CN201313546Y - High-speed overhead passenger device for coal mine - Google Patents
High-speed overhead passenger device for coal mine Download PDFInfo
- Publication number
- CN201313546Y CN201313546Y CNU2008202159864U CN200820215986U CN201313546Y CN 201313546 Y CN201313546 Y CN 201313546Y CN U2008202159864 U CNU2008202159864 U CN U2008202159864U CN 200820215986 U CN200820215986 U CN 200820215986U CN 201313546 Y CN201313546 Y CN 201313546Y
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- track
- steel rope
- wire rope
- getting
- rope
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Abstract
A high-speed overhead passenger device for a coal mine comprises endless wire ropes running in a circulating way and a passenger carrier lapped on the wire rope. The device is characterized in that a steel beam is arranged above the wire rope on each side, a plurality of hanging tubes are connected on the steel beam, a getting on station is arranged on the initial section of the wire rope on each side, a getting off station is arranged on the end section of the wire rope on each side, the wire rope corresponding to the getting on station inclines downwardly, and the wire rope corresponding to the getting off station inclines upwardly; both the getting on station and the getting off station comprise a triangular track with an opened top, in addition, the getting on station further comprises a releasing mechanism and the getting off station further comprises a non-return mechanism; and each track is connected between the two corresponding handing tubes via two general clamps, the wire rope passes through the track, the passenger carrier is hung on the wire rope via a triangular hanger with an opened bottom, and roller wheels capable of rolling on the surfaces of the two sides of the track are arranged on the two sides of the hanger. The high-speed overhead passenger device can ensure the safety of passengers when passengers get on/off the passenger carrier, and remarkably increases the running speed of the wire rope.
Description
Technical field
The utility model relates to colliery high speed overhead manned equipment.
Background technology
The colliery has the steel rope that adopts the running of continuous rope cycle mode with the fixed rope clip overhead manned equipment, and aircraft is fixed on the steel rope, and aircraft moves along with the running of steel rope, and personnel are delivered by aircraft.Because in running, travelling people person's steel rope gets on the bus when promptly going up aircraft all the time, catch up with aircraft and take, when getting off, aircraft is also mobile, so upper and lower to take device very dangerous, the running velocity of steel rope is lower for this reason, generally can only be about 1.2m/s.
The utility model content
The purpose of this utility model is to propose the colliery high speed overhead manned equipment that a kind of travelling people person can safe upper and lower aircraft.
For achieving the above object, the utility model is taked following technical scheme:
The utility model comprises the steel rope and the aircraft that is overlapped on the steel rope of continuous rope cycle mode running, above every side steel rope, be provided with girder steel, be connected with some suspended tubes on the girder steel, be provided with bus loading zone in the beginning of every side steel rope section, the latter end of steel rope is provided with debarkation stop, the pairing steel rope of bus loading zone is downward-sloping, and the pairing steel rope of debarkation stop is inclined upwardly; Bus loading zone and debarkation stop respectively comprise the inc triangle track in top, and in addition, bus loading zone also comprises clearance mechanism, and debarkation stop also comprises non-return mechanism; Each is connected track between cooresponding two suspended tubes by two universal clamps, and steel rope passes from track, and described aircraft is hung on the steel rope by the inc triangular hook in bottom, and the both sides of hook are provided with the roller that can roll on surface, track both sides.
Initiating terminal at the bus loading zone track is fixed with baffle plate, and the end of debarkation stop track is fixed with anti-collision block.
In the front and back of bus loading zone and the front and back of debarkation stop one group of rope sheave is set respectively, rope sheave is fixed on the corresponding suspended tubes by universal clamp.
Above the track of bus loading zone, be provided with the Safety hood that links together by connecting arm and track.
Described clearance mechanism has adapter plate, front frame, hydraulic driver, clearance baffle plate and after poppet; Described adapter plate is fixed between the two corresponding suspended tubes by universal clamp, described front frame and after poppet are fixed on the adapter plate, the rear end of hydraulic driver is hinged on the after poppet, the piston rod of described hydraulic driver and described clearance baffle plate upper end are hinged, and the middle part of clearance baffle plate is hinged on the front frame by bearing pin.
Described non-return mechanism has support, swing arm, lock dog and non-return piece; Described support is fixing in orbit, and described swing arm is hinged on the support by bearing pin, and fixedly in the swing arm, described non-return piece is fixed on the support and is in below the lock dog described lock dog.
Described rope sheave has bent axle, and rope sheave is connected with universal clamp by bent axle, and bent axle and universal clamp bonded assembly one end are square shaft.
Aircraft of the present utility model glides along the bevelled track when bus loading zone, in the process that glides, because the effect of the component of acceleration of acceleration due to gravity on slideway, the speed of aircraft is more and more faster, when leaving bus loading zone, speed reaches the system running speed value, with the steel rope overlap joint of high-speed cruising, with the steel rope ahead running.When running to debarkation stop, aircraft and steel rope break away from, along sliding on the acclivitous track, speed decelerates to zero gradually by system's runtime value, and travelling people person of the present utility model is getting on the bus or when getting off, aircraft all remains static, so aircraft is very safe up and down for personnel, further, owing to can guarantee travelling people person's aircraft safety up and down, the running velocity of steel rope can improve greatly.
Description of drawings
For the easier quilt of content of the present utility model is clearly understood, below the specific embodiment and in conjunction with the accompanying drawings of basis, the utility model is described in further detail, wherein
Fig. 1 is embodiment 1 system diagram;
Fig. 2 is the bus loading zone diagrammatic sketch;
Fig. 3 is the debarkation stop diagrammatic sketch;
Fig. 4 is that aircraft is connected diagrammatic sketch with track;
Fig. 5 is the track diagrammatic sketch;
Fig. 6 is the A-A view of Fig. 3;
Fig. 7 is a clearance mechanism diagrammatic sketch;
Fig. 8 is that the B of Fig. 7 is to view;
Fig. 9 is the non-return mechanism diagrammatic sketch;
Figure 10 is that the C of Fig. 9 is to view;
Figure 11 is embodiment 2 diagrammatic sketch.
The specific embodiment
See Fig. 1, embodiment 1 comprises the steel rope 2 of continuous rope cycle mode running, drives operation by actuating device 21 and tail-pulley device 22.Be provided with bus loading zone e in the beginning of steel rope 2 section, the latter end of steel rope 2 is provided with debarkation stop f.
See Fig. 2 to Fig. 6, be provided with girder steel 1 above every side steel rope 2, by bolted connection some suspended tubes 4 are arranged on the girder steel 1, the pairing steel rope of bus loading zone e 2 is downward-sloping, and the pairing steel rope 2 of debarkation stop f is inclined upwardly.Bus loading zone e and debarkation stop f include the inc triangle track 5 in top, in addition, bus loading zone also comprises clearance mechanism 7 and is fixed on the baffle plate 11 of bus loading zone e track 5 initiating terminals that debarkation stop f also comprises non-return mechanism 8 and the anti-collision block 12 that is fixed on debarkation stop f track 5 ends.Track 5 respectively is connected between cooresponding two suspended tubes 4 by two universal clamps 6, adjusts the angle of inclination that track 5 can be adjusted in the position of universal clamp on suspended tubes, and steel rope 2 passes from track 5.Universal clamp is buied from market.Described aircraft 3 is hung on the steel rope 2 by the inc triangular hook 3-1 in bottom, the both sides of hook 3-1 are provided with the roller 3-2 that can roll on surface, track 5 both sides, what roller 3-2 adopted is antifriction-bearing box, the inboard, middle part of hook 3-1 is provided with rope lining 3-3, hook 3-1 hangs on the steel rope 2, with steel rope 2 friction be rope lining 3-3, can reduce the resistance of taxing of steel rope 2.In the front and back of bus loading zone e and the front and back of debarkation stop f one group of rope sheave 9 is set respectively, rope sheave 9 is fixed on the corresponding suspended tubes 4 by universal clamp 6.Described rope sheave 9 has bent axle 9-1, and rope sheave 9 is connected with universal clamp 6 by bent axle 9-1, and bent axle 9-1 and universal clamp 6 bonded assemblys one end are square shaft.Rope sheave 9 control steel ropes move in orbit.
Above the track 5 of bus loading zone e, be provided with the Safety hood 10 that links together by connecting arm 13 and track 5.
See Fig. 7 and Fig. 8, described clearance mechanism 7 has adapter plate 7-1, front frame 7-2, electro hydraulicthruster 7-3, clearance baffle plate 7-4 and after poppet 7-5; Described adapter plate 7-1 is fixed between the two corresponding suspended tubes 4 by universal clamp 6, described front frame 7-2 and after poppet 7-5 are fixed on the adapter plate 7-1, the piston rod 7-3-1 of described electro hydraulicthruster 7-3 and described clearance baffle plate 7-4 upper end are hinged, the rear portion of electro hydraulicthruster 7-3 is hinged on the after poppet 7-5, and the middle part of clearance baffle plate 7-4 is hinged on the front frame 7-2 by bearing pin 7-6.Electro hydraulicthruster 7-3 action drives clearance baffle plate 7-4 swing, and the operation passage of aircraft is opened.
See Fig. 9 and Figure 10, described non-return mechanism 8 has support 8-1, swing arm 8-2, lock dog 8-3 and non-return piece 8-4; Described support 8-1 is fixed on the track 5, and described swing arm 8-2 is hinged on the support 8-1 by bearing pin 8-5, and fixedly on the swing arm 8-2, described non-return piece 8-4 is fixed on the support 8-1 described lock dog 8-3.Under the normal circumstances, swing arm 8-2 is sagging, and swing arm 8-2 can swing by line direction before aircraft, opens passage to aircraft.Because the lock dog 8-3 on the swing arm 8-2 is subjected to stopping of non-return piece 8-4, swing arm 8-2 can't swing by the preceding line direction of contrary aircraft, prevents that like this aircraft from retreating down on the steel rope that slides into high-speed cruising.
During use, travelling people person is placed on aircraft on the track of bus loading zone, personnel are sitting on the aircraft, start the master cock of clearance mechanism, the clearance baffle plate 7-4 of clearance mechanism opens, and aircraft slides on the bevelled track from track, glide along track, when the speed of aircraft reaches the steel rope running velocity, with the steel rope overlap joint of high-speed cruising, with the steel rope ahead running.When running to debarkation stop, aircraft and steel rope break away from, and along sliding on the bevelled track, speed decelerates to zero gradually, and travelling people person gets off, and takes aircraft.
See Figure 11, present embodiment is an intermediate station, promptly is provided with intermediate station between bus loading zone and debarkation stop, makes things convenient for travelling people person to break the journey, and what intermediate station was taked is that debarkation stop and bus loading zone are spliced by connection pipe.
Claims (7)
1, a kind of colliery high speed overhead manned equipment, comprise the steel rope (2) of continuous rope cycle mode running and be overlapped on aircraft (3) on the steel rope (2), it is characterized in that: be provided with girder steel (1) in every side steel rope (2) top, be connected with some suspended tubes (4) on the girder steel (1), beginning section at every side steel rope (2) is provided with bus loading zone (e), the latter end of steel rope (2) is provided with debarkation stop (f), the pairing steel rope of bus loading zone (e) (2) is downward-sloping, and the pairing steel rope of debarkation stop (f) (2) is inclined upwardly; Bus loading zone (e) and debarkation stop (f) respectively comprise the inc triangle track in top (5), and in addition, bus loading zone also comprises clearance mechanism (7), and debarkation stop (f) also comprises non-return mechanism (8); Each is connected track (5) between cooresponding two suspended tubes (4) by two universal clamps (6), steel rope (2) passes from track (5), described aircraft (3) is hung on the steel rope (2) by bottom inc triangular hook (3-1), and the both sides of hook (3-1) are provided with the roller (3-2) that can roll on surface, track (5) both sides.
2, colliery according to claim 1 high speed overhead manned equipment is characterized in that: the initiating terminal at bus loading zone (e) track (5) is fixed with baffle plate (11), and the end of debarkation stop (f) track (5) is fixed with anti-collision block (12).
3, colliery according to claim 1 high speed overhead manned equipment is characterized in that: in the front and back of bus loading zone (e) and the front and back of debarkation stop (f) one group of rope sheave (9) is set respectively, rope sheave (9) is fixed on the corresponding suspended tubes (4) by universal clamp (6).
4, colliery according to claim 1 high speed overhead manned equipment is characterized in that: track (5) top at bus loading zone is provided with the Safety hood (10) that links together by connecting arm (13) and track (5).
5, colliery according to claim 1 high speed overhead manned equipment is characterized in that: described clearance mechanism (7) has adapter plate (7-1), front frame (7-2), hydraulic driver (7-3), clearance baffle plate (7-4) and after poppet (7-5); Described adapter plate (7-1) is fixed between the two corresponding suspended tubes (4) by universal clamp (6), described front frame (7-2) and after poppet (7-5) are fixed on the adapter plate (7-1), the rear end of hydraulic driver (7-3) is hinged on the after poppet (7-5), the piston rod (7-3-1) of described hydraulic driver (7-3) is hinged with described clearance baffle plate (7-4) upper end, and the middle part of clearance baffle plate (7-4) is hinged on the front frame (7-2) by bearing pin (7-6).
6, colliery according to claim 1 high speed overhead manned equipment is characterized in that: described non-return mechanism (8) has support (8-1), swing arm (8-2), lock dog (8-3) and non-return piece (8-4); Described support (8-1) is fixed on the track (5), described swing arm (8-2) is hinged on the support (8-1) by bearing pin (8-5), in the fixedly swing arm of described lock dog (8-3) (8-2), described non-return piece (8-4) is fixed on the support (8-1) and is in lock dog (8-3) below.
7, colliery according to claim 3 high speed overhead manned equipment, it is characterized in that: described rope sheave (9) has bent axle (9-1), rope sheave (9) is connected with universal clamp (6) by bent axle (9-1), and bent axle (9-1) is a square shaft with universal clamp (6) bonded assembly one end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008202159864U CN201313546Y (en) | 2008-11-27 | 2008-11-27 | High-speed overhead passenger device for coal mine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008202159864U CN201313546Y (en) | 2008-11-27 | 2008-11-27 | High-speed overhead passenger device for coal mine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201313546Y true CN201313546Y (en) | 2009-09-23 |
Family
ID=41125335
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008202159864U Expired - Fee Related CN201313546Y (en) | 2008-11-27 | 2008-11-27 | High-speed overhead passenger device for coal mine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201313546Y (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2011066693A1 (en) * | 2009-12-03 | 2011-06-09 | 肖公平 | Mineral ropeway large-slope static get-on/off device |
| CN105416303A (en) * | 2015-12-25 | 2016-03-23 | 湖南远扬煤机制造有限公司 | Zero-speed boarding and alighting device for aerial ropeway |
| CN106043322A (en) * | 2016-05-30 | 2016-10-26 | 山东科技大学 | Mining overhead man-riding device capable of being decelerated at get-off point and use method of mining overhead man-riding device |
| CN107054385A (en) * | 2017-03-20 | 2017-08-18 | 单超 | Overhead manned equipment and monorail crane grade separation mechanism |
-
2008
- 2008-11-27 CN CNU2008202159864U patent/CN201313546Y/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2011066693A1 (en) * | 2009-12-03 | 2011-06-09 | 肖公平 | Mineral ropeway large-slope static get-on/off device |
| CN105416303A (en) * | 2015-12-25 | 2016-03-23 | 湖南远扬煤机制造有限公司 | Zero-speed boarding and alighting device for aerial ropeway |
| CN106043322A (en) * | 2016-05-30 | 2016-10-26 | 山东科技大学 | Mining overhead man-riding device capable of being decelerated at get-off point and use method of mining overhead man-riding device |
| CN106043322B (en) * | 2016-05-30 | 2017-11-14 | 山东科技大学 | Get off the mining cable car that can a little slow down |
| CN107054385A (en) * | 2017-03-20 | 2017-08-18 | 单超 | Overhead manned equipment and monorail crane grade separation mechanism |
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Legal Events
| 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: 20090923 Termination date: 20171127 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |