CN201292015Y - Integrated airplane service ground well - Google Patents
Integrated airplane service ground well Download PDFInfo
- Publication number
- CN201292015Y CN201292015Y CNU2008201406915U CN200820140691U CN201292015Y CN 201292015 Y CN201292015 Y CN 201292015Y CN U2008201406915 U CNU2008201406915 U CN U2008201406915U CN 200820140691 U CN200820140691 U CN 200820140691U CN 201292015 Y CN201292015 Y CN 201292015Y
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- CN
- China
- Prior art keywords
- lifting
- pulley
- well
- take
- main driving
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- 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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- 230000005540 biological transmission Effects 0.000 claims abstract description 50
- 238000007789 sealing Methods 0.000 claims description 15
- 238000012423 maintenance Methods 0.000 claims description 5
- 239000000725 suspension Substances 0.000 claims description 4
- 238000005299 abrasion Methods 0.000 abstract 1
- FGRBYDKOBBBPOI-UHFFFAOYSA-N 10,10-dioxo-2-[4-(N-phenylanilino)phenyl]thioxanthen-9-one Chemical compound O=C1c2ccccc2S(=O)(=O)c2ccc(cc12)-c1ccc(cc1)N(c1ccccc1)c1ccccc1 FGRBYDKOBBBPOI-UHFFFAOYSA-N 0.000 description 2
- 239000000428 dust Substances 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000011067 equilibration Methods 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 210000001138 tear Anatomy 0.000 description 1
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- General Details Of Gearings (AREA)
Abstract
The utility model discloses an integrated airplane service ground well; a lifting tank body is arranged on a tank body frame; a guiding wheel and lifting pulleys are arranged on the tank body frame; the tank body frame is limited on a lifting slide rail through the guiding wheel; a transmission mechanism comprises a transmission motor, a main transmission shaft driven by the transmission motor; two take-up pulleys are arranged on the main transmission shaft; transmission ropes are fixedly connected with the take-up pulleys; the transmission rope on the take-up pulley on one side of the main transmission shaft passes through the lifting pulley arranged on one side of the tank body frame and is fixed on the well body; the transmission rope on the take-up pulley on the other side of the main transmission shaft passes through the lifting pulley arranged on the other side of the tank body frame and is fixed on the well body. The integrated airplane service ground well adopts integrated structure design, is convenient and simple in opening and closing, has compact structure and greatly reduces potential fault points; meanwhile, the transmission mechanism also adopts integrated structure and can sufficiently lubricate rotary parts in transmission case, and reduce abrasion and noise generated by transmission, so as to improve the service life of equipments.
Description
Technical field
The utility model relates to a kind of airport and supplies with the guarantee final terminal, relates in particular to a kind of integrated form aircraft duties ground well that is used for airport hardstand, comprehensive maintenance hangar.
Background technology
Existing aircraft duties ground well comprises manual ground well, automatic ground well and full automaticity ground well.China Patent No. " 200620035796.5 " provides a kind of " semi-automatic lifting formula aircraft duties ground well ", comprise well body and the well lid that cooperates with the well body, also comprise jacking system and counter weight device, jacking system comprise the guide rail that is provided with in the well body, with the guide rail bearing fit and the slide rail of captiveing joint with well lid, counter weight device comprises that the sliding rope of two pulleys being provided with on the slide rail, two pulley rooms goes up that be provided with and the clump weight well lid weight-matched, slide rail be provided with preceding operating surface that electric elements are installed and with the cooresponding back of preceding operating surface operating surface.China Patent No. " 200520035441.1 " provides a kind of " full automaticity aircraft duties ground well ", comprise glass-felt plastic cylindrical shell, working box, jacking system, well lid, jacking system is a spindle gear, place in the cylindrical shell, comprise upper end and working box bottom bonded assembly screw mandrel, driving screw mandrel motor rotating; Motor is installed on the frame, and working box is supported by screw mandrel, and periphery is by rack-mounted support bar column equilibration guiding.
Adopt the S. A. ground well or the full automaticity ground well of said structure mainly to have the following disadvantages: one, the S. A. ground well adopts counterweight block structure, and well lid is very heavy, opens and close extremely inconvenient, sometimes be difficult to open, when work finishes, when closing well lid, the staff requires great effort inefficiency.Two, the lifting device structure in S. A. ground well and the full automaticity ground well disperses, and potential faults point is many, has potential safety hazard, causes aircraft duties ground well often can not normally use because break down when work.Three, each rotary part can't lubricate in the jacking system in S. A. ground well and the full automaticity ground well, and easily laying dust weares and teares greatly, and service life is short.Four, big in the jacking system in S. A. ground well and the full automaticity ground well owing to wearing and tearing, cause noise big, influence staff's operation.
The utility model content
The purpose of this utility model is to overcome the problems referred to above that the transmission jacking system in the existing aircraft duties ground well exists, and a kind of integrated form aircraft duties ground well is provided.The utility model adopts the integrated structure design, open and close simple and convenient, compact conformation, significantly reduced the potential faults point, transmission device also adopts integrated structure, can reduce wearing and tearing to each rotary part sufficient lubrication in the transmission gearbox, reduce the noise that transmission brings simultaneously, improved service life of equipment.
For achieving the above object, the technical solution adopted in the utility model is as follows:
A kind of integrated form aircraft duties ground well, comprise the well body, well lid, transmission device, lifting casing and lifting sliding rail, it is characterized in that: described lifting casing is arranged on the box frame, box frame is provided with track adjusting wheel and lifting pulley, box frame is spacing on lifting sliding rail by track adjusting wheel, described transmission device comprises driving motor and the main driving axle that is driven by driving motor, main driving axle is provided with two take-up pulleies, be fixedly connected with transmission rope on the take-up pulley, be fixed on the well body behind the lifting pulley of transmission rope on the take-up pulley of main driving axle one side, be fixed on the well body behind the lifting pulley of the transmission rope on the take-up pulley of main driving axle opposite side by the setting of box frame opposite side by box frame one side setting.
Described transmission device also comprises the sealing box body, it is external that driving motor is arranged on seal box, main driving axle passes the sealing box body, and the main driving axle in the sealing box body is provided with the gear driving pair that cooperates with driving motor, and take-up pulley is arranged on the external both sides main driving axle of seal box.
Described transmission device also comprises counter drive shaft, and described counter drive shaft is provided with and driving motor bonded assembly retarder and the pinion that cooperates with gear driving pair on the main driving axle.
Also be provided with power-transfer clutch on the described counter drive shaft, described power-transfer clutch is arranged between retarder and the pinion.
Described lifting sliding rail is four, is separately fixed on the well body wall, and the track adjusting wheel on every lifting sliding rail is two.
Described lifting pulley is four, is separately positioned on four angles of box frame bottom, and the transmission rope of main driving axle one side cooperates with two lifting pulleys of box frame one side.
Described transmission rope is fixed on the suspension ring of well body wall after by lifting pulley.
Also be provided with access cover on the described well body for maintenance usefulness.
Adopt advantage of the present utility model to be:
One, in the utility model, the lifting casing is arranged on the box frame, box frame is provided with track adjusting wheel and lifting pulley, box frame is spacing on lifting sliding rail by track adjusting wheel, transmission device comprises driving motor and the main driving axle that is driven by driving motor, main driving axle is provided with two take-up pulleies, be fixedly connected with transmission rope on the take-up pulley, be fixed on the well body behind the lifting pulley of transmission rope on the take-up pulley of main driving axle one side by box frame one side setting, be fixed on the well body behind the lifting pulley of transmission rope on the take-up pulley of main driving axle opposite side by the setting of box frame opposite side, integrated structure is all adopted in lifting and transmission, lifting is steadily reliable, need not manual operation, noise is less during lifting.
Two, the utility model is compared with the S. A. ground well of employing counterweight block structure, and no clump weight has reduced well lid weight, conveniently opens and closes, and when work finished, the staff closed well lid, high efficiency easily.
Three, the utility model is compared with the jacking system in the full automaticity ground well with the S. A. ground well, and running part adopts centralized configuration, and compact conformation has reduced the potential faults point, has reduced potential safety hazard, has safeguarded the normal use of aircraft duties ground wells.
Four, the utility model is compared with the jacking system in the full automaticity ground well with the S. A. ground well, adopt integrated structure, gear driving pair, pinion, retarder are arranged in the sealing box body, solved the problem of laying dust, at the sealing lubricating oil of annotating in the box body, reduce wearing and tearing, improved the service life of equipment.
Five, the utility model is compared with the jacking system in the full automaticity ground well with the S. A. ground well, owing to reduced wearing and tearing, thus reduced noise, be beneficial to staff's operation.
Six, the track adjusting wheel on every lifting sliding rail of the utility model is two, and spacing fixing more reliable, lifting is more steady.
Seven, also be provided with on the utility model well body for the access cover that overhauls usefulness, easy access is safeguarded.
Description of drawings
Fig. 1 is the utility model master TV structure scheme drawing
Fig. 2 is the utility model side-looking structural representation
Fig. 3 is the utility model transmission device structural representation
Be labeled as among the figure: 1, well body, 2, well lid, 3, the lifting casing, 4, lifting sliding rail, 5, box frame, 6, track adjusting wheel, 7, lifting pulley, 8, driving motor, 9, main driving axle, 10, take-up pulley, 11, sealing box body, 12, gear driving pair, 13, counter drive shaft, 14, retarder, 15, pinion, 16, power-transfer clutch, 17, suspension ring, 18, access cover, 19, the cable rewinding machine structure.
The specific embodiment
A kind of integrated form aircraft duties ground well, comprise well body 1, well lid 2, transmission device, lifting casing 3 and lifting sliding rail 4, lifting casing 3 is arranged on the box frame 5, box frame 5 is provided with track adjusting wheel 6 and lifting pulley 7, box frame 5 is spacing on lifting sliding rail 4 by track adjusting wheel 6, described transmission device comprises driving motor 8 and the main driving axle 9 that is driven by driving motor 8, main driving axle 9 is provided with two take-up pulleies 10, be fixedly connected with transmission rope on the take-up pulley 10, be fixed on the well body 1 behind the lifting pulley 7 of transmission rope on the take-up pulley of main driving axle 9 one sides by box frame 5 one side settings, be fixed on the well body 1 behind the lifting pulley 7 of the transmission rope on the take-up pulley 10 of main driving axle 9 opposite sides by box frame 5 opposite side settings.
In the utility model, transmission device also comprises sealing box body 11, driving motor 8 is arranged on outside the sealing box body 11, main driving axle 9 passes sealing box body 11, main driving axle in the sealing box body 11 is provided with the gear driving pair 12 that cooperates with driving motor 8, and take-up pulley 10 is arranged on the both sides main driving axle that seals outside the box body 11.In addition, transmission device also comprises counter drive shaft 13, is being provided with on the counter drive shaft 13 and driving motor 8 bonded assembly retarders 14 and the pinion 15 that cooperates with gear driving pair 12 on the main driving axle 9.And also be provided with power-transfer clutch 16 on counter drive shaft 13, described power-transfer clutch 16 is arranged between retarder 14 and the pinion 15.Lifting sliding rail 4 is set to four, and every length is about 1300mm, is provided with two on well body 1 left wall, is provided with two on well body 1 right wall, and the track adjusting wheel on every lifting sliding rail 4 is two.Lifting pulley is four, is separately positioned on four angles of box frame 5 bottoms, and the transmission rope of main driving axle 9 one sides cooperates with two lifting pulleys of box frame 5 one sides.Transmission rope is fixed on the suspension ring 17 of well body wall after by lifting pulley.On the well body, also be provided with access cover 18 for maintenance usefulness.
Aircraft duties ground well is mainly used to provide the maintenance service to the various aircrafts in the hangar or on the hardstand.In well body 1, be provided with cable rewinding machine structure 19, cable on the cable rewinding machine structure 19 is connected with lifting casing 3, during 3 liftings of lifting casing, driving motor 8 passes to power-transfer clutch 16 after slowing down by one group of turbine worm retarder that is arranged on the counter drive shaft 13, after the power-transfer clutch output, driving main driving axle 9 by one group of pinion again rotates, the take-up pulley 10 at two ends, main driving axle 9 left and right sides is connected with main driving axle 9 rigidity simultaneously, take-up pulley 10 and then main driving axle 9 rotates, make with the lifting pulley 7 bonded assembly steel cables of lifting casing 3 and on take-up pulley 10, receive or put, by track adjusting wheel 6, lifting casing 3 is moved up and down on lifting sliding rail 4, thereby realized the liter of lifting casing 3 or fall.
Obviously; those of ordinary skill in the art is according to technological know-how of being grasped and customary means; according to above said content, can also make the various ways that does not break away from the utility model basic fundamental thought, these pro forma conversion are all within protection domain of the present utility model.
Claims (8)
1, a kind of integrated form aircraft duties ground well, comprise well body (1), well lid (2), transmission device, lifting casing (3) and lifting sliding rail (4), it is characterized in that: described lifting casing (3) is arranged on the box frame (5), box frame (5) is provided with track adjusting wheel (6) and lifting pulley (7), box frame (5) is spacing on lifting sliding rail (4) by track adjusting wheel (6), described transmission device comprises driving motor (8) and the main driving axle (9) that is driven by driving motor (8), main driving axle (9) is provided with two take-up pulleies (10), take-up pulley is fixedly connected with transmission rope on (10), be fixed on the well body (1) behind the lifting pulley of transmission rope on the take-up pulley of main driving axle (9) one sides, be fixed on the well body (1) behind the lifting pulley of transmission rope on the take-up pulley of main driving axle (9) opposite side by the setting of box frame opposite side by box frame one side setting.
2, integrated form aircraft duties ground well according to claim 1, it is characterized in that: described transmission device also comprises sealing box body (11), driving motor (8) is arranged on outside the sealing box body (11), main driving axle (9) passes sealing box body (11), main driving axle in the sealing box body (11) is provided with the gear driving pair (12) that cooperates with driving motor (8), and take-up pulley (10) is arranged on the outer both sides main driving axle of sealing box body (11).
3, integrated form aircraft duties ground well according to claim 2, it is characterized in that: described transmission device also comprises counter drive shaft (13), and described counter drive shaft (13) is provided with and driving motor (8) bonded assembly retarder (14) and the pinion (15) that cooperates with gear driving pair (12) on the main driving axle (9).
4, integrated form aircraft duties ground well according to claim 3 is characterized in that: also be provided with power-transfer clutch (16) on the described counter drive shaft (13), described power-transfer clutch (16) is arranged between retarder (14) and the pinion (15).
5, according to claim 1,2,3 or 4 described integrated form aircraft duties ground wells, it is characterized in that: described lifting sliding rail (4) is four, is separately fixed on the well body wall, and the track adjusting wheel (6) on the every lifting sliding rail (4) is two.
6, according to claim 1,2,3 or 4 described integrated form aircraft duties ground wells, it is characterized in that: described lifting pulley (7) is four, be separately positioned on four angles of box frame (5) bottom, the transmission rope of main driving axle (9) one sides cooperates with two lifting pulleys (7) of box frame (5) one sides.
7, according to claim 1,2,3 or 4 described integrated form aircraft duties ground wells, it is characterized in that: described transmission rope is fixed on the suspension ring (17) of well body wall after by lifting pulley (7).
8, according to claim 1,2,3 or 4 described integrated form aircraft duties ground wells, it is characterized in that: also be provided with access cover (18) on the described well body (1) for maintenance usefulness.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201406915U CN201292015Y (en) | 2008-10-14 | 2008-10-14 | Integrated airplane service ground well |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201406915U CN201292015Y (en) | 2008-10-14 | 2008-10-14 | Integrated airplane service ground well |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201292015Y true CN201292015Y (en) | 2009-08-19 |
Family
ID=41005481
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008201406915U Expired - Lifetime CN201292015Y (en) | 2008-10-14 | 2008-10-14 | Integrated airplane service ground well |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201292015Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102285461A (en) * | 2011-05-24 | 2011-12-21 | 成都克伏特航空设备有限公司 | Full-automatic lifting integrated airplane service ground well |
| CN109703775A (en) * | 2019-02-15 | 2019-05-03 | 成都克伏特航空设备有限公司 | Fatigue duty ground well is renovated in purely mechanic lifting |
-
2008
- 2008-10-14 CN CNU2008201406915U patent/CN201292015Y/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102285461A (en) * | 2011-05-24 | 2011-12-21 | 成都克伏特航空设备有限公司 | Full-automatic lifting integrated airplane service ground well |
| CN102285461B (en) * | 2011-05-24 | 2014-02-19 | 成都克伏特航空设备有限公司 | Fully automatic lifting integrated aircraft service pit |
| CN109703775A (en) * | 2019-02-15 | 2019-05-03 | 成都克伏特航空设备有限公司 | Fatigue duty ground well is renovated in purely mechanic lifting |
| CN109703775B (en) * | 2019-02-15 | 2024-05-24 | 成都克伏特航空设备有限公司 | Purely mechanical lifting flip service ground well |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: CHEN DEZHANG Free format text: FORMER OWNER: HUANG JUNFU Effective date: 20090724 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20090724 Address after: Sichuan city of Chengdu province Chenghua District East sanhuan Longtan Industrial circle round 1 Pfister Enterprise Building No. 6, zip code: 610052 Patentee after: Chen Dezhang Address before: Department of science and technology, Mianyang Vocational and Technical College, Sichuan, Mianyang 621000, China Patentee before: Huang Junfu |
|
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20090819 |