model is to design a kind of afterbody lifting mechanism of aircraft gulley emptier, enlarging the range of use of gulley emptier, and improves the stability of whole device.
Its main technical schemes be in outside frame, be provided with can lifting inner frame, the lower fulcrum of hoist cylinder is connected with the bottom of outside frame, the piston rod of hoist cylinder is connected with inner frame top, in inner frame, be provided with can lifting slide block, slide block utilizes driving band to be connected with the top of inner frame.
Sprocket wheel is installed on top at inner frame, and an end of driving band is connected with the top of hoist cylinder, and the other end is connected with slide block.
Inboard at outside frame is provided with chute, in the outside of inner frame roller is installed, and inner frame utilizes roller to embed chute, is installed in the outside frame.
Inboard at inner frame is provided with chute, in the outside of slide block roller is installed, and slide block utilizes roller to embed chute, is installed in the inner frame.
Outside frame is installed on the chassis of gulley emptier, connects workplatform and little foul water tank on slide block.
Afterbody pedal, step are set on workplatform, foul valve and dirt inlet are set on little foul water tank.
Big foul water tank is installed on the chassis, wheel is set below the chassis, operator's compartment is set, foul valve and water inlet and hydraulic efficiency pressure system are set, dirt inlet is set on the top of big foul water tank in the bottom of big foul water tank in the front portion on chassis.
The utility model has the advantages that because lifting frame has comprised little foul water tank, workplatform, make a cover mechanism have lifting platform and receive two kinds of functions of sewage, thereby both can be used for the sewage disposal of airliner, can be used for the sewage disposal of air minibus again, improve the range of use of whole device, made things convenient for the sewage disposal work of various passenger planes; Secondly, this device utilizes internal and external frame formula structure and cooperating of slide block to realize lifting, and texture ratio is more reasonable, and especially stability better.
Description of drawings
Fig. 1 is an elevator composition of the present utility model.
Fig. 2 is the left view of Fig. 1.
Fig. 3 is the gulley emptier constructional drawing.
Fig. 4 is the part birds-eye view on right side among Fig. 3.
The specific embodiment
As shown in the figure: in whole lifting frame 4, be provided with in the outside frame 18 can lifting inner frame 17, the lower fulcrum of hoist cylinder 19 is connected with the bottom of outside frame 18, the piston rod of hoist cylinder 19 is connected with inner frame 17 tops, in inner frame 17, be provided with can lifting slide block 20, slide block 20 utilizes driving band 16 to be connected with the top of inner frame 17.
Sprocket wheel 22 is installed on top at inner frame 17, and an end of driving band 16 is connected with the top of hoist cylinder 19, and the other end is connected with slide block 20.When inner frame 17 stretched lifting because of hoist cylinder 19, chain 16 can drag slide block 20 up-and-down movements.
Inboard at outside frame 18 is provided with chute, in the outside of inner frame 17 roller is installed, and inner frame 17 utilizes roller to embed chute, is installed in the outside frame 18.Under the effect of hoist cylinder, inner frame 17 utilize its roller can be in the inboard chutes that are provided with of outside frame 18 up-and-down movement.
Inboard at inner frame 17 is provided with chute, in the outside of slide block 20 roller is installed, and slide block 20 utilizes roller to embed chute, is installed in the inner frame 17.Among Fig. 1 23 is the crossbeam on outside frame 18 tops, and 15 among Fig. 3 is illuminating lamp.
Outside frame 18 is installed on the chassis 24 of gulley emptier, connects workplatform 11 and little foul water tank 6 on slide block 20.During the slide block up-and-down movement, can drive little foul water tank up-and-down movement, so that transport the sewage on large-scale or the air minibus.
Afterbody pedal 14, step 13 and platform guardrail 5 are set on workplatform 11, so that the staff operates up and down, foul valve 10 and dirt inlet 12 are set on little foul water tank 6, sewage on the blimp enters in the foul water tank through dirt inlet 12, when gulley emptier ran to the appointed place, sewage was got rid of through foul valve again.
Big foul water tank 2 is installed on chassis 24, wheel 25 is set below chassis 24,24 front portion is provided with operator's compartment 1 on the chassis, and foul valve 7 and water inlet 9 and hydraulic efficiency pressure system 8 are set in the bottom of big foul water tank 2, on the top of big foul water tank 2 dirt inlet 3 is set.Big foul water tank is used to handle the sewage of airliner.The front portion of big foul water tank 2 is a filtered water tank, and the rear portion is used to hold sewage, and filtered water tank is used for the clear water of use in the splendid attire supply aircraft toilet, and its rear portion is used to receive the dirt in the aircraft toilet.
During installation, the outside frame 18 of lifting frame 4 is fixed on the car chassis 24, inner frame 17 is installed in the groove of outside frame 18 inboards by the side direction roller, slide block 20 utilizes the side direction roller of itself to be installed in the groove of inner frame 17 inboards again, the lower fulcrum of oil cylinder 19 is fixed on the bottom of outside frame 18, fulcrum is fixed on the top of inner frame 17 on it, driving band 16 can be a chain 16, one end of chain 16 is fixed on the slide block 20, after the other end is walked around sprocket wheel 22 on the inner frame 17, be fixed on the oil cylinder 19, when oil cylinder 19 liftings, inner frame 17 is also done corresponding action, and the sprocket wheel 22 of chain 16 on inner frame 17 moves, drive slide block 20 liftings, slide block 20 drives workplatform 11 up-and-down movements again.
When work, when the big-and-middle-sized aircraft of vehicle service, promote workplatform 11 to aircraft required service height, when the vehicle service blimp, fall workplatform to the bottom surface of little foul water tank 6 and land.Make a covering device be applicable to two kinds of types, enlarged the range of use of device, handled easily.
Little foul water tank 6 has reception, holds, the function of sewage effluent, and workplatform 11 is welded on the last plane of little foul water tank 6, erecting stage guardrail 5 on workplatform 11.Afterbody pedal 14 is welded at the trailing flank of little foul water tank 6.

Claims (7)

1, the afterbody lifting mechanism of aircraft gulley emptier, it is characterized in that in outside frame (18), being provided with can lifting inner frame (17), the lower fulcrum of hoist cylinder (19) is connected with the bottom of outside frame (18), the piston rod of hoist cylinder (19) is connected with inner frame (17) top, in inner frame (17), be provided with can lifting slide block (20), slide block (20) utilizes driving band (16) to be connected with the top of inner frame (17).
2, mechanism according to claim 1 is characterized in that on the top of inner frame (17) sprocket wheel (22) being installed, and an end of driving band (16) is connected with the top of hoist cylinder (19), and the other end is connected with slide block (20).
3, mechanism according to claim 1 is characterized in that in the inboard of outside frame (18) chute being set, and in the outside of inner frame (17) roller is installed, and inner frame (17) utilizes roller to embed chute, is installed in the outside frame (18).
4, mechanism according to claim 1 is characterized in that in the inboard of inner frame (17) chute being set, and in the outside of slide block (20) roller is installed, and slide block (20) utilizes roller to embed chute, is installed in the inner frame (17).
5, mechanism according to claim 1 is characterized in that outside frame (18) is installed on the chassis (24) of gulley emptier, goes up at slide block (20) to connect workplatform (11) and little foul water tank (6).
6, mechanism according to claim 5 is characterized in that afterbody pedal (14), step (13) are set on workplatform (11), and foul valve (10) and dirt inlet (12) are set on little foul water tank (6).
7, mechanism according to claim 5, it is characterized in that (24) go up installation big foul water tank (2) on the chassis, below chassis (24), wheel is set, the front portion of (24) is provided with operator's compartment (1) on the chassis, foul valve (7) and water inlet (9) and hydraulic efficiency pressure system (8) are set in the bottom of big foul water tank (2), dirt inlet (3) are set on the top of big foul water tank (2).
CN 02293114 2002-12-28 2002-12-28 Tail lifting mechanism of sewage vehicle for aircraft Expired - Fee Related CN2592584Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 02293114 CN2592584Y (en) 2002-12-28 2002-12-28 Tail lifting mechanism of sewage vehicle for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 02293114 CN2592584Y (en) 2002-12-28 2002-12-28 Tail lifting mechanism of sewage vehicle for aircraft

Publications (1)

Publication Number Publication Date
CN2592584Y true CN2592584Y (en) 2003-12-17

Family

ID=33751209

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 02293114 Expired - Fee Related CN2592584Y (en) 2002-12-28 2002-12-28 Tail lifting mechanism of sewage vehicle for aircraft

Country Status (1)

Country Link
CN (1) CN2592584Y (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104150133A (en) * 2014-07-31 2014-11-19 丹阳市亚力车业有限公司 Lifting support of motor sweeper

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104150133A (en) * 2014-07-31 2014-11-19 丹阳市亚力车业有限公司 Lifting support of motor sweeper
CN104150133B (en) * 2014-07-31 2016-01-20 丹阳市亚力车业有限公司 A kind of pickup sweeper lifting support

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20031217

Termination date: 20111228