CN104535101A - Damping slide block device for high-speed rocket sled test - Google Patents

Damping slide block device for high-speed rocket sled test Download PDF

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Publication number
CN104535101A
CN104535101A CN201410692769.4A CN201410692769A CN104535101A CN 104535101 A CN104535101 A CN 104535101A CN 201410692769 A CN201410692769 A CN 201410692769A CN 104535101 A CN104535101 A CN 104535101A
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cushion blocking
hole
housing
connecting hole
boxlike cavity
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CN201410692769.4A
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CN104535101B (en
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余元元
龚明生
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AVIC Aerospace Life Support Industries Ltd
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AVIC Aerospace Life Support Industries Ltd
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Abstract

The invention discloses a damping slide block device for high-speed rocket sled test. The damping slide block device comprises a slide block body and a damping mechanism. The slide block body comprises a box-type cavity, the center of the box type cavity is provided with a positioning boss, and the sidewalls of the box-type cavity are provided with lateral connection holes. The damping mechanism is mounted in the box-type cavity, and comprises a casing, a vertical damping assembly, a course damping pad and a lateral damping pad, the center of the casing is provided with a positioning hole, the sidewalls of the casing are provided with kidney-shaped connecting holes, the casing is vertically provided with through holes, the vertical damping assembly is mounted in the through holes, the course damping pad is mounted between the outer wall, along the direction vertical to a slide rail, of the casing and the box-type cavity, and the lateral damping pad is mounted between the outer wall along the slide rail direction of the casing and the box type cavity. The damping slide block device can damp vibration of a rocket sled in three coordinate directions to provide a proper environment for rocket sled test.

Description

For the vibration damping slide block device of high-speed rocket sledge test
Technical field
The invention belongs to high-speed rocket sledge sled test technical field, be specifically related to a kind of vibration damping slide block device for the test of high-speed rocket sledge.
Background technology
Rocket sledge sled test is the one very effective ground dynamic test between testing laboratory and full-scale flight test, this test method possesses full-scale dynamic test ability with it, testpieces quality and size are restricted hardly, test speed and overload level are greatly with efficient, safety, repeatable high, the excellent feature of economy, become the new theory identifying various weaponry, new technology, new material and the requisite testing equipment of new construction, aviation, space flight, weapons, electronics, the specialty such as nuclear weapon more and more brings rocket sled track test into fundamental test means in.
Slide block is the key member of rocket sledge, rocket sledge runs along rail high speed by means of the slide block be fastened on slide rail rail head, slide block should fasten track, rocket sledge is made to have the movement locus determined, do not depart from slide rail, keep certain interval again and between the rail head of track, slide block is passed through smoothly.This fastening structure just, makes slide block can by load such as suffered huge aerodynamic force, motor power, damping force during rocket sledge high-speed cruising, and the shock and vibration produced due to these load instability is delivered on slide rail; Simultaneously also can by can not be definitely smooth-going due to slide rail, when causing high-speed cruising, because the random shock that contacts, rub and collide and produce and vibration passing are to rocket sledge between slide block with track.Therefore slide block not only serves the effect of transmitted load between slide rail and rocket sledge, self also needs to have the good rigidity of structure and intensity simultaneously.Traditional slide block is generally designed to have stronger rigid structure, and slide block is connected with car body also to adopt and is rigidly connected.
But along with weaponry is to development that is high-speed, high-power and high-level efficiency direction, the impact of mechanical vibration on the quality of product, performance and the market competitiveness is increasing.The Design and manufacture of product plays conclusive effect to its dynamic property, product also needs on-line monitoring, the at any time Dynamic controlling such as tracing trouble and on-call maintenance when using, this just requires the test environment that Rocket sled test can provide the tests such as similar guided missile suitable, accelerating curve can be designed to approach the overload curves in practical flight as far as possible, and vibration environment is substantially close to the magnitude of practical flight in test.
The dynamic load that slide block and rail interaction produce, sharply increases along with the raising of Rocket sled test speed, on traditional testpieces that this forced vibration can be directly delivered to and rocket sledge carries of being rigidly connected.Therefore, under Rocket sled test environment, usual the born dynamic load of flight test exemplar may than more severe under free flight mode of operation.For high-speed test (HST), because the magnitude of vibration is excessive, be often difficult to meet the requirement of testpieces to vibration environment.Therefore, pursue simply slide block stiffness this for time design viewpoint very of a specified duration need to be reconsidered.
The many employings of traditional vibration reducing measure are requiring the mode of higher testpieces or core component junction mounting dampers wherein to vibration environment, when testpieces size and weight are comparatively large, be often difficult to realize when the installing space around core component is not enough.Simultaneously in order to the integrality of warranty test part, vibration damper is often arranged on its outside, the construction weight of rocket sledge and physical dimension are increased more, the thrust of rocket sledge engine and aerodynamic configuration are had higher requirement, causes the significantly raising of design difficulty and implementation cost.
Summary of the invention
The object of the present invention is to provide a kind of vibration damping slide block device for the test of high-speed rocket sledge, it not only has the good rigidity of structure and intensity, to bear and to transmit the various load in high-speed test (HST) process, also with between rocket sledge car body adopt and flexibly connect simultaneously, vibration damping can be carried out to rocket sledge, to provide suitable Rocket sled test test environment on three coordinate directions.
The technical solution adopted for the present invention to solve the technical problems is:
There is provided a kind of vibration damping slide block device for the test of high-speed rocket sledge, this device comprises:
Slider body, described slider body comprises the chute be connected with slide rail, the boxlike cavity being arranged on described chute top, and the central authorities of described boxlike cavity are provided with positioning boss, and any two sidewalls paralleled of described boxlike cavity are respectively equipped with multiple sides connecting hole;
Damper mechanism, described damper mechanism is arranged in boxlike cavity, described damper mechanism comprises housing, vertical damping assembly, course cushion blocking and side direction cushion blocking, the central authorities of described housing are provided with pilot hole, the bottom of described pilot hole and positioning boss recessed bond ing, top and the register pin of described pilot hole are slidably connected, described register pin is fixedly connected with rocket sledge car body, the sidewall of described housing is provided with the multiple kidney-shaped connecting holes corresponding with described multiple sides connecting hole, described kidney-shaped connecting hole is connected with side connecting hole by sliding axle, described kidney-shaped connecting hole can do course or sideway movement on sliding axle, described housing is vertically provided with multiple through hole, described vertical damping assembly is installed in described through hole, the bottom of described vertical damping assembly is fixedly connected with through hole, the top of described vertical damping assembly is stretched out through hole and is fixedly connected with rocket sledge car body, described course cushion blocking is arranged on described housing along between the outer wall and the inwall of boxlike cavity in vertical slide rail direction, described side direction cushion blocking is arranged on described housing along between the outer wall and the inwall of boxlike cavity in slide rail direction.
By technique scheme, described vertical damping assembly comprises the end cap placed successively from bottom to up, lower cushion blocking, T-shaped axle and upper cushion blocking, described end cap is fixedly connected with the bottom of through hole, described lower cushion blocking is placed on end cap, described T-shaped axle comprises supporting plate and vertical pivot, described supporting plate is placed on lower cushion blocking, and described upper cushion blocking is sleeved on vertical pivot, and the top that described vertical pivot stretches out through hole is threaded with rocket sledge car body.
By technique scheme, the surrounding inwall of described boxlike cavity is provided with convex tendon, and described convex tendon is provided with the inner side connecting hole corresponding with described multiple sides connecting hole.
By technique scheme, the shape of described housing is groined type.
By technique scheme, this device also comprises upper cover plate, and described upper cover plate is fixedly mounted on the top of boxlike cavity.
By technique scheme, between the bottom of described housing and boxlike cavity, between described housing and upper cover plate, be respectively equipped with gap.
By technique scheme, the top of described housing is also provided with multiple square hole.
By technique scheme, upper cushion blocking, lower cushion blocking, course cushion blocking and side direction cushion blocking are wire gauze or rubber blanket.
The beneficial effect that the present invention produces is: damper mechanism is arranged in slider body by this device, the integrated design of both realizations, construction weight and the physical dimension of rocket sledge can be reduced, when rocket sledge generation vertical motion, rocket sledge car body is because being fixedly connected with vertical damping assembly, and be slidably connected by register pin and housing, therefore the object of vertical vibration damping is reached by vertical damper mechanism, when there is course or lateral vibration in rocket sledge, because housing is connected with sliding axle by kidney-shaped connecting hole, and pilot hole and positioning boss recessed bond ing, therefore housing can be driven by kidney-shaped connecting hole along the axis of sliding axle or move radially, realize the course of housing or be displaced sideways, in the process of movement, housing can compress course cushion blocking or side direction cushion blocking, reach the object of course or side direction vibration damping.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the invention will be further described, in accompanying drawing:
Fig. 1 is the structural representation of the embodiment of the present invention;
Fig. 2 is the cut-open view along A-A line in Fig. 1;
Fig. 3 is the cut-open view along B-B line in Fig. 1;
Fig. 4 is the exploded perspective view of the embodiment of the present invention;
Fig. 5 is the structural representation of slider body;
Fig. 6 is the exploded perspective view of damper mechanism.
Wherein: 9-chute, 10-boxlike cavity, 11-upper cover plate, 12-register pin, 13-sliding axle, 14-damper mechanism, 15-bolt, the vertical damping assembly of 16-, 17-course cushion blocking, 18-side direction cushion blocking, 19-convex tendon, connecting hole inside 20-, the upper connecting hole of 21-, 22-side connecting hole, 23-positioning boss, the upper cushion blocking of 24-, 25-T shape coupling shaft, 2501-supporting plate, 2502-vertical pivot, cushion blocking under 26-, 27-end cap, 28-kidney-shaped connecting hole, 29-square hole, 30-through hole, 31-positioning round table, 32-pilot hole, 33-housing.
Embodiment
In order to make object of the present invention, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the present invention is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the present invention, be not intended to limit the present invention.
As shown in figs 1 to 6, a kind of vibration damping slide block device for the test of high-speed rocket sledge, this device comprises:
Slider body, as shown in Figure 5, slider body comprises the chute 9 be connected with slide rail, the boxlike cavity 10 being arranged on chute 9 top, and the central authorities of boxlike cavity 10 are provided with positioning boss 23, and any two sidewalls paralleled of boxlike cavity 10 are respectively equipped with multiple sides connecting hole 22;
Damper mechanism 14, as shown in Figure 1, damper mechanism 14 is arranged in boxlike cavity 10, as Fig. 2, shown in Fig. 6, damper mechanism 14 comprises housing 33, vertical damping assembly 16, course cushion blocking 17 and side direction cushion blocking 18, the central authorities of housing 33 are provided with pilot hole 32, the bottom of pilot hole 32 and positioning boss 23 recessed bond ing, top and the register pin 12 of pilot hole 32 are slidably connected, register pin 12 is fixedly connected with rocket sledge car body, the sidewall of housing 33 is provided with the multiple kidney-shaped connecting holes 28 corresponding with multiple sides connecting hole 22, kidney-shaped connecting hole 28 is connected with side connecting hole 22 by sliding axle 13, kidney-shaped connecting hole 28 can do course or sideway movement on sliding axle 13, housing 33 is vertically provided with multiple through hole 30, vertical damping assembly 16 is installed in through hole 30, the bottom of vertical damping assembly 16 is fixedly connected with through hole 30, the top of vertical damping assembly 16 is stretched out through hole 30 and is fixedly connected with rocket sledge car body, course cushion blocking 17 is arranged on housing 33 along between the outer wall and the inwall of boxlike cavity 10 in vertical slide rail direction, side direction cushion blocking 18 is arranged on housing 33 along between the outer wall and the inwall of boxlike cavity 10 in slide rail direction.
In a preferred embodiment of the invention, as shown in Fig. 3, Fig. 6, vertical damping assembly 16 comprises end cap 27, lower cushion blocking 26, T-shaped axle 25 and the upper cushion blocking 24 placed successively from bottom to up, end cap 27 is fixedly connected with the bottom of through hole 30, lower cushion blocking 26 is placed on end cap 27, and T-shaped axle 25 comprises supporting plate 2501 and vertical pivot 2502, and supporting plate 2501 is placed on lower cushion blocking 26, upper cushion blocking 24 is sleeved on vertical pivot 2502, and the top that vertical pivot 2502 stretches out through hole 30 is threaded with rocket sledge car body.
In a preferred embodiment of the invention, as shown in Figure 5, the surrounding inwall of boxlike cavity 10 is provided with convex tendon 19, convex tendon 19 is provided with the inner side connecting hole 20 corresponding with multiple sides connecting hole 22, during installation, sliding axle 13 is arranged on side connecting hole 22 and inner side connecting hole 20, can increase the intensity of boxlike cavity.
In a preferred embodiment of the invention, as shown in Figure 6, the shape of housing 33 is groined type, can alleviate the weight of housing.
In a preferred embodiment of the invention, as Figure 1-Figure 4, this device also comprises upper cover plate 11, and upper cover plate 11 is fixedly mounted on the top of boxlike cavity 10, concrete, upper cover plate 11 be arranged on by bolt 15 be opened in convex tendon 19 top upper connecting hole 21 in.Rupture once the excessive sliding axle that causes of vertical load, upper cover plate 11 can prevent damper mechanism 14 from deviating from boxlike cavity 10, ensures security.
In a preferred embodiment of the invention, as shown in Figure 3, Figure 4, gap is respectively equipped with between the bottom of housing 33 and boxlike cavity 10, between housing 33 and upper cover plate 11, when vertical load is excessive cause sliding axle 13 to be out of shape time, can avoid colliding between the bottom of damper mechanism 14 and boxlike cavity 10 or upper cover plate 11.
In a preferred embodiment of the invention, as shown in Figure 6, the top of housing 33 is also provided with multiple square hole 29, not only can alleviate the weight of this device, can also be used for sensor installation.
In a preferred embodiment of the invention, upper cushion blocking 24, lower cushion blocking 26, course cushion blocking 17 and side direction cushion blocking 18 is wire gauze or rubber blanket, these cushion blockings also can adopt other form as required, and its concrete technical parameter should carry out designing and adjusting according to the natural mode of vibration of rocket sledge, trystate and vibration environment etc.
As shown in figs 1 to 6, principle of work of the present invention is: this device by installing damper mechanism 14 in slider body, the integrated design of both realizations, construction weight and the physical dimension of rocket sledge can be reduced, damper mechanism 14 is respectively equipped with cushion blocking at three change in coordinate axis direction, when rocket sledge car body is when being connected with this device, the pre compressed magnitude of damper mechanism on three change in coordinate axis direction should be ensured, in order to avoid when unidirectional side is compressed, opposite side leaves larger gap, under vibration to when having clearance side to move, there is larger impact, reduce effectiveness in vibration suppression, in addition, resilience can be there is and fill up gap in reserved decrement when there is gap,
When rocket sledge generation vertical motion, because rocket sledge car body is threaded with the vertical pivot 2502 of T-shaped axle 25, vertical pivot 2502 is stepped form, top is screw rod, bottom is polished rod, and rocket sledge car body is slidably connected by register pin 12 and housing 33, so rocket sledge car body by the lower cushion blocking 26 of the supporting plate 2501 of T-shaped axle 25 extruding downwards, or can upwardly go up cushion blocking 24, reach the object of vertical vibration damping;
When there is course or lateral vibration in rocket sledge, register pin 12 is fixedly connected with rocket sledge car body, can be specifically that both adopt interference fit, to bear the oscillating load in course and side direction, T-shaped axle 25 is made not bear course and side load, because housing 33 is connected with sliding axle 13 by kidney-shaped connecting hole 28, and pilot hole 32 and positioning boss 23 recessed bond ing, therefore rocket sledge car body can drive housing 33 by kidney-shaped connecting hole 28 along the axis of sliding axle 13 or move radially, realize the course of housing 33 or be displaced sideways, in the process of movement, housing 33 can compress course cushion blocking 17 or side direction cushion blocking 18, reach the object of course or side direction vibration damping.
The present invention is when embody rule, as shown in Figure 5, slider body upper design becomes a boxlike cavity 10, appropriate cavities 10 both sides parallel with slide rail are provided with three row for installing the side connecting hole 22 of sliding axle 13, the inwall surrounding of boxlike cavity 10 is provided with eight convex tendons 19, the top of convex tendon 19 is provided with connecting hole 21, upper connecting hole 21 is for installing cover plate 11, the side of convex tendon is provided with inner side connecting hole 20, inner side connecting hole 20 is for installing sliding axle 13, the central authorities of boxlike cavity 10 are provided with positioning boss 23, positioning boss 23 is also provided with the inner side connecting hole 20 for installing sliding axle 13,
As Figure 1-Figure 4, the damper mechanism 14 of " well " font is installed in boxlike cavity 10, as shown in Figure 6, damper mechanism 14 comprises housing 33, vertical damping assembly 16, course cushion blocking 17 and side direction cushion blocking 18, housing 33 both sides are processed with three row kidney-shaped connecting holes 28, housing 33 top is designed with four columniform through holes 30 at " well " font four infalls, the T-shaped axle 25 of vertical damping assembly 16 passes from through hole 30, the centre of housing 33 is provided with positioning round table 31, positioning round table 31 is for installing cover plate 11, the centre of positioning round table 31 machined the pilot hole 32 installing register pin 12, the middle upper cushion blocking 24 having through hole is installed in the top of T-shaped axle 25, lower cushion blocking 26 is installed in bottom, the bottom of through hole 30 to be spirally connected sealing with end cap 27,
As Figure 1-Figure 4, during installation, sliding axle 13 connects 20 and kidney-shaped connecting hole 28 through connecting hole 22, inner side, damper mechanism 14 is arranged on boxlike cavity 10, sliding axle can be a major axis running through boxlike cavity and arrange, also the semiaxis between boxlike cavity wall and its central authorities can be mounted in, damper mechanism 14 leaves enough gaps with the wall of boxlike cavity 10, and the gap location between eight flanges and boxlike cavity 10 wall of the front, rear, left and right of " well " font damper mechanism 14 is provided with course cushion blocking 17 and side direction cushion blocking 18.
The present invention is by damper mechanism and slider body Integrated design, effectively reduce physical dimension, reduce system weight, there is compact conformation, lightweight feature, vibration damping can also be carried out to rocket sledge on three of a coordinate system direction, the present invention is requiring on very harsh rocket sledge to vibration environment, can as one-level vibration insulating system, combinationally use with traditional vibration absorber, the present invention can be used as the general module of supersonic rocket sledge, have good transplantability, its cushion blocking can customize by the natural mode of vibration of different rocket sledge and actual user demand.
Should be understood that, for those of ordinary skills, can be improved according to the above description or convert, and all these improve and convert the protection domain that all should belong to claims of the present invention.

Claims (8)

1., for a vibration damping slide block device for high-speed rocket sledge test, it is characterized in that, this device comprises:
Slider body, described slider body comprises the chute (9) be connected with slide rail, the boxlike cavity (10) being arranged on described chute (9) top, the central authorities of described boxlike cavity (10) are provided with positioning boss (23), and any two sidewalls paralleled of described boxlike cavity (10) are respectively equipped with multiple sides connecting hole (22);
Damper mechanism (14), described damper mechanism (14) is arranged in boxlike cavity (10), described damper mechanism (14) comprises housing (33), vertical damping assembly (16), course cushion blocking (17) and side direction cushion blocking (18), the central authorities of described housing (33) are provided with pilot hole (32), the bottom of described pilot hole (32) and positioning boss (23) recessed bond ing, top and the register pin (12) of described pilot hole (32) are slidably connected, described register pin (12) is fixedly connected with rocket sledge car body, the sidewall of described housing (33) is provided with the multiple kidney-shaped connecting holes (28) corresponding with described multiple sides connecting hole (22), described kidney-shaped connecting hole (28) is connected with side connecting hole (22) by sliding axle (13), described kidney-shaped connecting hole (28) can do course or sideway movement on sliding axle (13), described housing (33) is vertically provided with multiple through hole (30), described vertical damping assembly (16) is installed in described through hole (30), the bottom of described vertical damping assembly (16) is fixedly connected with through hole (30), the top of described vertical damping assembly (16) is stretched out through hole (30) and is fixedly connected with rocket sledge car body, described course cushion blocking (17) is arranged on described housing (33) along between the outer wall and the inwall of boxlike cavity (10) in vertical slide rail direction, described side direction cushion blocking (18) is arranged on described housing (33) along between the outer wall and the inwall of boxlike cavity (10) in slide rail direction.
2. device according to claim 1, it is characterized in that, described vertical damping assembly (16) comprises the end cap (27) placed successively from bottom to up, lower cushion blocking (26), T-shaped axle (25) and upper cushion blocking (24), described end cap (27) is fixedly connected with the bottom of through hole (30), described lower cushion blocking (26) is placed on end cap (27), described T-shaped axle (25) comprises supporting plate and vertical pivot, described supporting plate is placed on lower cushion blocking (26), described upper cushion blocking (24) is sleeved on vertical pivot, the top that described vertical pivot stretches out through hole (30) is threaded with rocket sledge car body.
3. device according to claim 1, is characterized in that, the surrounding inwall of described boxlike cavity (10) is provided with convex tendon (19), and described convex tendon (19) is provided with the inner side connecting hole (20) corresponding with described multiple sides connecting hole (22).
4. device according to claim 1, is characterized in that, the shape of described housing (33) is groined type.
5. device according to claim 1, is characterized in that, this device also comprises upper cover plate (11), and described upper cover plate (11) is fixedly mounted on the top of boxlike cavity (10).
6. device according to claim 5, is characterized in that, is respectively equipped with gap between the bottom of described housing (33) and boxlike cavity (10), between described housing (33) and upper cover plate (11).
7. device according to claim 1, is characterized in that, the top of described housing (33) is also provided with multiple square hole (29).
8. device according to claim 1, is characterized in that, described upper cushion blocking (24), lower cushion blocking (26), course cushion blocking (17) and side direction cushion blocking (18) are wire gauze or rubber blanket.
CN201410692769.4A 2014-11-26 2014-11-26 damping slide block device for high-speed rocket sled test Active CN104535101B (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105424071A (en) * 2015-12-12 2016-03-23 航宇救生装备有限公司 Novel rocket sled damping device
CN111536196A (en) * 2020-05-21 2020-08-14 中国航天科工飞航技术研究院(中国航天海鹰机电技术研究院) Landing buffering vibration damper and high-speed magnetic suspension equipment
CN112504600A (en) * 2020-11-30 2021-03-16 中国工程物理研究院总体工程研究所 Guide sliding shoe of rocket sled

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4283053A (en) * 1977-05-13 1981-08-11 Herman Parker Air powered rocket sled game
US6056238A (en) * 1994-08-26 2000-05-02 Northrop Grumman Corporation Supersonic ground vehicle
WO2002004838A1 (en) * 2000-07-12 2002-01-17 Sealy Technology Llc Composite material spring modules for cushions
CN1718962A (en) * 2005-07-01 2006-01-11 河北理工大学 Tridimensional vibration isolation device
CN200975036Y (en) * 2006-10-13 2007-11-14 北京工业大学 Bidirectional shearing type vibrating device
CN102072830A (en) * 2010-12-31 2011-05-25 航宇救生装备有限公司 Water brake system for rocket sled
CN202039470U (en) * 2011-04-24 2011-11-16 广州大学 Three-dimensional shock isolating and absorbing device
CN203729160U (en) * 2014-02-27 2014-07-23 青岛四方车辆研究所有限公司 Vibration attenuation composite spring absorber assembly for floating slab tracks

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4283053A (en) * 1977-05-13 1981-08-11 Herman Parker Air powered rocket sled game
US6056238A (en) * 1994-08-26 2000-05-02 Northrop Grumman Corporation Supersonic ground vehicle
WO2002004838A1 (en) * 2000-07-12 2002-01-17 Sealy Technology Llc Composite material spring modules for cushions
CN1718962A (en) * 2005-07-01 2006-01-11 河北理工大学 Tridimensional vibration isolation device
CN200975036Y (en) * 2006-10-13 2007-11-14 北京工业大学 Bidirectional shearing type vibrating device
CN102072830A (en) * 2010-12-31 2011-05-25 航宇救生装备有限公司 Water brake system for rocket sled
CN202039470U (en) * 2011-04-24 2011-11-16 广州大学 Three-dimensional shock isolating and absorbing device
CN203729160U (en) * 2014-02-27 2014-07-23 青岛四方车辆研究所有限公司 Vibration attenuation composite spring absorber assembly for floating slab tracks

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
丁春全等: "火箭橇试验减振系统力学仿真研究", 《舰船电子工程》 *
王云: "火箭橇试验滑轨的发展与展望", 《航空科学技术》 *
赵继波等: "火箭橇加载试验技术研究", 《爆炸与冲击》 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105424071A (en) * 2015-12-12 2016-03-23 航宇救生装备有限公司 Novel rocket sled damping device
CN111536196A (en) * 2020-05-21 2020-08-14 中国航天科工飞航技术研究院(中国航天海鹰机电技术研究院) Landing buffering vibration damper and high-speed magnetic suspension equipment
CN112504600A (en) * 2020-11-30 2021-03-16 中国工程物理研究院总体工程研究所 Guide sliding shoe of rocket sled
CN112504600B (en) * 2020-11-30 2022-09-27 中国工程物理研究院总体工程研究所 Guide sliding shoe of rocket sled

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