CN102072830A - Water brake system for rocket sled - Google Patents

Water brake system for rocket sled Download PDF

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Publication number
CN102072830A
CN102072830A CN201010615560XA CN201010615560A CN102072830A CN 102072830 A CN102072830 A CN 102072830A CN 201010615560X A CN201010615560X A CN 201010615560XA CN 201010615560 A CN201010615560 A CN 201010615560A CN 102072830 A CN102072830 A CN 102072830A
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CN
China
Prior art keywords
water
track
rocket
tank
rocket sled
Prior art date
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Application number
CN201010615560XA
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Chinese (zh)
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CN102072830B (en
Inventor
余元元
谭贤德
龚明生
黄凤发
刘军
赵华
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AVIC Aerospace Life Support Industries Ltd
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AVIC Aerospace Life Support Industries Ltd
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Publication date
Application filed by AVIC Aerospace Life Support Industries Ltd filed Critical AVIC Aerospace Life Support Industries Ltd
Priority to CN201010615560.XA priority Critical patent/CN102072830B/en
Publication of CN102072830A publication Critical patent/CN102072830A/en
Application granted granted Critical
Publication of CN102072830B publication Critical patent/CN102072830B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The invention provides a water brake system for a rocket sled, which comprises a water brake arranged on a rocket sled vehicle body and a water tank arranged on a track braking section of a rocket sled track, wherein the water brake is arranged on the front part of the rocket sled vehicle body and comprises a water inlet, a water splitting wedge and two water guide channels which are arranged symmetrically on the left and right; the water inlet is arranged in the center of the front end of the rocket sled vehicle body, and the water splitting wedge separates the water inlets into left and right parts to be communicated with the two water guide channels respectively; the water outlets of the two water guide channels are arranged on the two sides of the rocket sled vehicle body respectively; and the water tank is a strip water tank made of a light and brittle material and contains water, the water tank is arranged on a water tank track which is positioned between the two rails of the rocket sled track and parallel to the rocket sled track, and the position of the cross section of the water tank relative to the rocket sled track is consistent with the position of the water inlet relative to the rocket sled track. The structure makes the brake load of the reducing section of the rocket sled have the shortest and most direct power transmission line and minimizes added bending moment generated by the brake load.

Description

A kind of water brake system of rocket sled
Technical field
The invention belongs to rocket sledge slide rail experimental technique field, relate in particular to the water brake system of rocket sled.
Background technology
The scoop-like water brake device that is mounted in sledge body main structure bottom that tradition double track rocket sledge adopts usually, the not only quality of this brake own is heavy, the additional drag feature is big, and brake the time can produce big pitching moment, need increase for this reason body construction just, intensity and increase motor power.Be subjected to the structural limitations and the available dynamic matching state of this rocket sledge, traditional double track rocket sledge brake speed is difficult to surpass mach one.
Summary of the invention
Technical matters to be solved by this invention is: at above-mentioned the deficiencies in the prior art, provide a kind of and use under supersonic speed, and can bear big load, be applied to the water brake system of double track rocket sled.
The present invention for the technical scheme that problem adopted of the above-mentioned proposition of solution is:
A kind of water brake system of rocket sled, it comprises water brake device that is arranged on the rocket sled car body and the tank that is arranged on the rocket sled track stopping element; The water brake device is arranged on the front portion of rocket sled car body; The water brake device comprises that water inlet, cutwater split two conduit pipes that distribute with left-right symmetric; Described water inlet is arranged on the front end central authorities of rocket sled car body, and cutwater is split and is positioned at water inlet, after cutwater is split water inlet is divided right and left respectively with two conduit pipe UNICOMs; The water delivering orifice of two conduit pipes is separately positioned on the both sides of rocket sled car body;
Described tank is the bar shaped tank, tank adopts light crisp material to make, be filled with water in the groove, tank is arranged between the rocket sled track double track and is parallel on the tank track of rocket sled track, the tank xsect is prized track with respect to the position and the water inlet of rocket sled track with respect to rocket position consistency.
In the such scheme, the water brake system also comprises the tank track that is used to support tank, and the tank track is arranged between the double track and is parallel to rocket sledge track; When the rocket sledge passed through, the tank track was in the below of rocket sledge and does not collide with the rocket sledge.
In the such scheme, conduit pipe comprises intake tunnel, exhalant canal and the circular arc passage between intake tunnel and exhalant canal, and the angle between the axis of intake tunnel and the axis of exhalant canal is 160 °~170 °.
In the such scheme, the most advanced and sophisticated line face that plane, water inlet place and described cutwater are split is in the same plane or place the place ahead of most advanced and sophisticated line face.
In the such scheme, described water brake device is with respect to described cutwater splitter end line symmetry.
In the such scheme, the rocket of described conduit pipe outside sled car body front end is provided with fiaring cone.
Beneficial effect of the present invention is:
1. because the water brake device is arranged on the front portion of rocket sled car body, and can place in the rocket sled car body and car body fusion design, when the water brake device bumps against tank, can be so that water brake device and car body bear the substantial load of current all directions jointly, this structure makes the brake load of rocket sledge braking section have short, the most direct power transmission route, and the additional bending moment of its generation is minimized, brake speed can reach 1.85 Mach.
2. the water brake device is arranged on rocket sled Vehicular body front, can not cause a devastating effect to body construction even the water brake device destroys to some extent, and this water brake device is relatively independent, and has good portability.
3, the rocket of described conduit pipe outside sled car body front end is provided with fiaring cone, and fiaring cone can reduce aerodynamic drag to carrying out rectification, and effect is more obvious in the supersonic speed test.
Description of drawings
Fig. 1 is the structural representation with rocket sled car body of the embodiment of the invention.
Fig. 2 is the structural representation of two conduit pipes.
Fig. 3 is the scheme of installation of tank and tank track.
1-water inlet among the figure, the 2-cutwater is split, 3-water delivering orifice, 4-outlet conduit, 5-fiaring cone, 6-inlet channel, 7-car body, 8-tank, 9-tank track, 10-rocket sled track.
Embodiment
The water brake system embodiment of rocket sled of the present invention as shown in Figure 1, 2, 3, it comprises water brake device that is arranged on the rocket sled car body 7 and the tank 8 that is arranged on the rocket sled track stopping element; The water brake device is arranged on the front portion of rocket sled car body 7; The water brake device comprises that water inlet 1, cutwater split 2 and two conduit pipes; Described water inlet 1 is arranged on the front end central authorities of rocket sled car body 7, and cutwater is split 2 and is positioned at water inlet, cutwater split 2 water inlet 1 divided right and left after respectively with two conduit pipe UNICOMs; The water delivering orifice 3 of two conduit pipes is separately positioned on the both sides of rocket sled car body 7.
The rocket sled car body front end of described conduit pipe outside is provided with fiaring cone 5.
As shown in Figure 2, conduit pipe comprises intake tunnel 6, exhalant canal 4 and the circular arc passage between intake tunnel and exhalant canal, and the angle between the axis of the axis of intake tunnel 6 and exhalant canal 4 is 160 °~170 °.
Water inlet plane, 1 place and described cutwater split that 2 most advanced and sophisticated line face is in the same plane, and the width of water inlet 1 is 180mm, and described two conduit pipes are split 2 most advanced and sophisticated lines with respect to described cutwater and are symmetrical arranged.
As shown in Figure 3, described tank 8 is the bar shaped tank, tank 8 adopts light crisp material to make, be filled with water in the tank 8, tank is prized between track 10 double tracks and parallel and rocket sled track at rocket, the tank xsect is prized track 10 with respect to the position and the water inlet 1 of rocket sled track 10 with respect to rocket position consistency.
In order to protect the rocket sledge not broken by tank 8, tank 8 adopts the lightweight foamed plastics material to make disposable use.
The water brake system also comprises the tank track 9 that is used to support tank 8, and tank track 9 is arranged on the below of tank 8.
In the present embodiment, cutwater splits 2 by 30CrMnSiA(D) machine adds and makes, and the material of conduit pipe is 30CrMnSiA.
The principle of work of the embodiment of the invention is: after the rocket sled enters stopping element, the water brake device of rocket sled front end hits tank 8, tank 8 fragmentations, water in the tank enters water inlet, current are split 2 by cutwater and are divided into two strands, enter two conduit pipes respectively, after the circular arc passage of conduit pipe turns to, flow out from water delivering orifice 3 respectively.Momentum conversion by water brake device and water produces water brake power, realizes the braking of rocket sledge.
Protection scope of the present invention is not limited to the above embodiments, and obviously, those skilled in the art can carry out various changes and distortion and do not depart from the scope of the present invention and spirit the present invention.If these changes and distortion belong in the scope of claim of the present invention and equivalent technologies thereof, then the intent of the present invention also comprises these changes and is out of shape interior.

Claims (6)

1. the water brake system of rocket sled is characterized in that: it comprises and is arranged on the water brake device on the rocket sled car body and is arranged on tank on the rocket sled track stopping element; The water brake device is arranged on the front portion of rocket sled car body; The water brake device comprises that water inlet, cutwater split two conduit pipes that distribute with left-right symmetric; Described water inlet is arranged on the front end central authorities of rocket sled car body, and cutwater is split and is positioned at water inlet, after cutwater is split water inlet is divided right and left respectively with two conduit pipe UNICOMs; The water delivering orifice of conduit pipe is separately positioned on the both sides of rocket sled car body;
Described tank is the bar shaped tank, tank adopts light crisp material to make, be filled with water in the groove, tank is arranged between the rocket sled track double track and is parallel on the tank track of rocket sled track, the tank xsect is prized track with respect to the position and the water inlet of rocket sled track with respect to rocket position consistency.
2. water brake as claimed in claim 1 system, it is characterized in that: it also comprises the tank track that is used to support tank, the tank track is arranged between the double track and is parallel to rocket sledge track; When the rocket sledge passed through, the tank track was in the below of rocket sledge and does not collide with the rocket sledge.
3. water brake as claimed in claim 1 system, it is characterized in that: conduit pipe comprises intake tunnel, exhalant canal and the circular arc passage between intake tunnel and exhalant canal, and the angle between the axis of intake tunnel and the axis of exhalant canal is 160 °~170 °.
4. water brake as claimed in claim 1 system, it is characterized in that: the most advanced and sophisticated line face that plane, water inlet place and described cutwater are split is in same plane or places the place ahead of most advanced and sophisticated line face.
5. as each described water brake system of claim 1 to 4, it is characterized in that: described water brake device is with respect to described cutwater splitter end line symmetry.
6. as each described water brake system of claim 1 to 4, it is characterized in that: the rocket sled car body front end of described conduit pipe outside is provided with fiaring cone.
CN201010615560.XA 2010-12-31 2010-12-31 Water brake system for rocket sled Expired - Fee Related CN102072830B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201010615560.XA CN102072830B (en) 2010-12-31 2010-12-31 Water brake system for rocket sled

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201010615560.XA CN102072830B (en) 2010-12-31 2010-12-31 Water brake system for rocket sled

Publications (2)

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CN102072830A true CN102072830A (en) 2011-05-25
CN102072830B CN102072830B (en) 2014-04-09

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104535101A (en) * 2014-11-26 2015-04-22 航宇救生装备有限公司 Damping slide block device for high-speed rocket sled test
CN112208791A (en) * 2020-10-14 2021-01-12 航宇救生装备有限公司 Recovery system for head of umbrella shooting gun

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201581800U (en) * 2009-11-23 2010-09-15 石家庄煤矿机械有限责任公司 Adjustable hydraulic brake
CN201917463U (en) * 2010-12-31 2011-08-03 航宇救生装备有限公司 Hydraulic brake system of rocket pry

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201581800U (en) * 2009-11-23 2010-09-15 石家庄煤矿机械有限责任公司 Adjustable hydraulic brake
CN201917463U (en) * 2010-12-31 2011-08-03 航宇救生装备有限公司 Hydraulic brake system of rocket pry

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
余元元: "《双轨火箭滑车高速水刹装置研究》", 《中国优秀硕士学位论文全文数据库》, no. 06, 15 June 2009 (2009-06-15) *
梁在湖等: "《水刹车》", 《武汉水利电力学院学报》, no. 4, 31 December 1978 (1978-12-31) *
樊正祥: "《水刹车的选型计算》", 《西部探矿工程》, vol. 8, no. 4, 31 July 1996 (1996-07-31), pages 31 - 32 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104535101A (en) * 2014-11-26 2015-04-22 航宇救生装备有限公司 Damping slide block device for high-speed rocket sled test
CN112208791A (en) * 2020-10-14 2021-01-12 航宇救生装备有限公司 Recovery system for head of umbrella shooting gun
CN112208791B (en) * 2020-10-14 2023-10-13 航宇救生装备有限公司 Rifle head recovery system of umbrella shooting gun

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C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
EE01 Entry into force of recordation of patent licensing contract

Application publication date: 20110525

Assignee: Chinese Air Lifesaving Inst.

Assignor: Aerospace Life-Support Industries Co., Ltd.

Contract record no.: 2015420000110

Denomination of invention: Hydraulic brake system of rocket pry

Granted publication date: 20140409

License type: Exclusive License

Record date: 20150624

LICC Enforcement, change and cancellation of record of contracts on the licence for exploitation of a patent or utility model
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140409

Termination date: 20191231

CF01 Termination of patent right due to non-payment of annual fee