CN109211305A - High-speed ejection device for marble array - Google Patents

High-speed ejection device for marble array Download PDF

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Publication number
CN109211305A
CN109211305A CN201811121546.7A CN201811121546A CN109211305A CN 109211305 A CN109211305 A CN 109211305A CN 201811121546 A CN201811121546 A CN 201811121546A CN 109211305 A CN109211305 A CN 109211305A
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China
Prior art keywords
piston
piston cylinder
hoodle
cylinder
gun tube
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Application number
CN201811121546.7A
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Chinese (zh)
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CN109211305B (en
Inventor
徐小辉
李干
刘佳贵
宋春明
韦忠瑄
张中威
岳松林
程怡豪
马超
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Army Engineering University of PLA
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Army Engineering University of PLA
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01DMEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D21/00Measuring or testing not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F1/00Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

The invention discloses a marble array high-speed ejection device which comprises a pressurizing device, a piston cylinder, a first piston, an elastic piece, a first sealing ring, a second piston, a gun barrel, a diaphragm, a housing, marbles and a pressure relief switch, wherein the pressurizing device is arranged on the piston cylinder; the top end of the piston cylinder is connected with the gun barrel; the top end of the gun barrel is fixedly connected with a housing, a plurality of launching holes are formed in the housing, and marbles are filled in the launching holes; the second piston is arranged in the gun barrel; the diaphragm is arranged at the upper end of the gun barrel; the first piston is arranged in the piston cylinder; a spring is arranged at the lower end of the first piston, and a first sealing ring is arranged between the upper end of the first piston and the piston cylinder; the lower end of the first piston divides the inner cavity of the piston cylinder into an upper cavity and a lower cavity; the lower end of the first piston is provided with a vent hole which communicates the upper cavity with the lower cavity, and a first one-way valve is arranged in the vent hole; the pressurizing device is communicated with the lower cavity of the piston cylinder; the bottom of the piston cylinder is also connected with a pressure relief switch; the device can be used as an emitting device of an explosion source in a vacuum chamber explosion simulation test device.

Description

A kind of hoodle array high speed ejection device
Technical field
The invention belongs to explode and impact technology field, especially a kind of hoodle array high speed ejection device.
Background technique
Similar physics simulation experiment method is a kind of effective method of Study of The Underground explosion issues.In underground explosion effect In vacuum chamber simulator, quick-fried source is its core apparatus.In the underground explosion simulation test of big equivalent, existing quick-fried source model Using miniature medicine ball or cavity filled with high pressure gas is simulated, and the quick release of cavity high pressure gas is its key technology, In existing technology, external M.A.Sadovskii and V.V.Adushkin of Geophysics Institute of the former Soviet Union etc. earliest are learned Person simulates cavity using thin-walled rubber air bag built in spherical nickel filament metal grate, heats nickel filament by low-tension current to hardening crack Ball achievees the purpose that discharge compressed gas.But the heating time of the device nickel filament is uncontrollable, rubber pneumatic bag is likely to A breach randomly is opened from somewhere and causes the uneven of gas ejection, is not consistent with underground explosion physical process, to test simulation As a result it impacts;It is domestic earliest by engineering university of ground force blast impulse prevent and reduce natural disasters National Key Laboratory in document (Xu is small The contracting of brightness, the big equivalent Shallow-Embedded Under-Ground explosion throwing blast crater effect of the such as Qiu Yanyu, Wang Mingyang is more quick-fried than simulation test device development (J) It fries and flexibility is utilized using cloche simulated high-pressure cavity with report, quick-fried source device in impact, DOI:10.11883/bzycj) The method that the high-velocity wire fragment and shock wave that the explosion of primacord center generates carry out broken glass ball cover reaches quick release compression The purpose of gas, but due to needing using the hazardous explosion prones article such as electric cap, primacord in this method, to experimental condition requirement High, test safety, the feature of environmental protection be not high.Pneumatic mode is used to realize that hoodle array high speed ejection carrys out shattered glass cover with this to reach Device to quick release compressed gas not yet appears in the newspapers, and existing hoodle ejector has steam catapult, explosion ejector And Electromagnetical ejector, it is respectively the kinetic energy of ejection, these catapult-launching gear skills by steam thermal energy, chemistry of explosives energy and electromagnetic energy Art is complicated, is mainly used for the large-sized powers such as carrier-borne aircraft equipment.
Summary of the invention
The purpose of the present invention is to provide a kind of hoodle array high speed ejection devices, can be used as current vacuum room blast analogue The core component of quick-fried source device in experimental rig, achievees the purpose that high pressure gas quick release, to solve test safety and can The problem of operability.
The technical solution for realizing the aim of the invention is as follows:
A kind of hoodle array high speed ejection device, including pressurizing device, piston cylinder, first piston, elastic component, the first sealing Circle, second piston, gun tube, diaphragm, housing, hoodle, compression relief cock.
The piston cylinder top is equipped with through-hole, and through-hole is connected with gun tube, is connected inside gun tube bottom and piston cylinder;It is described Gun tube top is fixed with housing, and housing is equipped with multiple launch holes, is filled with hoodle in launch hole;The second piston setting exists In gun tube, it can be slided up and down in gun tube;The diaphragm is arranged in gun tube upper end, to be sealed to gun tube upper end;Described One piston is arranged in piston cylinder, can slide up and down in piston cylinder;The first piston vertical section is I-shaped;And lower end surface Area is greater than upper surface area;The first piston lower end is equipped with elastic component, and elastic component pushes up first piston upper end and work The contact of plug cylinder upper end inner wall, and the first sealing ring is equipped between first piston upper end and piston cylinder, the first sealing ring is to piston cylinder Top through-hole is sealed;Piston cylinder internal cavities are divided into upper and lower two cavitys by the first piston lower end;Described first Piston is equipped with venthole, and upper and lower cavity is connected to by venthole, and the first check valve, the first check valve are equipped in venthole Make gas that can only flow to upper plenum from lower cavity through venthole;The pressurizing device passes through the pipeline and piston cylinder of piston cylinder bottom Lower cavity be connected;The pipeline of the piston cylinder bottom is also connected with compression relief cock, to carry out to cavity gas under piston cylinder Pressure release.
Compared with prior art, the present invention its remarkable advantage:
(1) hoodle array high speed ejection device of the invention is driven using high pressure gas as driving source compared to explosive It is dynamic, the safety and the feature of environmental protection of test are improved, the experimental study for the development underground explosion effect of related fields provides pole Big convenience;
(2) hoodle array high speed ejection device of the invention, first piston act on high-speed motion in high pressure gas, work as diaphragm After rupture, achievees the effect that sealing embedded in gun tube upper end, so that only a small amount of high pressure gas acts on hoodle, avoid A large amount of high pressure gas enters housing in piston cylinder, so that the emission rate quantification of hoodle measures, improves experiment and surveys Measure accuracy;
(3) hoodle array high speed ejection device of the invention has high efficiency, low pollution, occupies little space, operation side Just, stabilized ejection, repeatability are good, require on-the-ground test condition relatively low.
Present invention is further described in detail with reference to the accompanying drawing.
Detailed description of the invention
Fig. 1 is hoodle array high speed ejection apparatus structure schematic diagram of the invention.
Fig. 2 is that enlarged diagram is connected at the top of gun tube.
Specific embodiment
In order to illustrate technical solution of the present invention and technical purpose, with reference to the accompanying drawing and specific embodiment is the present invention It is further to introduce.
In conjunction with Fig. 1, a kind of hoodle array high speed ejection device of the invention, including pressurizing device, piston cylinder 5, first are living Fill in 11, elastic component 6, the first sealing ring 12, second piston 13, gun tube 14, diaphragm 15, housing 17, hoodle 18, compression relief cock;
5 top of piston cylinder is equipped with through-hole, and through-hole is connected with gun tube 14, is connected inside 14 bottom of gun tube and piston cylinder 5 It is logical;14 top of gun tube is fixed with housing 17, and housing 17 is equipped with multiple launch holes, is filled with hoodle 18 in launch hole;Institute It states second piston 13 to be arranged in gun tube 14, can be slided up and down in gun tube 14;The diaphragm 15 setting in 14 upper end of gun tube, with 14 upper end of gun tube is sealed;The first piston 11 is arranged in piston cylinder 5, can slide up and down in piston cylinder 5;It is described 11 vertical section of first piston is I-shaped;And lower end surface area is greater than upper surface area;11 lower end of first piston is equipped with bullet Property part 6, elastic component 6 pushes up 11 upper end of first piston and contacts with 5 upper end inner wall of piston cylinder, and 11 upper end of first piston and work The first sealing ring 12 is equipped between plug cylinder 5, the first sealing ring 12 is sealed 5 top through-hole of piston cylinder;The first piston 5 internal cavities of piston cylinder are divided into upper and lower two cavitys by 11 lower ends;11 lower end of first piston is equipped with venthole 9, ventilation Hole 9 is connected to two cavitys up and down, and the first check valve 8 is equipped in venthole 9, and the first check valve 8 makes gas can only be from lower cavity Upper plenum is flowed to through venthole 9;The pressurizing device is connected by the pipeline of 5 bottom of piston cylinder with the lower cavity of piston cylinder 5, To be filled with high pressure gas to piston cylinder 5;The pipeline of 5 bottom of piston cylinder is also connected with compression relief cock, to the lower sky of piston cylinder 5 Chamber gas carries out pressure release.
Further, 11 lower end of first piston and 5 inner wall of piston cylinder cooperate, the first piston 11 and piston cylinder 5 Between be equipped with guiding mechanism, to guarantee sliding stability of the first piston 11 in piston cylinder 5.
As an implementation, the guiding mechanism is guide plate, and the guide plate 10 is fixed on the overhead of piston cylinder 5 Intracavitary, the guide plate 10 is equipped with pilot hole and multiple ventholes;Cooperate among the first piston 11 with pilot hole, it can edge Pilot hole slides up and down, and venthole is not separated with the upper plenum for guaranteeing piston cylinder 5 by guide plate 10.
Alternatively embodiment, the guiding mechanism are guide ring;The guide ring is arranged in 5 upper end of piston cylinder It is internal;Guide ring is axial axially coaxial with 5 upper end through-hole of piston cylinder;The 11 upper end outer wall of first piston and guide ring inner wall paste It closes, 11 upper end of first piston can slide up and down in guide ring.
In other embodiment, the guiding mechanism is guide rod, and the guide rod is arranged in 5 upper end of piston cylinder Inside has extended downwardly guide rod from 5 upper wall of piston cylinder, and 11 upper end of first piston is equipped with pilot hole, and pilot hole is located at Outside first sealing ring 12, the pilot hole of guide rod and first piston 11 cooperates, and first piston 11 can be slided up and down along guide rod.
Further, the pressurizing device includes high pressure gas cylinder 1, pressure reducing valve 2, second one-way valve 4;The high pressure gas cylinder 1 It is connected through pressure reducing valve 2 with second one-way valve 4, the second one-way valve 4 is connected with the pipeline of 5 bottom of piston cylinder.High pressure gas cylinder 1 High pressure gas is after the decompression of pressure reducing valve 2, by second one-way valve 4 to filling out high pressure gas in piston cylinder 5.
Further, the hoodle array high speed ejection device is additionally provided with pressure measuring unit, is filled out with accurately detecting pressurizing device The gas pressure filled.
In some embodiments, the pressure measuring unit is pressure gauge 3, and the escape pipe after pressure reducing valve 2 is arranged in pressure gauge 3 On.
In other embodiment, the pressure measuring unit is pressure sensor, and the pressure sensor setting is subtracting The pipeline of escape pipe, 5 bottom of piston cylinder after pressure valve 2 is connected with 5 internal cavities of piston cylinder.
Preferably, the compression relief cock includes solenoid valve 19, switch 20;The pipe of the solenoid valve 19 and 5 bottom of piston cylinder Road is connected;20 pairs of 19 power on/off of solenoid valve of the switch realize the releasing pressure automatically to gas in piston cylinder 5 by solenoid valve 19.
In conjunction with Fig. 2, further, the gun tube 14 is gradually reduced close to the upper end diameter of diaphragm or 14 upper end of gun tube is set The cone 16 for having upward diameter to be gradually reduced, when so that second piston 13 being moved upwards along gun tube 14, second piston 13 is due to height After speed moves across diaphragm 15, the high pressure gas of 13 bottom of second piston is avoided to reach sealing effect embedded in 14 upper end of gun tube Body enters in housing 17, to have an impact to test environment parameter, so that the emission rate quantification of hoodle 18 measures, mentions High experiment measurement accuracy.
Further, 5 bottom of piston cylinder is detachable structure, and to dismantle installation, 5 bottom of piston cylinder is equipped with Capping is equipped with the second sealing ring 29 and is sealed between capping and cylinder body.
Further, the shape of the hoodle 18 can be the other shapes such as spherical shape, ellipsoid, cylinder, can be in housing With hemispherical, taper or other shapes of array distribution on 17.
Further, the elastic component 6 is spring or rubber.
When test, high pressure gas cylinder 1 is opened, after filling high pressure gas to rated pressure to piston cylinder 5 by pressurizing device, is closed Close high pressure gas cylinder 1 and pressure reducing valve 2.High pressure gas is after the first check valve 8 and venthole 9 at this time, full of on first piston 11 Lower two inside cavities, since 11 lower end surface area of first piston is greater than upper surface area, first piston 11 makes first upwards Sealing ring 12 is in impaction state, thus sealing piston cylinder 5.It turns on the switch 20, starts solenoid valve 19, in 5 lower chamber of piston cylinder High pressure gas through 19 quick release of solenoid valve, due to the effect of the first check valve 8, the intracorporal high pressure gas of 5 epicoele of piston cylinder It can not be flowed out by stomata 9, first piston 11 quick slide downward and compression elastic piece 6 under huge differential pressure action are lived at this time The intracorporal high pressure gas of 5 epicoele of plug cylinder is sprayed from the top of first piston 11, drives the upward high-speed motion of second piston 13, thus It compresses 14 internal gas of gun tube and generates two-stage compression gas, when high pressure gas reaches Rupture of Membrane pressure in gun tube 14,15 quilt of diaphragm After crushing, 18 high speed ejection of hoodle inside housing 17 completes emission test.It can also vacuumize inside gun tube 14 to reduce big gun Pressure inside pipe 14, and then improve the compression speed of second piston 13.
Hoodle array high speed ejection device of the invention drives compared to explosive, changes using high pressure gas as driving source The safety and the feature of environmental protection of test have been apt to it, the experimental study for the development underground explosion effect of related fields provides great side Just;By adjusting in gun tube 14 pressure and second piston 13 along 14 upward high-speed motion of gun tube when, on the gun tube 14 End, reaches sealing effect, and the only high pressure gas in gun tube 14 acts on hoodle 18, avoids a large amount of high in piston cylinder 5 Body of calming the anger enters housing 18, so that the emission rate quantification of hoodle measures, improves experiment measurement accuracy.

Claims (10)

1. a kind of hoodle array high speed ejection device, which is characterized in that including pressurizing device, piston cylinder (5), first piston (11), elastic component (6), the first sealing ring (12), second piston (13), gun tube (14), diaphragm (15), housing (17), hoodle (18), compression relief cock;
Piston cylinder (5) top is equipped with through-hole, and through-hole is connected with gun tube (14), and gun tube (14) bottom and piston cylinder (5) are internal It is connected;Gun tube (14) top is fixed with housing (17), and housing (17) is equipped with multiple launch holes, is filled in launch hole Hoodle (18);Second piston (13) setting can slide up and down in gun tube (14) in gun tube (14);The diaphragm (15) It is arranged in gun tube (14) upper end, to be sealed to gun tube (14) upper end;The first piston (11) is arranged in piston cylinder (5) It is interior, it can be slided up and down in piston cylinder (5);First piston (11) vertical section is I-shaped;And lower end surface area is greater than upper Face area;First piston (11) lower end is equipped with elastic component (6), and elastic component (6) pushes up first piston (11) upper end It is contacted with piston cylinder (5) upper end inner wall, and is equipped with the first sealing ring (12) between first piston (11) upper end and piston cylinder (5), First sealing ring (12) is sealed piston cylinder (5) top through-hole;First piston (11) lower end is internal by piston cylinder (5) Cavity is divided into upper and lower two cavitys;First piston (11) lower end is equipped with venthole (9), and venthole (9) will be upper and lower empty Chamber connection, and the first check valve (8) are equipped in venthole (9), the first check valve (8) makes gas can only be from lower cavity through venthole (9) upper plenum is flowed to;The pressurizing device is connected by the pipeline of piston cylinder (5) bottom with the lower cavity of piston cylinder (5);Institute The pipeline for stating piston cylinder (5) bottom is also connected with compression relief cock, to carry out pressure release to cavity gas under piston cylinder (5).
2. hoodle array high speed ejection device according to claim 1, which is characterized in that the first piston (11) is under End cooperates with piston cylinder (5) inner wall, is equipped between the first piston (11) and piston cylinder (5) and guarantees first piston (11) in work The guiding mechanism of sliding stability in plug cylinder (5).
3. hoodle array high speed ejection device according to claim 2, which is characterized in that the guiding mechanism is guiding Plate, the guide plate (10) are fixed in the upper plenum of piston cylinder (5), and the guide plate (10) is equipped with pilot hole and multiple logical Stomata;The first piston (11) is intermediate to be cooperated with pilot hole, can be slided up and down along pilot hole.
4. hoodle array high speed ejection device according to claim 1 or 2, which is characterized in that the guiding mechanism is to lead Xiang Huan;The guide ring is arranged inside piston cylinder (5) upper end;Guide ring is axial axially coaxial with piston cylinder (5) upper end through-hole; First piston (11) the upper end outer wall is bonded with guide ring inner wall, and first piston (11) upper end can be in guide ring up and down Sliding.
5. hoodle array high speed ejection device according to claim 2, which is characterized in that the guiding mechanism is guiding Bar, the guide rod are arranged inside piston cylinder (5) upper end, have extended downwardly guide rod from piston cylinder (5) upper wall, and described first Piston (11) upper end is equipped with pilot hole, and pilot hole is located at outside the first sealing ring (12), guide rod and first piston (11) Pilot hole cooperation, first piston (11) can be slided up and down along guide rod.
6. hoodle array high speed ejection device according to claim 1, which is characterized in that the pressurizing device includes high pressure Gas cylinder (1), pressure reducing valve (2), second one-way valve (4);The high pressure gas cylinder (1) is through pressure reducing valve (2) and second one-way valve (4) phase Even, the second one-way valve (4) is connected with the pipeline of piston cylinder (5) bottom.
7. hoodle array high speed ejection device according to claim 1, which is characterized in that be additionally provided with detection pressurizing device and fill out The pressure measuring unit of the gas pressure filled.
8. hoodle array high speed ejection device according to claim 1, which is characterized in that the pressure measuring unit is pressure gauge (3) or pressure sensor.
9. hoodle array high speed ejection device according to claim 1, which is characterized in that the compression relief cock includes electromagnetism Valve (19), switch (20);The solenoid valve (19) is connected with the pipeline of piston cylinder (5) bottom;The switch (20) is to solenoid valve (19) power on/off.
10. hoodle array high speed ejection device according to claim 1, which is characterized in that the gun tube (14) is close to film The upward diameter in upper end of piece (15) is gradually reduced or gun tube (14) upper end is equipped with the cone (16) that upward diameter is gradually reduced, and is made Second piston (13) when being moved upwards along gun tube (14), second piston (13) is embedded in gun tube (14) upper end.
CN201811121546.7A 2018-09-26 2018-09-26 High-speed catapulting device of marble array Active CN109211305B (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109780930A (en) * 2019-03-19 2019-05-21 江苏心源航空科技有限公司 A kind of air bubble emitter
CN109781508A (en) * 2019-03-05 2019-05-21 武汉深海蓝科技有限公司 A kind of pneumatic type emitter
CN115127114A (en) * 2022-06-27 2022-09-30 北京理工大学 Ignition device for reaction gas gun and reaction gas gun

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0791888A (en) * 1993-09-28 1995-04-07 Japan Steel Works Ltd:The Missile launching device
CN101865760A (en) * 2010-05-28 2010-10-20 中国科学院力学研究所 Gas gun scheme experiment system of high-speed rain movable model
US8256406B1 (en) * 2011-06-01 2012-09-04 Kevin Kirkpatrick Systems and methods for regulating pneumatic gas propulsion
CN103629424A (en) * 2013-12-04 2014-03-12 中国飞机强度研究所 Fast pneumatic valve
CN106442177A (en) * 2016-10-26 2017-02-22 中国工程物理研究院总体工程研究所 Air cannon with quick closure function and use method of air cannon
CN108506149A (en) * 2018-03-12 2018-09-07 河北工业大学 A kind of hoodle ejection diaphragm cylinder formula ocean wave generator

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0791888A (en) * 1993-09-28 1995-04-07 Japan Steel Works Ltd:The Missile launching device
CN101865760A (en) * 2010-05-28 2010-10-20 中国科学院力学研究所 Gas gun scheme experiment system of high-speed rain movable model
US8256406B1 (en) * 2011-06-01 2012-09-04 Kevin Kirkpatrick Systems and methods for regulating pneumatic gas propulsion
CN103629424A (en) * 2013-12-04 2014-03-12 中国飞机强度研究所 Fast pneumatic valve
CN106442177A (en) * 2016-10-26 2017-02-22 中国工程物理研究院总体工程研究所 Air cannon with quick closure function and use method of air cannon
CN108506149A (en) * 2018-03-12 2018-09-07 河北工业大学 A kind of hoodle ejection diaphragm cylinder formula ocean wave generator

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
郭纬;徐小辉;李干;李杰;蒋海明;李志浩: "二级高压驱动阵列弹珠同步弹射微型爆源的研制", 《***与冲击》 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109781508A (en) * 2019-03-05 2019-05-21 武汉深海蓝科技有限公司 A kind of pneumatic type emitter
CN109780930A (en) * 2019-03-19 2019-05-21 江苏心源航空科技有限公司 A kind of air bubble emitter
CN115127114A (en) * 2022-06-27 2022-09-30 北京理工大学 Ignition device for reaction gas gun and reaction gas gun
CN115127114B (en) * 2022-06-27 2023-08-22 北京理工大学 Ignition device for reaction gas gun and reaction gas gun

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