CN103623582B - Brake device mounted on flight experience device - Google Patents
Brake device mounted on flight experience device Download PDFInfo
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- CN103623582B CN103623582B CN201310575094.0A CN201310575094A CN103623582B CN 103623582 B CN103623582 B CN 103623582B CN 201310575094 A CN201310575094 A CN 201310575094A CN 103623582 B CN103623582 B CN 103623582B
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- brake
- skid
- pushing block
- main bearing
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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 be arranged in flight experience device.
Background technology
Along with the raising of people's living standard, people are more and more higher for the pursuit enthusiasm of entertainment life, especially young people, some stimulations of most pursuit, thrilling recreations, this is also the adjustment of the duty to daily high pressure, high load capacity, thus has actively optimistic work phychology when can ensure work.In more existing large-scale public places of entertainment; there are many stimulations, thrilling entertainment selection; as outdoor projects such as roller-coasters; utilize actual visual impact and body-feeling to reach and stimulate thrilling object; be arranged in outdoor due to these projects and move comparatively violent; though have a lot of roads safety guard, but still there is potential safety hazard.For this reason, people start the entertainment selection designing many indoor, adopt the apparatus synchronization action that the film of indoor broadcasting and visitor take, allow visitor have sensation on the spot in person, and the apparatus of indoor is also comparatively heavy, inertia during motion is larger, make troubles to brake like this, according to traditional brake gear, often easily occur the phenomenon of skidding, namely stop incessantly, can work the mischief to the life security of visitor like this.
And for example Chinese patent ZL200610062119.7, propose a kind of action imitation equipment for amusement, system and method, its retaining mechanism adopted comprises the locking oil cylinder that the link, the centre position that are fixedly connected with vehicle frame are articulated in the upper connecting rod of the both sides up and down of link and lower link, the train wheel bridge installed in one end of upper connecting rod, the lower plate corresponding with train wheel bridge installed in one end of lower link and the other end that is simultaneously connected to connecting rod and lower link respectively, be provided with spring between upper connecting rod and link, 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 to unclamp or the upper supporting surface of clamping guide-rail, the mutual extruding that what the mode of this locking utilized is between train wheel bridge and lower plate, thus the guide rail between clamping train wheel bridge and lower plate support, complete locking, and due to machine itself comparatively heavy, inertia is larger, this locking mode is adopted to be difficult to realize locking fast, often could realize locking thoroughly after machine slides a bit of displacement, lock consuming time longer; And the part of train wheel bridge, lower plate and guide rail contact does not do any particular design, interplanar friction is just utilized to realize locking, very easily there is skidding, when even the thrust of locking oil cylinder does not reach certain value, machine can slide along guide rail and not realize locking, therefore makes locking delayed, there is locking time delay, cause difficulty to the establishment of control program, cause the position stopped 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, manipulation side easily, braking quality is good, can realize the device of Quick brake, i.e. a kind of brake gear be arranged in flight experience device in flight experience process.
Technical problem to be solved by this invention realizes by the following technical solutions:
A kind of brake gear be arranged in 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 vertical crowded thruster by the crowded post that pushes away, the middle part that pushing block is squeezed in described upper brake is connected by the middle part of upper gangbar with upper main bearing, 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 squeezing 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 side direction and squeezes thruster, the crowded pushing block of side brake and side skid, described side direction squeezes thruster between upper main bearing and lower main bearing, and side direction squeezes thruster and support platform is connected, described side skid is between upper skid and lower skid, and the side of side skid is squeezed pushing block by side brake and squeezed thruster with side direction and be connected.
The bottom surface of described upper skid is evenly provided with an anti-skidding sawtooth of transverse direction, and described upper skid is made up of abrasive rubber material.
The upper bottom surface of described lower skid is evenly provided with No. two anti-skidding sawtooth of transverse direction, and described lower skid is made up of abrasive rubber material.
The opposite side of described side skid is provided with vertical anti-skidding sawtooth, and described side skid is made up of abrasive rubber material.
The direction all walked with machine in the teeth groove direction of the anti-skidding sawtooth of transverse direction, No. two anti-skidding sawtooth of transverse direction and a vertical anti-skidding sawtooth is perpendicular, and adopt abrasive rubber material to make, effectively avoid the generation of skidding when conventional planar friction-type is locked, extend service life, and utilize an anti-skidding sawtooth of transverse direction, No. two anti-skidding sawtooth of transverse direction and vertical anti-skidding sawtooth to extrude the carrying out of guide rail simultaneously, friction is produced from three faces, add frictional force, can realize braking fast, security performance is high, manipulates comparatively stable.
After flight experience device moves to assigned address, the vertical thruster that squeezes can be utilized to promote upper lever beam, upper lever beam and lower lever beam open, extension spring and tension spring on tractive respectively, and make brake squeeze pushing block, lower brake is squeezed pushing block and is mutually drawn close, final clamping is in that pushing block is squeezed in brake, guide rail between pushing block is squeezed in lower brake, realizes vertical brake; And utilize side direction to squeeze thruster to promote side skid and push against the guide rail being positioned at support platform both sides, thus from laterally realizing brake.
When needs are walked, the vertical thruster that squeezes can be utilized to shrink, and reset under the tractive of upper extension spring, tension spring, make that pushing block is squeezed in brake, lower brake squeeze pushing block mutually away from, and squeeze the skid reset of thruster drive side by side direction, such flight experience device can be walked.
The invention has the beneficial effects as follows: the present invention has the advantages such as reasonable in design, manipulation side's convenience and braking quality are good, adopt the vertical and mode combined of laterally braking, and the direction utilizing the teeth groove direction of an anti-skidding sawtooth of transverse direction, No. two anti-skidding sawtooth of transverse direction and vertical anti-skidding sawtooth all to walk with machine is perpendicular, thus avoid the generation of the skidding of conventional brake device, Quick brake can be realized in flight experience process.
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 be upper skid of the present invention look up structural representation;
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 the A direction view of Fig. 4.
Detailed description of the invention
The technological means realized to make the present invention, creation characteristic, reaching object and effect is easy to understand, below the present invention being set forth further.
As shown in Figures 1 to 5, a kind of brake gear be arranged in 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 symmetry is 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 vertical crowded thruster 20 by the crowded post 8 that pushes away, the middle part that pushing block 9 is squeezed in described upper brake is connected by the middle part of upper gangbar 18 with upper main bearing 2, 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 squeezing 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 side direction and squeezes thruster 15, the crowded pushing block 16 of side brake and side skid 17, described side direction squeezes thruster 15 between upper main bearing 2 and lower main bearing 3, and side direction squeezes thruster 15 and support platform 1 is connected, described side skid 17 is between upper skid 11 and lower skid 12, and the side of side skid 17 is squeezed pushing block 16 by side brake and squeezed thruster 15 with side direction and be connected.
The bottom surface of described upper skid 11 is evenly provided with an anti-skidding sawtooth 1101 of transverse direction, and described upper skid 11 is made up of abrasive rubber material.
The upper bottom surface of described lower skid 12 is evenly provided with No. two anti-skidding sawtooth 1201 of transverse direction, and described lower skid 12 is made up of 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 up of abrasive rubber material.
An anti-skidding sawtooth 1101 of transverse direction, the direction all walked with machine in the teeth groove direction of No. two anti-skidding sawtooth of transverse direction 1201 and vertical anti-skidding sawtooth 1701 is perpendicular, and adopt abrasive rubber material to make, effectively avoid the generation of skidding when conventional planar friction-type is locked, extend service life, and utilize an anti-skidding sawtooth 1101 of transverse direction, No. two anti-skidding sawtooth of transverse direction 1201 and vertical anti-skidding sawtooth 1701 extrude the carrying out of guide rail simultaneously, friction is produced from three faces, add frictional force, can realize braking fast, security performance is high, manipulate comparatively stable.
After flight experience device moves to assigned address, the vertical thruster 20 that squeezes can be utilized to promote upper lever beam 4, upper lever beam 4 and lower lever beam 5 open, extension spring 6 and tension spring 7 on tractive respectively, and make brake squeeze pushing block 9, lower brake is squeezed pushing block 14 and is mutually drawn close, final clamping is in that pushing block 9 is squeezed in brake, guide rail between pushing block 14 is squeezed in lower brake, realizes vertical brake; And utilize side direction to squeeze thruster 15 to promote side skid 17 and push against the guide rail being positioned at support platform 1 both sides, thus from laterally realizing brake.
When needs are walked, the vertical thruster 20 that squeezes can be utilized to shrink, and reset under the tractive of upper extension spring 6, tension spring 7, make that pushing block 9 is squeezed in brake, lower brake squeeze pushing block 14 mutually away from, and squeeze thruster 15 by side direction and drive side skid 17 to reset, such flight experience device can be walked.
More than show and describe general 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; the just principle of the present invention described in above-described embodiment and description; 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.Application claims protection domain is defined by appending claims and equivalent thereof.
Claims (4)
1. one kind is arranged on the brake gear in 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 vertical crowded thruster by the crowded post that pushes away, the middle part that pushing block is squeezed in described upper brake is connected by the middle part of upper gangbar with upper main bearing, 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 squeezing 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 side direction and squeezes thruster, the crowded pushing block of side brake and side skid, described side direction squeezes thruster between upper main bearing and lower main bearing, and side direction squeezes thruster and support platform is connected, described side skid is between upper skid and lower skid, and the side of side skid is squeezed pushing block by side brake and squeezed thruster with side direction and be connected.
2. a kind of brake gear be arranged in flight experience device according to claim 1, is characterized in that: the bottom surface of described upper skid is evenly provided with an anti-skidding sawtooth of transverse direction, and described upper skid is made up of abrasive rubber material.
3. a kind of brake gear be arranged in flight experience device according to claim 1, is characterized in that: the upper bottom surface of described lower skid is evenly provided with No. two anti-skidding sawtooth of transverse direction, and described lower skid is made up of abrasive rubber material.
4. a kind of brake gear be arranged in 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 up of 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 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103623582A CN103623582A (en) | 2014-03-12 |
| CN103623582B true 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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| Country | Link |
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| CN (1) | CN103623582B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
Family Cites Families (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 |
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- 2013-11-13 CN CN201310575094.0A patent/CN103623582B/en active Active
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| CN103623582A (en) | 2014-03-12 |
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