CN2835699Y - a liquid gas buffer - Google Patents
a liquid gas buffer Download PDFInfo
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- CN2835699Y CN2835699Y CN 200420108483 CN200420108483U CN2835699Y CN 2835699 Y CN2835699 Y CN 2835699Y CN 200420108483 CN200420108483 CN 200420108483 CN 200420108483 U CN200420108483 U CN 200420108483U CN 2835699 Y CN2835699 Y CN 2835699Y
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Abstract
Description
技术领域 本实用新型一种液气缓冲器属于起重、装卸机械、电梯和矿车的安全装置领域。Technical field The utility model relates to a liquid-gas buffer, which belongs to the field of safety devices for hoisting, loading and unloading machinery, elevators and mine cars.
背景技术 目前,液气缓冲器有如下几种形式:1、依靠缓冲芯棒与活塞之间的间隙量来进行缓冲。这样一方面对缓冲芯棒加工、安装有严格的要求,一方面设计困难。2、依靠缸筒内密布的缓冲小孔来进行缓冲。同样具有设计困难,很难准确计算各孔的大小和分布,另外缓冲特性不可调整。Background technology At present, there are several types of liquid-gas buffers: 1. Buffering depends on the gap between the buffer mandrel and the piston. In this way, on the one hand, there are strict requirements on the processing and installation of the buffer mandrel, and on the other hand, the design is difficult. 2. Rely on the dense buffer holes in the cylinder for buffering. It is also difficult to design, it is difficult to accurately calculate the size and distribution of each hole, and the cushioning characteristics cannot be adjusted.
发明内容 本实用新型的目的是为了克服现有相关液气缓冲器的不足,提供了一种依靠节流阀进行缓冲的液气缓冲器,缓冲器具有液体腔和气体腔两个腔。更好地改善了缓冲性能,使缓冲特性更合理,且回弹力很小。构造新颖、结构简单、工艺性好、缓冲特性好。SUMMARY OF THE INVENTION The purpose of this utility model is to overcome the shortcomings of the existing related liquid-gas buffers, and provide a liquid-gas buffer that relies on a throttle valve for buffering. The buffer has two chambers, a liquid chamber and a gas chamber. The cushioning performance is better improved, the cushioning characteristics are more reasonable, and the rebound force is small. The structure is novel, the structure is simple, the manufacturability is good, and the cushioning property is good.
本实用新型采用的技术方案是:一种液气缓冲器,它由装在活塞部件IV外面的缸筒部件I、装在活塞部件IV内部的节流阀II、装在活塞部件IV一端的活塞杆部件III和装在缸筒部件I一端的导向套部件V组成。缓冲器在缸体3内腔中充满液压油成为液体腔A,活塞筒17的右内腔充满氮气成为气体腔B,气体腔B在液体腔A的右面。The technical scheme adopted in the utility model is: a liquid-gas buffer, which consists of a cylinder part I installed outside the piston part IV, a throttle valve II installed inside the piston part IV, and a piston installed at one end of the piston part IV. The rod part III is composed of a guide sleeve part V mounted on one end of the cylinder part I. The buffer is filled with hydraulic oil in the inner chamber of the cylinder body 3 to form a liquid chamber A, and the right inner chamber of the
缸筒部件I由缸体3和安装在缸体3左端中心孔内的螺塞1和密封圈2组成;装在缸体3内腔中的活塞杆部件III由节流阀II、导向环6、密封圈7、活塞筒17、气阀18组成;导向环6和密封圈7分别安装在活塞筒17左部外圆柱面的两个环槽内,气阀18装在活塞筒17的右上端;装在活塞杆部件III左端的节流阀II由阀座4、阀芯5、碟簧9、阀体8组成;阀心5前部为圆锥状插在阀座4中,后部为柱状,碟簧9安装在阀心5后部,阀座4和阀心5装在阀体8内,阀体8装在活塞筒17的左部内腔中,靠螺纹固定在活塞筒17头部上;装在活塞筒17内的活塞部件IV由密封圈10、导向环11、活塞体12组成;导向环11和密封圈10分别装在活塞体12上;导向套部件V由导向环13、导向套14、防尘圈16组成,导向环13、防尘圈16安装在导向套14上,导向套14用螺栓15固定在缸体3上;见附图1。Cylinder part I is composed of cylinder body 3, screw plug 1 and sealing ring 2 installed in the center hole of the left end of cylinder body 3; piston rod part III installed in the inner cavity of cylinder body 3 is composed of throttle valve II,
本实用新型的有益效果:由于采用节流阀,可使缓冲性能随碟簧的调节而调整。在缓冲结束后可使缓冲器无回弹力,使缓冲特性更合理。构造简单。使用面广。可用于起重机械、装卸机械、电梯和矿车运行碰撞时缓冲冲击。The beneficial effects of the utility model: due to the adoption of the throttle valve, the cushioning performance can be adjusted with the adjustment of the disc spring. After the end of buffering, the buffer can be made without resilience, so that the buffering characteristics are more reasonable. The structure is simple. It is widely used. It can be used to cushion the impact of hoisting machinery, loading and unloading machinery, elevators and mining vehicles when they collide.
附图说明 图1-液气缓冲器的剖视图;图中:I.缸筒部件,II.节流阀,III.活塞杆部件,IV.活塞部件,V.导向套部件1.螺塞,2.密封圈,3.缸体,4.阀座,5.阀芯,6.导向环,7.密封圈,8.阀体,9.碟簧,10.密封圈,11.导向环,12.活塞,13.导向环,14.导向套,15.螺杆,16.防尘圈,17.活塞杆,18.气阀,A.油腔,B.气腔。Description of the drawings Figure 1 - Sectional view of the liquid-gas buffer; in the figure: I. Cylinder part, II. Throttle valve, III. Piston rod part, IV. Piston part, V. Guide sleeve part 1. Screw plug, 2 .Seal ring, 3. Cylinder body, 4. Valve seat, 5. Valve core, 6. Guide ring, 7. Seal ring, 8. Valve body, 9. Disc spring, 10. Seal ring, 11. Guide ring, 12 .Piston, 13. Guide ring, 14. Guide sleeve, 15. Screw, 16. Dust ring, 17. Piston rod, 18. Air valve, A. Oil chamber, B. Air chamber.
具体实施方式 以附图为例说明具体实施方式:使用时,当液气缓冲器的活塞杆部件III的外端受到撞击力时,活塞杆17向缸筒I内的油腔运动,压缩油腔,这时油腔在受外力的作用下油压急剧升高,液压油在高压作用下把节流阀II的阀芯5打开,液压油通过节流阀II进入活塞杆17内腔,推动活塞杆内的活塞12,压缩气腔,使撞击时的机械能变为液压油和气体的热能,从而起到缓冲撞击的作用。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT Take the attached drawings as an example to illustrate the specific implementation: when in use, when the outer end of the piston rod part III of the liquid-pneumatic buffer is subjected to an impact force, the
当撞击力比较小时或撞击速度比较小时,撞击的能量不足以把节流阀II的阀芯5打开,这时液压油通过阀芯5和阀座4之间的小间隙进入活塞杆17内腔,压缩气腔,从而起到缓冲作用。当撞击力比较大时,大的撞击能量把节流阀II的阀芯5打开,液压油通过阀芯5与阀座4之间的大间隙进入活塞杆17内腔,压缩气腔,从而缓解了撞击猛烈时的峰值,改善了缓冲特性,使之更为合理。当缓冲结束后,节流阀关闭,关闭后节流阀的阀芯与阀座间的间隙很小,液压油在压缩气体的作用下,经该小间隙流回液体腔。使缓冲器回复原样。由于回复时,阀芯与阀座间的间隙很小,所以,回复油很少,从而使回弹力很小,可称为无回弹缓冲器。When the impact force is relatively small or the impact speed is relatively small, the energy of the impact is not enough to open the
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420108483 CN2835699Y (en) | 2004-10-22 | 2004-10-22 | a liquid gas buffer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420108483 CN2835699Y (en) | 2004-10-22 | 2004-10-22 | a liquid gas buffer |
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| CN2835699Y true CN2835699Y (en) | 2006-11-08 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN 200420108483 Expired - Fee Related CN2835699Y (en) | 2004-10-22 | 2004-10-22 | a liquid gas buffer |
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Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100430622C (en) * | 2007-02-06 | 2008-11-05 | 南京航空航天大学 | Aircraft Landing Gear Buffers with Internal Throttles |
| RU2405981C1 (en) * | 2009-06-25 | 2010-12-10 | Федеральное казенное предприятие "Научно-испытательный центр ракетно-космической промышленности" | Method for testing hydraulic buffer of launching site with imitation of natural loading conditions |
| CN102042360A (en) * | 2010-12-27 | 2011-05-04 | 四川川南减震器集团有限公司 | Shock-absorbing device |
| CN102454740A (en) * | 2010-10-15 | 2012-05-16 | Y.S.S.泰国有限公司 | shock absorber using gas pressure |
| CN102518618A (en) * | 2011-12-27 | 2012-06-27 | 山东天一液压科技股份有限公司 | Hydraulic cylinder |
| CN102518619A (en) * | 2011-12-27 | 2012-06-27 | 山东天一液压科技股份有限公司 | Elastic buffering hydraulic cylinder |
| CN104019174A (en) * | 2014-06-18 | 2014-09-03 | 姜雨 | High-pressure sealed nitrogen spring |
| CN106015428A (en) * | 2016-07-18 | 2016-10-12 | 天津优瑞纳斯液压机械有限公司 | Hydraulic buffering device used for hydraulic buffering car stop |
| CN106286674A (en) * | 2015-06-05 | 2017-01-04 | 哈尔滨飞机工业集团有限责任公司 | A kind of autonomous retractable landing gear buffer |
| CN106742079A (en) * | 2016-12-29 | 2017-05-31 | 北京空间机电研究所 | A kind of reusable landing buffer device of carrier rocket |
| CN107956834A (en) * | 2017-12-27 | 2018-04-24 | 山东科技大学 | A kind of combined type multi-cylinder linkage buffer and its application |
| CN110886803A (en) * | 2019-11-29 | 2020-03-17 | 中国北方车辆研究所 | Single-cylinder type hydro-pneumatic spring |
| CN111503206A (en) * | 2020-06-10 | 2020-08-07 | 江阴市洪腾机械有限公司 | Liquid-gas composite buffer |
| CN114370475A (en) * | 2022-01-14 | 2022-04-19 | 中国北方车辆研究所 | Built-in air chamber balance hydro-pneumatic suspension |
-
2004
- 2004-10-22 CN CN 200420108483 patent/CN2835699Y/en not_active Expired - Fee Related
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100430622C (en) * | 2007-02-06 | 2008-11-05 | 南京航空航天大学 | Aircraft Landing Gear Buffers with Internal Throttles |
| RU2405981C1 (en) * | 2009-06-25 | 2010-12-10 | Федеральное казенное предприятие "Научно-испытательный центр ракетно-космической промышленности" | Method for testing hydraulic buffer of launching site with imitation of natural loading conditions |
| CN102454740A (en) * | 2010-10-15 | 2012-05-16 | Y.S.S.泰国有限公司 | shock absorber using gas pressure |
| CN102042360A (en) * | 2010-12-27 | 2011-05-04 | 四川川南减震器集团有限公司 | Shock-absorbing device |
| CN102518618A (en) * | 2011-12-27 | 2012-06-27 | 山东天一液压科技股份有限公司 | Hydraulic cylinder |
| CN102518619A (en) * | 2011-12-27 | 2012-06-27 | 山东天一液压科技股份有限公司 | Elastic buffering hydraulic cylinder |
| CN104019174A (en) * | 2014-06-18 | 2014-09-03 | 姜雨 | High-pressure sealed nitrogen spring |
| CN106286674A (en) * | 2015-06-05 | 2017-01-04 | 哈尔滨飞机工业集团有限责任公司 | A kind of autonomous retractable landing gear buffer |
| CN106286674B (en) * | 2015-06-05 | 2018-08-24 | 哈尔滨飞机工业集团有限责任公司 | A kind of autonomous retractable landing gear buffer |
| CN106015428A (en) * | 2016-07-18 | 2016-10-12 | 天津优瑞纳斯液压机械有限公司 | Hydraulic buffering device used for hydraulic buffering car stop |
| CN106742079A (en) * | 2016-12-29 | 2017-05-31 | 北京空间机电研究所 | A kind of reusable landing buffer device of carrier rocket |
| CN106742079B (en) * | 2016-12-29 | 2019-04-09 | 北京空间机电研究所 | A reusable landing buffer for a launch vehicle |
| CN107956834A (en) * | 2017-12-27 | 2018-04-24 | 山东科技大学 | A kind of combined type multi-cylinder linkage buffer and its application |
| CN110886803A (en) * | 2019-11-29 | 2020-03-17 | 中国北方车辆研究所 | Single-cylinder type hydro-pneumatic spring |
| CN111503206A (en) * | 2020-06-10 | 2020-08-07 | 江阴市洪腾机械有限公司 | Liquid-gas composite buffer |
| CN114370475A (en) * | 2022-01-14 | 2022-04-19 | 中国北方车辆研究所 | Built-in air chamber balance hydro-pneumatic suspension |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |