CN202333706U - Inverted-type automatic cable pay-off and take-up device of aircraft service ground well - Google Patents

Inverted-type automatic cable pay-off and take-up device of aircraft service ground well Download PDF

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Publication number
CN202333706U
CN202333706U CN2011204327391U CN201120432739U CN202333706U CN 202333706 U CN202333706 U CN 202333706U CN 2011204327391 U CN2011204327391 U CN 2011204327391U CN 201120432739 U CN201120432739 U CN 201120432739U CN 202333706 U CN202333706 U CN 202333706U
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CN
China
Prior art keywords
cable tube
take
retractable cable
transmission
shaft
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Active
Application number
CN2011204327391U
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Chinese (zh)
Inventor
陈德章
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.)
CHENGDU GRAFT AVIATION EQUIPMENT Co Ltd
Original Assignee
CHENGDU GRAFT AVIATION EQUIPMENT 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.)
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Application filed by CHENGDU GRAFT AVIATION EQUIPMENT Co Ltd filed Critical CHENGDU GRAFT AVIATION EQUIPMENT Co Ltd
Priority to CN2011204327391U priority Critical patent/CN202333706U/en
Application granted granted Critical
Publication of CN202333706U publication Critical patent/CN202333706U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses an inverted-type automatic cable pay-off and take-up device of an aircraft service ground well, which comprises a rack, a transmission mechanism and a pay-off and take-up wire bobbin for paying off and taking up wire cables, wherein the pay-off and take-up wire bobbin is longitudinally arranged on the rack, and is provided with a guide groove ring matched with the wire cables; the transmission mechanism comprises a transmission motor, a speed reducer, a conical gear, a driving shaft, an electromagnetic clutch and a driven shaft; the speed reducer is arranged on the transmission shaft of the transmission motor; the transmission shaft of the transmission motor is connected with the driving shaft through the conical gear; the driving shaft is connected with the driven shaft through the electromagnetic clutch; and the driven shaft and the pay-off and take-up wire bobbin are connected fixedly so as to drive the pay-off and take-up wire bobbin to move. According to the utility model, electromagnetic absorption and separated transmission is adopted, obvious transmission component abrasion does not exist, the transmission is more reliable, also the structure is compact, the applied force is good, and the take-up space is saved.

Description

Aircraft duties ground well flip-over type cable automatic deploying and retracting line apparatus
Technical field
The utility model relates to a kind of cable conveying equipment, relates in particular to a kind of aircraft duties ground well flip-over type cable automatic deploying and retracting line apparatus that is used for airline and airport hardstand, maintenance hangar and aircraft factory.
Background technology
At present, each airline and airport hardstand, maintenance hangar and aircraft factory power supply, hydraulic power source, oil sources are had relatively high expectations to conveying equipment when remote the conveying.In conveying equipment, also there is more problem in existing Winder, can't coiling, manage and power up etc. be united two into one, and moving body does not adopt the fluid pressure type trailer yet in addition, loads, promotes inconvenient.The coiling dial rotation is dumb, has the blocked portion problem, has reduced transporting velocity; Maximum winding length is shorter, has reduced operating efficiency; Motor is intake easily, causes Winder not use, and car body moves inconvenience etc.
In order to address the above problem; Chinese patent number " 200820064457.9 " has proposed the electronic friction-type take-up mechanism of a kind of aircraft duties ground well; The applying date is on July 29th, 2008; Open day is on May 6th, 2009, comprises drive unit and take-up pulley, and drive unit comprises drive motors, the driven wheel that is connected with drive motors and the friction pulley that is cooperated with take-up pulley by the driven wheel drive; Said take-up pulley is provided with the take-up groove that cooperates with cable, and the take-up groove is shape distribution in the shape of a spiral on take-up pulley, is provided with the carbon brush slip-ring that is connected with cable in the take-up pulley.But in practical application, but have following problem: one, adopt frictional drive, friction pulley is as driving wheel; Take-up reel is as driven pulley, and because of friction pulley can only be the picture rubber tire, and take-up reel is the steel wheel; In the course of the work, the friction pulley quick abrasion causes transmission unreliable; The friction pulley replacement cycle is extremely short, makes the shortening in useful life of whole take-up mechanism.Two, electronic friction-type take-up mechanism is loosely organized, and installing space is excessive, causes the volume of whole ground well to increase.Three, take-up groove shape distribution in the shape of a spiral, because of no moulds of industrial equipment guarantee, complex manufacturing technology, the making precision is low.
Summary of the invention
The purpose of the utility model is to overcome the problems referred to above that existing aviation exists with drawing cable; A kind of aircraft duties ground well flip-over type cable automatic deploying and retracting line apparatus is provided, and the utility model adopts the transmission of electromagnetism suction type, does not have tangible drive disk assembly wearing and tearing; Transmission is more reliable; And compact conformation, and stressed good, practice thrift the take-up space.
For realizing above-mentioned purpose, the technical scheme that the utility model adopts is following:
A kind of aircraft duties ground well flip-over type cable automatic deploying and retracting line apparatus; Comprise frame, it is characterized in that: also comprise transmission mechanism and the retractable cable tube that is used for the folding and unfolding cable, said retractable cable tube vertically is arranged on the frame; The retractable cable tube is provided with the gathering sill circle that cooperates with cable; Said transmission mechanism comprises driving motor, decelerator, conical gear, driving shaft, electromagnetic clutch and driven shaft, and said decelerator is arranged on the power transmission shaft of driving motor, and the power transmission shaft of driving motor is connected with driving shaft through conical gear; Driving shaft is connected with driven shaft through electromagnetic clutch, and driven shaft is fixedly connected with the retractable cable tube and drives the motion of retractable cable tube.
Said frame is provided with conical bearing, and conical bearing is positioned at retractable cable tube top and bottom, and driven shaft one end is connected with the conical bearing of retractable cable tube upper end, and the center that the other end passes the retractable cable tube is connected with the conical bearing of lower end.
Also be provided with on the said frame with the retractable cable tube and cooperate the spacing limiting component in the gathering sill circle of cable.
Said limiting component is position-limiting drum or gag lever post, and during for position-limiting drum, the retractable cable tube is arranged in the position-limiting drum; During for gag lever post, gag lever post is evenly distributed on around the retractable cable tube.
Said gathering sill circle is the Archimedian screw structure.
Adopt the advantage of the utility model to be:
One, the utility model comprises transmission mechanism and is used for the retractable cable tube of folding and unfolding cable, and said retractable cable tube vertically is arranged on the frame, and the retractable cable tube is provided with the gathering sill circle that cooperates with cable; Said transmission mechanism comprises driving motor, decelerator, conical gear, driving shaft, electromagnetic clutch and driven shaft, and said decelerator is arranged on the power transmission shaft of driving motor, and the power transmission shaft of driving motor is connected with driving shaft through conical gear; Driving shaft is connected with driven shaft through electromagnetic clutch, and driven shaft is fixedly connected with the retractable cable tube and drives the motion of retractable cable tube, adopts the transmission of electromagnetism suction type; Do not have tangible drive disk assembly wearing and tearing, transmission is more reliable, and transmission efficiency is high; Adopt the conical gear stressed effect good, the useful life of improving device, the mode that adopts the retractable cable tube vertically to be provided with; Not only practice thrift the take-up space, reduce power of motor, energy efficient; Institute's folding and unfolding cable or tubing length are rised appreciably; The line of equal length or pipe adopt this device can practice thrift space, a large amount of down-hole, and retractable cable efficient are higher.
Two, in the utility model, said frame is provided with conical bearing, and conical bearing is positioned at retractable cable tube top and bottom; Driven shaft one end is connected with the conical bearing of retractable cable tube upper end, and the center that the other end passes the retractable cable tube is connected with the conical bearing of lower end, and this structure has realized the center transmission of electromagnetism suction type; Structure is compact more; Take-up power is more even, and adopts the mode of conical bearing can reduce stress and concentrate, and can bear bigger radial load and axial load.
Three, in the utility model, also is provided with on the said frame with the retractable cable tube and cooperates, and said limiting component is position-limiting drum or gag lever post that during for position-limiting drum, the retractable cable tube is arranged in the position-limiting drum with the spacing limiting component in the gathering sill circle of cable; During for gag lever post; Gag lever post is evenly distributed on around the retractable cable tube; Limiting component through being provided with avoided take-up cable in the gathering sill circle in the take-up process to leave the gathering sill circle, and what guaranteed take-up cable more can be regular in the take-up process is wrapped in the gathering sill circle.
Four, in the utility model, said gathering sill circle is the Archimedian screw structure, makes the consistency of retractable cable tube better, and cable is stressed more even in the gathering sill circle, thereby has protected cable.
Description of drawings
Fig. 1 is the utility model structural representation
Be labeled as among the figure: 1, limiting component, 2, cable, 3, the gathering sill circle, 4, conical bearing, 5, electromagnetic clutch, 6, frame, 7, decelerator, 8, driving motor, 9, conical gear, 10, the retractable cable tube, 11, driving shaft, 12, driven shaft.
Embodiment
A kind of aircraft duties ground well flip-over type cable automatic deploying and retracting line apparatus; Comprise frame 6; Also comprise transmission mechanism and the retractable cable tube 10 that is used for folding and unfolding cable 2; Said retractable cable tube 10 vertically is arranged on the frame 6, and retractable cable tube 10 is provided with the gathering sill circle 3 that cooperates with cable, and said transmission mechanism comprises driving motor 8, decelerator 7, conical gear 9, driving shaft 11, electromagnetic clutch 5 and driven shaft 12; Said decelerator 7 is arranged on the power transmission shaft of driving motor 8; The power transmission shaft of driving motor 8 is connected with driving shaft 11 through conical gear 9, and driving shaft 11 is connected with driven shaft 12 through electromagnetic clutch 5, and driven shaft 12 is fixedly connected with retractable cable tube 10 and drives 10 motions of retractable cable tube.
The preferred implementation of the utility model does; Said frame 6 is provided with conical bearing 4; Conical bearing 4 is positioned at retractable cable tube 10 top and bottom; Driven shaft 12 1 ends are connected with the conical bearing 4 of retractable cable tube 10 upper ends, and the center that the other end passes retractable cable tube 10 is connected with the conical bearing 4 of retractable cable tube 10 lower ends.
The another preferred implementation of the utility model does, also is provided with on the said frame 6 with retractable cable tube 10 to cooperate the spacing limiting component 1 in gathering sill circle 3 of cable.
Further, said limiting component 1 is position-limiting drum or gag lever post, and during for position-limiting drum, retractable cable tube 10 is arranged in the position-limiting drum; During for gag lever post, gag lever post is evenly distributed on around the retractable cable tube 10.
The another preferred implementation of the utility model is that said gathering sill circle 3 is the Archimedian screw structure.
Below the utility model do is launched explanation:
In the utility model, driven shaft 12 is fixedly mounted on retractable cable tube 10 centers; Driving motor 8 be fixedly mounted on the frame 6 after decelerator 7 links to each other; Half is contained in driving shaft 11 1 ends electromagnetic clutch 5, and second half is contained in driven shaft 12 1 ends; The power transmission shaft of driving motor 8 is connected with driving shaft 11 through conical gear 9, makes the power transmission shaft of driving motor 8 and driving shaft 11 perpendicular, thereby makes retractable cable tube 10 vertically be provided with; Conical bearing 4 links to each other with driven shaft 12 and lays respectively at driven shaft 12 two ends.
The operation principle of the utility model is: after driving motor 8 charged work; Drawing cable button on the push dish; This moment, electromagnetic clutch 5 was charged, and driven shaft 12 forms positive engagement with driving shaft 11, rotated thereby drive retractable cable tube 10; 1 pair of cable 2 of limiting component is spacing in this process, and cable 2 is arranged in gathering sill circle 3 regularly.
Obviously; Those of ordinary skill in the art is according to technological know-how of being grasped and customary means; According to the above 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 the protection range of the utility model.

Claims (5)

1. aircraft duties ground well flip-over type cable automatic deploying and retracting line apparatus; Comprise frame (6); It is characterized in that: also comprise transmission mechanism and the retractable cable tube (10) that is used for the folding and unfolding cable; Said retractable cable tube (10) vertically is arranged on the frame (6); Retractable cable tube (10) is provided with the gathering sill circle (3) that cooperates with cable; Said transmission mechanism comprises driving motor (8), decelerator (7), conical gear (9), driving shaft (11), electromagnetic clutch (5) and driven shaft (12), and said decelerator (7) is arranged on the power transmission shaft of driving motor (8), and the power transmission shaft of driving motor (8) is connected with driving shaft (11) through conical gear (9); Driving shaft (11) is connected with driven shaft (12) through electromagnetic clutch (5), and driven shaft (12) is fixedly connected with retractable cable tube (10) and drives retractable cable tube (10) motion.
2. aircraft duties ground well flip-over type cable automatic deploying and retracting line apparatus according to claim 1; It is characterized in that: said frame (6) is provided with conical bearing (4); Conical bearing (4) is positioned at retractable cable tube (10) top and bottom; Driven shaft (12) one ends are connected with the conical bearing (4) of retractable cable tube (10) upper end, and the center that the other end passes retractable cable tube (10) is connected with the conical bearing (4) of retractable cable tube (10) lower end.
3. aircraft duties ground well flip-over type cable automatic deploying and retracting line apparatus according to claim 1 and 2 is characterized in that: also be provided with on the said frame (6) with retractable cable tube (10) and cooperate the spacing limiting component (1) in gathering sill circle (3) of cable.
4. aircraft duties ground well flip-over type cable automatic deploying and retracting line apparatus according to claim 3, it is characterized in that: said limiting component (1) is position-limiting drum or gag lever post, and during for position-limiting drum, retractable cable tube (10) is arranged in the position-limiting drum; During for gag lever post, gag lever post is evenly distributed on retractable cable tube (10) all around.
5. according to claim 1,2 or 4 described aircraft duties ground well flip-over type cable automatic deploying and retracting line apparatus, it is characterized in that: said gathering sill circle (3) is the Archimedian screw structure.
CN2011204327391U 2011-11-04 2011-11-04 Inverted-type automatic cable pay-off and take-up device of aircraft service ground well Active CN202333706U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011204327391U CN202333706U (en) 2011-11-04 2011-11-04 Inverted-type automatic cable pay-off and take-up device of aircraft service ground well

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011204327391U CN202333706U (en) 2011-11-04 2011-11-04 Inverted-type automatic cable pay-off and take-up device of aircraft service ground well

Publications (1)

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CN202333706U true CN202333706U (en) 2012-07-11

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105449592A (en) * 2015-11-27 2016-03-30 中国石油集团钻井工程技术研究院 Cable pay-off device for downhole instrument and pay-off method
CN111313339A (en) * 2020-04-17 2020-06-19 江苏枂硕电子科技有限公司 High-temperature-resistant power supply line protection device for automation equipment and use method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105449592A (en) * 2015-11-27 2016-03-30 中国石油集团钻井工程技术研究院 Cable pay-off device for downhole instrument and pay-off method
CN111313339A (en) * 2020-04-17 2020-06-19 江苏枂硕电子科技有限公司 High-temperature-resistant power supply line protection device for automation equipment and use method

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
EE01 Entry into force of recordation of patent licensing contract
EE01 Entry into force of recordation of patent licensing contract

Assignee: Chengdu comparison Technology Co., Ltd.

Assignor: Chengdu Graft Aviation Equipment Co., Ltd.

Contract record no.: 2017990000428

Denomination of utility model: Inverted-type automatic cable pay-off and take-up device of aircraft service ground well

Granted publication date: 20120711

License type: Exclusive License

Record date: 20171031