CN103623582A - Brake device mounted on flight experience device - Google Patents
Brake device mounted on flight experience device Download PDFInfo
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- CN103623582A CN103623582A CN201310575094.0A CN201310575094A CN103623582A CN 103623582 A CN103623582 A CN 103623582A CN 201310575094 A CN201310575094 A CN 201310575094A CN 103623582 A CN103623582 A CN 103623582A
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- brake
- skid
- pushing block
- main bearing
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- 238000010586 diagram Methods 0.000 description 2
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- 238000006073 displacement reaction Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
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Abstract
The invention relates to a brake device mounted on a flight experience device. The brake device mounted on the flight experience device comprises a supporting platform, a combined type brake is symmetrically mounted at the left end and the right end of the supporting platform, and the combined type brake comprises an upper main support, a lower main support and a lateral brake. The lateral brake comprises a lateral shoving and pushing device, a lateral brake shoving and pushing block and a lateral brake cushion. The lateral shoving and pushing device is located between the upper main support and the lower main support, the lateral shoving and pushing device is fixedly connected to a supporting platform, the lateral brake cushion is located between an upper brake cushion and a lower brake cushion, and one side of the lateral brake cushion is connected with the lateral shoving and pushing device through the lateral brake shoving and pushing block. The brake device mounted on the flight experience device has the advantages of being reasonable in structural design, convenient to control, good in brake performance and the like; the occurrence of slipping is avoided by adopting a vertical brake and a transverse brake combining mode and by using the fact that the tooth groove direction of first transverse antiskid zigzag teeth, the tooth groove direction of second transverse antiskid zigzag teeth and the tooth groove direction of vertical antiskid zigzag teeth are all perpendicular to the walking direction of a machine, and rapid braking can be achieved in a flight experience process.
Description
Technical field
The present invention relates to a kind of brake gear, specifically a kind of brake gear being arranged on flight experience device.
Background technology
Raising along with people's living standard, people are more and more higher for the pursuit enthusiasm of entertainment life, especially young people, mostly pursue recreation some stimulations, thrilling, this is also the adjustment to the duty of daily high pressure, high load capacity, thereby in the time of can guaranteeing work, has actively optimistic work phychology.In more existing large-scale public places of entertainment; the entertainment selection that has many stimulations, thrill; as outdoor projects such as roller-coasters; utilizing actual visual impact and body-feeling to reach stimulates thrilling object; because these projects are arranged in outdoor and move comparatively violent; though have a lot of roads safety guard, but still exist potential safety hazard.For this reason, people start to design many indoor entertainment selections, adopt the film of indoor broadcasting and the apparatus synchronization action that visitor takes, allow visitor have sensation on the spot in person, and indoor apparatus is also comparatively heavy, inertia during motion is larger, to brake, make troubles like this, if adopt traditional brake gear, often easily occur the phenomenon of skidding, stop incessantly, can work the mischief to visitor's life security like this.
Chinese patent ZL200610062119.7 and for example, a kind of action imitation equipment for amusement, system and method have been proposed, its retaining mechanism adopting comprise the upper connecting rod of the link that is fixedly connected with vehicle frame, both sides up and down that centre position is articulated in respectively link and lower link, the train wheel bridge of installing in one end of upper connecting rod, in one end of lower link, install with lower plate corresponding to train wheel bridge and the locking oil cylinder that is simultaneously connected to the other end of connecting rod and lower link, between upper connecting rod and link, be provided with spring, between lower link and described link, be provided with spring; Upper connecting rod and the folding of lower link phase described in locking oil cylinder pushing, and drive train wheel bridge and the folding of lower plate phase is unclamped or the upper support face of clamping guide-rail, what the mode of this locking was utilized is the mutual extruding between train wheel bridge and lower plate, thereby clamp the guide rail between train wheel bridge and lower plate support, complete locking, and because machine itself is comparatively heavy, inertia is larger, adopt this locking mode to be difficult to realize fast locking, often after machine slides a bit of displacement, could realize locking thoroughly, lock consuming time longer; And the part that train wheel bridge, lower plate contact with guide rail is not done any particular design, just utilize interplanar friction to realize locking, very easily there is skidding, when even the thrust of locking oil cylinder does not reach certain value, machine can slide and not realize locking along guide rail, therefore makes locking lag behind, there is locking time delay, cause difficulty to the establishment of control program, cause the position stopping each time inconsistent, have influence on the effect of amusement.
Summary of the invention
Technical problem to be solved by this invention be to provide a kind of reasonable in design, the side of controlling easily, braking quality is good, can in flight experience process, realize the device of Quick brake, i.e. a kind of brake gear being arranged on flight experience device.
Technical problem to be solved by this invention realizes by the following technical solutions:
A kind of brake gear being arranged on flight experience device, comprise support platform, the two ends, left and right of described support platform are symmetrically installed with combined type brake, described combined type brake comprises main bearing, lower main bearing and side direction brake, described main bearing, lower main bearing symmetry is arranged on the both sides up and down of support platform, described main bearing is connected with upper lever beam by hinged mode, the left end of described upper lever beam is connected with upper brake by hinged mode and squeezes pushing block, the right side central of upper lever beam is connected with support platform by upper extension spring, the right-hand member of upper lever beam is connected with the vertical thruster that squeezes by the crowded post that pushes away, the middle part that pushing block is squeezed in described upper brake is connected with the middle part of upper main bearing by upper gangbar, and the lower surface that pushing block is squeezed in upper brake is connected with braking vane, and the lower end of described upper braking vane is connected with skid, described lower main bearing is connected with lower lever beam by hinged mode, the left end of described lower lever beam is connected with lower brake by hinged mode and squeezes pushing block, and the right side central of lower lever beam is connected with support platform by tension spring, the described vertical other end that squeezes thruster is connected with the right-hand member of lower lever beam, the upper surface that pushing block is squeezed in described lower brake is connected with lower braking vane, the upper end of described lower braking vane is connected with lower skid, described side direction brake comprises that side direction is squeezed thruster, pushing block and side skid are squeezed in side brake, described side direction is squeezed thruster between upper main bearing and lower main bearing, and side direction is squeezed thruster and support platform is connected, described side skid is between upper skid and lower skid, and a side of side skid is braked and squeezed pushing block and squeeze thruster with side direction and be connected by side.
The bottom surface of described upper skid is evenly provided with horizontal anti-skidding sawtooth No. one, and described upper skid is made by abrasive rubber material.
The upper bottom surface of described lower skid is evenly provided with horizontal anti-skidding sawtooth No. two, and described lower skid is made by abrasive rubber material.
The opposite side of described side skid is provided with vertical anti-skidding sawtooth, and described side skid is made by abrasive rubber material.
The teeth groove direction of horizontal anti-skidding sawtooth, No. two horizontal anti-skidding sawtooth and vertical anti-skidding sawtooth is all perpendicular with the direction of machine walking, and adopt abrasive rubber material to make, the generation of the skidding while effectively having avoided the locking of conventional planar friction-type, extended service life, and utilize horizontal anti-skidding sawtooth, No. two horizontal anti-skidding sawtooth and vertical anti-skidding sawtooth pushing guide rail simultaneously, from three faces, produce friction, increased frictional force, can realize brake fast, security performance is high, controls comparatively stable.
When flight experience device moves to after assigned address, can utilize the vertical thruster that squeezes to promote upper lever beam, upper lever beam and lower lever beam open, extension spring and tension spring on difference tractive, and make brake squeeze pushing block, lower brake to squeeze pushing block and mutually draw close, final clamping in upper brake squeezed the guide rail between pushing block, the crowded pushing block of lower brake, realizes vertical brake; And utilize the crowded thruster promotion of side direction side skid to push against the guide rail that is positioned at support platform both sides, thereby from horizontal realization brake.
When needs are walked, can utilize the vertical thruster that squeezes to shrink, and reset under the tractive of upper extension spring, tension spring, make brake squeeze pushing block, the crowded pushing block of lower brake mutually away from, and by side direction, squeeze thruster and drive side skid to reset, flight experience device can be walked like this.
The invention has the beneficial effects as follows: the present invention has the advantages such as reasonable in design, the side's of controlling convenience and braking quality are good, adopt mode vertical and that laterally brake combines, and utilize the teeth groove direction of horizontal anti-skidding sawtooth, No. two horizontal anti-skidding sawtooth and vertical anti-skidding sawtooth all perpendicular with the direction of machine walking, thereby avoided the generation of the skidding of traditional brake gear, can in flight experience process, realize Quick brake.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the present invention is further described.
Fig. 1 is main TV structure schematic diagram of the present invention;
Fig. 2 is the structural representation of looking up of upper skid of the present invention;
Fig. 3 is the plan structure schematic diagram of lower skid of the present invention;
Fig. 4 is the structural representation of side direction brake of the present invention;
Fig. 5 is that the A of Fig. 4 is to view.
The specific embodiment
For technological means, creation characteristic that the present invention is realized, reach object and effect is easy to understand, below the present invention is further set forth.
As shown in Figures 1 to 5, a kind of brake gear being arranged on flight experience device, comprise support platform 1, the two ends, left and right of described support platform 1 are symmetrically installed with combined type brake, described combined type brake comprises main bearing 2, lower main bearing 3 and side direction brake, described main bearing 2, lower main bearing 3 symmetries are arranged on the both sides up and down of support platform 1, described main bearing 2 is connected with upper lever beam 4 by hinged mode, the left end of described upper lever beam 4 is connected with upper brake by hinged mode and squeezes pushing block 9, the right side central of upper lever beam 4 is connected with support platform 1 by upper extension spring 6, the right-hand member of upper lever beam 4 is connected with the vertical thruster 20 that squeezes by the crowded post 8 that pushes away, the middle part that pushing block 9 is squeezed in described upper brake is connected with the middle part of upper main bearing 2 by upper gangbar 18, and the lower surface that pushing block 9 is squeezed in upper brake is connected with braking vane 10, and the lower end of described upper braking vane 10 is connected with skid 11, described lower main bearing 3 is connected with lower lever beam 5 by hinged mode, the left end of described lower lever beam 5 is connected with lower brake by hinged mode and squeezes pushing block 14, and the right side central of lower lever beam 5 is connected with support platform 1 by tension spring 7, the described vertical other end that squeezes thruster 20 is connected with the right-hand member of lower lever beam 5, the upper surface that pushing block 14 is squeezed in described lower brake is connected with lower braking vane 13, the upper end of described lower braking vane 13 is connected with lower skid 12, described side direction brake comprises that side direction is squeezed thruster 15, pushing block 16 and side skid 17 are squeezed in side brake, described side direction is squeezed thruster 15 between upper main bearing 2 and lower main bearing 3, and side direction is squeezed thruster 15 and support platform 1 is connected, described side skid 17 is between upper skid 11 and lower skid 12, and a side of side skid 17 is braked and squeezed pushing block 16 and squeeze thruster 15 with side direction and be connected by side.
The bottom surface of described upper skid 11 is evenly provided with horizontal anti-skidding sawtooth 1101 No. one, and described upper skid 11 is made by abrasive rubber material.
The upper bottom surface of described lower skid 12 is evenly provided with horizontal anti-skidding sawtooth 1201 No. two, and described lower skid 12 is made by abrasive rubber material.
The opposite side of described side skid 17 is provided with vertical anti-skidding sawtooth 1701, and described side skid 17 is made by abrasive rubber material.
A horizontal anti-skidding sawtooth 1101, the teeth groove direction of No. two horizontal anti-skidding sawtooth 1201 and vertical anti-skidding sawtooth 1701 is all perpendicular with the direction of machine walking, and adopt abrasive rubber material to make, the generation of the skidding while effectively having avoided the locking of conventional planar friction-type, extended service life, and utilize horizontal anti-skidding sawtooth 1101 No. one, No. two horizontal anti-skidding sawtooth 1201 and vertical anti-skidding sawtooth 1701 be pushing guide rail simultaneously, from three faces, produce friction, increased frictional force, can realize brake fast, security performance is high, control comparatively stable.
When flight experience device moves to after assigned address, can utilize the vertical thruster 20 that squeezes to promote upper lever beam 4, upper lever beam 4 and lower lever beam 5 open, extension spring 6 and tension spring 7 on difference tractive, and make brake squeeze pushing block 9, lower brake to squeeze pushing block 14 and mutually draw close, the final guide rail that squeezes 14 of pushing blocks in the crowded pushing block 9 of upper brake, lower brake that clamps, realizes vertical brake; And utilize the crowded thruster 15 promotion side skids 17 of side direction to push against the guide rail that is positioned at support platform 1 both sides, thereby from horizontal realization brake.
When needs are walked, can utilize the vertical thruster 20 that squeezes to shrink, and reset under the tractive of upper extension spring 6, tension spring 7, make brake squeeze pushing block 9, the crowded pushing block 14 of lower brake mutually away from, and squeezing thruster 15 drive side skids 17 resets by side direction, flight experience device can be walked like this.
More than show and described basic principle of the present invention, principal character and advantage of the present invention.The technical staff of the industry should understand; the present invention is not restricted to the described embodiments; what in above-described embodiment and description, describe is principle of the present invention; without departing from the spirit and scope of the present invention; the present invention also has various changes and modifications, and these changes and improvements all fall in the claimed scope of the invention.The claimed scope of the present invention is defined by appending claims and equivalent thereof.
Claims (4)
1. the brake gear being arranged on flight experience device, comprise support platform, the two ends, left and right of described support platform are symmetrically installed with combined type brake, described combined type brake comprises main bearing, lower main bearing and side direction brake, described main bearing, lower main bearing symmetry is arranged on the both sides up and down of support platform, described main bearing is connected with upper lever beam by hinged mode, the left end of described upper lever beam is connected with upper brake by hinged mode and squeezes pushing block, the right side central of upper lever beam is connected with support platform by upper extension spring, the right-hand member of upper lever beam is connected with the vertical thruster that squeezes by the crowded post that pushes away, the middle part that pushing block is squeezed in described upper brake is connected with the middle part of upper main bearing by upper gangbar, and the lower surface that pushing block is squeezed in upper brake is connected with braking vane, and the lower end of described upper braking vane is connected with skid, described lower main bearing is connected with lower lever beam by hinged mode, the left end of described lower lever beam is connected with lower brake by hinged mode and squeezes pushing block, and the right side central of lower lever beam is connected with support platform by tension spring, the described vertical other end that squeezes thruster is connected with the right-hand member of lower lever beam, the upper surface that pushing block is squeezed in described lower brake is connected with lower braking vane, the upper end of described lower braking vane is connected with lower skid, it is characterized in that: described side direction brake comprises that side direction is squeezed thruster, pushing block and side skid are squeezed in side brake, described side direction is squeezed thruster between upper main bearing and lower main bearing, and side direction is squeezed thruster and support platform is connected, described side skid is between upper skid and lower skid, and a side of side skid is braked and squeezed pushing block and squeeze thruster with side direction and be connected by side.
2. a kind of brake gear being arranged on flight experience device according to claim 1, is characterized in that: the bottom surface of described upper skid is evenly provided with horizontal anti-skidding sawtooth No. one, and described upper skid is made by abrasive rubber material.
3. a kind of brake gear being arranged on flight experience device according to claim 1, is characterized in that: the upper bottom surface of described lower skid is evenly provided with horizontal anti-skidding sawtooth No. two, and described lower skid is made by abrasive rubber material.
4. a kind of brake gear being arranged on flight experience device according to claim 1, is characterized in that: the opposite side of described side skid is provided with vertical anti-skidding sawtooth, and described side skid is made by abrasive rubber material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310575094.0A CN103623582B (en) | 2013-11-13 | 2013-11-13 | Brake device mounted on flight experience device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310575094.0A CN103623582B (en) | 2013-11-13 | 2013-11-13 | Brake device mounted on flight experience device |
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| Publication Number | Publication Date |
|---|---|
| CN103623582A true CN103623582A (en) | 2014-03-12 |
| CN103623582B CN103623582B (en) | 2015-04-01 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310575094.0A Active CN103623582B (en) | 2013-11-13 | 2013-11-13 | Brake device mounted on flight experience device |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109529364A (en) * | 2018-11-22 | 2019-03-29 | 北京中冶设备研究设计总院有限公司 | A kind of coaster wagon rack device |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3680487A (en) * | 1970-02-20 | 1972-08-01 | Salvatore Cirami | Walking robot amusement ride |
| WO1996015514A1 (en) * | 1994-11-16 | 1996-05-23 | Eduard Feuer | Flight simulator with full roll rotation capability |
| CN202106959U (en) * | 2011-04-18 | 2012-01-11 | 中南大学 | Anti-slip brake control system of an airplane |
| CN202703889U (en) * | 2012-06-05 | 2013-01-30 | 陈晓春 | Propelling and braking integrated unit |
| CN203648058U (en) * | 2013-11-13 | 2014-06-18 | 芜湖华强文化科技产业有限公司 | Braking device arranged on flying experience device |
-
2013
- 2013-11-13 CN CN201310575094.0A patent/CN103623582B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3680487A (en) * | 1970-02-20 | 1972-08-01 | Salvatore Cirami | Walking robot amusement ride |
| WO1996015514A1 (en) * | 1994-11-16 | 1996-05-23 | Eduard Feuer | Flight simulator with full roll rotation capability |
| CN202106959U (en) * | 2011-04-18 | 2012-01-11 | 中南大学 | Anti-slip brake control system of an airplane |
| CN202703889U (en) * | 2012-06-05 | 2013-01-30 | 陈晓春 | Propelling and braking integrated unit |
| CN203648058U (en) * | 2013-11-13 | 2014-06-18 | 芜湖华强文化科技产业有限公司 | Braking device arranged on flying experience device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109529364A (en) * | 2018-11-22 | 2019-03-29 | 北京中冶设备研究设计总院有限公司 | A kind of coaster wagon rack device |
| CN109529364B (en) * | 2018-11-22 | 2020-03-24 | 北京中冶设备研究设计总院有限公司 | Roller coaster frame device |
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| Publication number | Publication date |
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| CN103623582B (en) | 2015-04-01 |
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