CN108918073A - A kind of ballisticimpact experimental provision under hot conditions - Google Patents

A kind of ballisticimpact experimental provision under hot conditions Download PDF

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Publication number
CN108918073A
CN108918073A CN201810600720.XA CN201810600720A CN108918073A CN 108918073 A CN108918073 A CN 108918073A CN 201810600720 A CN201810600720 A CN 201810600720A CN 108918073 A CN108918073 A CN 108918073A
Authority
CN
China
Prior art keywords
measured
target body
ballisticimpact
experimental provision
under hot
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201810600720.XA
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Chinese (zh)
Inventor
郑百林
杨彪
刘焦
张锴
史同承
李毅然
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tongji University
AECC Commercial Aircraft Engine Co Ltd
Original Assignee
Tongji University
AECC Commercial Aircraft Engine Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Tongji University, AECC Commercial Aircraft Engine Co Ltd filed Critical Tongji University
Priority to CN201810600720.XA priority Critical patent/CN108918073A/en
Publication of CN108918073A publication Critical patent/CN108918073A/en
Pending legal-status Critical Current

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M7/00Vibration-testing of structures; Shock-testing of structures
    • G01M7/08Shock-testing

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

The present invention relates to a kind of ballisticimpact experimental provisions under hot conditions, including cabinet and chamber door to be opened/closed, chamber door is equipped with the shell hole to be opened/closed passed through for bullet, target body to be measured is mounted in cabinet by bracket and claw and face shell hole, experimental provision includes muti-piece heater and the fan that is arranged in front of every piece of heater, the channel of fan face target body to be measured and cabinet wall, the cabinet wall filling with insulation material.Compared with prior art, the present invention is heated by heater, then the intracorporal rapid air movement of case is made by fan, air is heated when passing through heater, by heating target body to be measured when target body to be measured, due to forming air duct between target body to be measured and cabinet wall, air recycles in air duct, it is possible to guarantee that target body to be measured evenly and rapidly heats up;And high degree of automation.

Description

A kind of ballisticimpact experimental provision under hot conditions
Technical field
The present invention relates to ballisticimpact experimental technique fields, and in particular to a kind of real for the ballisticimpact under hot conditions Experiment device.
Background technique
The non-inclusive accident of aero-engine will lead to the serious airplane crash of fatal crass, therefore in the research and development of aero-engine Cheng Zhong, it is ensured that the casing containment of engine is the most important condition of engine health operation.Study engine crankcase inclusiveness One important experiment is ballisticimpact experiment, is tested by room temperature ballisticimpact to determine engine inclusive design at present Relevant parameter.In fact the operating ambient temperature range of engine contains (- 25 DEG C~600 DEG C), institute from low temperature to high temperature It is also critically important for engine inclusive design, to carry out the ballisticimpact experiment of casing material at high operating temperatures, it opens The heating device that hair can guarantee that casing material is heated evenly and temperature can achieve 600 DEG C or more has important research significance And application prospect.
The difficult point of high temperature ballisticimpact experiment at present is that casing material is heated and kept the temperature during the experiment, simultaneously Also need to guarantee the operability and safety of experiment, carrying out the fixed mode of target body after conventional heating target body again there will naturally be Certain risk, furthermore during the experiment guarantee target body heating temperature reach preset temperature and be heated evenly be also experiment Important indicator.Guarantee the safety of target body clamping device during the experiment and the absorption of body is also to test smooth implementation Key.
Summary of the invention
It is simple, heated that it is an object of the present invention to overcome the above-mentioned drawbacks of the prior art and provide a kind of structures The uniform ballisticimpact experimental provision under hot conditions.
The purpose of the present invention can be achieved through the following technical solutions:It is a kind of real for the ballisticimpact under hot conditions Experiment device, the experimental rig include cabinet and chamber door to be opened/closed, and the chamber door is equipped with to be opened/closed to be passed through for bullet Shell hole, target body to be measured is mounted in cabinet by bracket and claw and face shell hole, and the experimental provision includes muti-piece heater And the fan in front of every piece of heater is set, and the channel of fan the face target body and cabinet wall to be measured, the cabinet Inner wall filling with insulation material.
The present invention is heated by heater, then makes the intracorporal rapid air movement of case by fan, air is by adding It is heated when hot device, it is empty due to forming air duct between target body to be measured and cabinet wall by heating target body to be measured when target body to be measured Gas recycles in air duct, it is possible to guarantee that target body to be measured evenly and rapidly heats up.
The heater quantity is 2, and is symmetricly set on the Channel front end of target body two sidewalls and cabinet wall to be measured.
Partition is fixed on the cabinet wall, the heater and fan are fixedly mounted on partition, the partition It is parallel with chamber door.
One far from chamber door of the target body to be measured is equipped with bullet absorption mesh between side and cabinet wall, bullet is arranged Absorption mesh impinges upon on cabinet wall after can preventing bullet from passing through target body to be measured.
Preferably, the material of the bullet absorption mesh is asbestos.
The target body surface to be measured is equipped with temperature sensor.
The experimental provision further includes the controller connecting with temperature sensor, the controller and heater and shell hole The switch of opening and closing connects.By controller and temperature sensor, temperature can be increased from required temperature automatically, be then turned on bullet Hole, experiment start, high degree of automation.
The controller is PLC controller.
The heat-barrier material is mineral wool, since mineral wool has good thermal insulation property, and it is transparent, so testing Picture of the bullet across target body to be measured when can be shot in journey, therefore, the outer surface of cabinet opens up form or using transparent material.
The bracket is more root posts that cabinet wall bottom is arranged in, and the target body to be measured is placed on the top of column End, the claw is to be arranged in two opposing sidewalls of cabinet wall, and abut with the side of target body to be measured.Branch of the invention Frame and claw are all made of elongated column support or abut target body to be measured, and too big shadow will not be thus generated to air duct It rings, guarantees the heating of target body to be measured, and the nail of different model is selected to squeeze claw, the angle of adjustable target body to be measured.
Compared with prior art, the beneficial effects of the present invention are embodied in following several respects:
(1) it is heated by heater, the intracorporal rapid air movement of case is then made by fan, air passes through heater When be heated, by heating target body to be measured when target body to be measured, due to forming air duct between target body to be measured and cabinet wall, air exists It is recycled in air duct, it is possible to guarantee that target body to be measured evenly and rapidly heats up;
(2) high degree of automation, ballisticimpact experiment and the heating of target plate material can synchronous progress, improve experiment can Operability avoids the problem of target plate temperature reduces caused by removing heating equipment in experimentation;
(3) picture of the bullet across target body to be measured when can be shot;
It (4) can be by adjusting bracket and claw to the claming angle of target body to be measured, to realize tiltedly hitting for target body to be measured.
Detailed description of the invention
Fig. 1 is main view the schematic diagram of the section structure of the invention;
Fig. 2 is side elevational cross-section structural schematic diagram of the invention.
Wherein, 1 is chamber door, and 2 be cabinet, and 3 be partition, and 4 be heater, and 5 be temperature sensor, and 6 be fan, and 7 be air duct, 8 be target body to be measured, and 9 be heat-barrier material, and 10 be bullet absorption mesh, and 11 be PLC controller, and 12 be shell hole, and 13 be bracket, and 14 be card Pawl.
Specific embodiment
It elaborates below to the embodiment of the present invention, the present embodiment carries out under the premise of the technical scheme of the present invention Implement, the detailed implementation method and specific operation process are given, but protection scope of the present invention is not limited to following implementation Example.
Embodiment 1
A kind of ballisticimpact experimental provision under hot conditions, structure is as shown in Figure 1 and Figure 2, including cabinet 2 with And chamber door 1 to be opened/closed, chamber door 1 are equipped with the shell hole 12 to be opened/closed passed through for bullet, target body 8 to be measured passes through bracket 13 and card Pawl 14 is mounted in cabinet 2 and face shell hole 12, and experimental provision includes muti-piece heater 4 and is arranged before every piece of heater 4 The fan 6 of side, the channel of 6 face of fan target body 8 and 2 inner wall of cabinet to be measured, 2 inner wall filling with insulation material 9 of cabinet.
The present invention is heated by heater 4, then makes the rapid air movement in cabinet 2 by fan 6, and air passes through It is heated when heater 4, by heating target body 8 to be measured when target body 8 to be measured, due to being formed between 2 inner wall of target body 8 to be measured and cabinet Air duct 7, air recycle in air duct 7, it is possible to guarantee that target body 8 to be measured evenly and rapidly heats up.
4 quantity of heater is 2, and is symmetricly set on the Channel front end of 8 two sidewalls of target body and 2 inner wall of cabinet to be measured.
Partition 3 is fixed on 2 inner wall of cabinet, heater 4 and fan 6 are fixedly mounted on partition 3, partition 3 and chamber door 1 In parallel.
It is equipped with bullet absorption mesh 10 between a side of the target body 8 to be measured far from chamber door 1 and 2 inner wall of cabinet, bullet is set Absorption mesh 10 impinges upon on 2 inner wall of cabinet after can preventing bullet from passing through target body 8 to be measured.
The material of bullet absorption mesh 10 is asbestos.
8 surface of target body to be measured is equipped with temperature sensor 5.
Experimental provision further includes the PLC controller 11 connecting with temperature sensor 5, PLC controller 11 and heater 4 and bullet The switch connection that hole 12 is opened and closed.By PLC controller 11 and temperature sensor 5, temperature can be increased from required temperature automatically, It is then turned on shell hole 12, experiment starts, high degree of automation.
Heat-barrier material 9 is mineral wool, since mineral wool has good thermal insulation property, and it is transparent, so in experimentation Picture of the bullet across target body 8 to be measured when can be shot, therefore, the outer surface of cabinet 2 opens up form or using transparent material.
Bracket 13 is more root posts that 2 inner wall bottom of cabinet is arranged in, and target body 8 to be measured is placed on the top of column, claw 14 be to be arranged in two opposing sidewalls of 2 inner wall of cabinet, and abut with the side of target body 8 to be measured.Bracket 13 of the invention with And claw 14 is all made of elongated column support or abuts target body 8 to be measured, and too big shadow will not be thus generated to air duct 7 It rings, guarantees the heating of target body 8 to be measured, and the nail of different model is selected to squeeze claw 14, the angle of adjustable target body 8 to be measured Degree.

Claims (10)

1. a kind of ballisticimpact experimental provision under hot conditions, which includes cabinet and case to be opened/closed Door, the chamber door are equipped with the shell hole to be opened/closed passed through for bullet, and target body to be measured is mounted in cabinet by bracket and claw And face shell hole, which is characterized in that the experimental provision includes muti-piece heater and the wind that is arranged in front of every piece of heater Fan, the channel of fan the face target body and cabinet wall to be measured, the cabinet wall filling with insulation material.
2. a kind of ballisticimpact experimental provision under hot conditions according to claim 1, which is characterized in that described Heater quantity be 2, and be symmetricly set on the Channel front end of target body two sidewalls and cabinet wall to be measured.
3. a kind of ballisticimpact experimental provision under hot conditions according to claim 1 or 2, which is characterized in that Partition is fixed on the cabinet wall, the heater and fan are fixedly mounted on partition, and the partition and chamber door are flat Row.
4. a kind of ballisticimpact experimental provision under hot conditions according to claim 1, which is characterized in that described One far from chamber door of target body to be measured bullet absorption mesh is equipped between side and cabinet wall.
5. a kind of ballisticimpact experimental provision under hot conditions according to claim 4, which is characterized in that described The material of bullet absorption mesh is asbestos.
6. a kind of ballisticimpact experimental provision under hot conditions according to claim 1, which is characterized in that described Target body surface to be measured be equipped with temperature sensor.
7. a kind of ballisticimpact experimental provision under hot conditions according to claim 6, which is characterized in that described Experimental provision further include the controller being connect with temperature sensor, the switch that the controller and heater and shell hole are opened and closed connects It connects.
8. a kind of ballisticimpact experimental provision under hot conditions according to claim 7, which is characterized in that described Controller be PLC controller.
9. a kind of ballisticimpact experimental provision under hot conditions according to claim 1, which is characterized in that described Heat-barrier material be mineral wool.
10. a kind of ballisticimpact experimental provision under hot conditions according to claim 1, which is characterized in that institute The bracket stated is more root posts that cabinet wall bottom is arranged in, and the target body to be measured is placed on the top of column, the claw To be arranged in two opposing sidewalls of cabinet wall, and abutted with the side of target body to be measured.
CN201810600720.XA 2018-06-12 2018-06-12 A kind of ballisticimpact experimental provision under hot conditions Pending CN108918073A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810600720.XA CN108918073A (en) 2018-06-12 2018-06-12 A kind of ballisticimpact experimental provision under hot conditions

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810600720.XA CN108918073A (en) 2018-06-12 2018-06-12 A kind of ballisticimpact experimental provision under hot conditions

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Publication Number Publication Date
CN108918073A true CN108918073A (en) 2018-11-30

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112710567A (en) * 2020-12-23 2021-04-27 中国人民解放军陆军工程大学 Temperature-controllable ballistic impact experimental device
CN113492998A (en) * 2021-01-15 2021-10-12 西北工业大学 Experimental device and experimental method for simulating projectile multi-angle impact of aircraft fuel tank

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US9354136B1 (en) * 2013-07-10 2016-05-31 Invocon, Inc. Method for determination of multiple shrapnel hits on a ballistic target threat
CN105716962A (en) * 2016-02-01 2016-06-29 浙江大学 Blade local heating constant-speed fly-off test technology used for casing containment test
CN107515154A (en) * 2017-08-26 2017-12-26 大连理工大学 A kind of experimental provision and its evaluation method using zap pit three-dimensional appearance volume as the fabric ballistic performance of index

Patent Citations (5)

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Publication number Priority date Publication date Assignee Title
US8307694B1 (en) * 2008-03-18 2012-11-13 Invocon, Inc. Hypervelocity impact detection method and system for determining impact location in a detection surface
CN102609557A (en) * 2011-11-11 2012-07-25 南京航空航天大学 Safety analysis method for uncontained failure of aircraft engine rotors
US9354136B1 (en) * 2013-07-10 2016-05-31 Invocon, Inc. Method for determination of multiple shrapnel hits on a ballistic target threat
CN105716962A (en) * 2016-02-01 2016-06-29 浙江大学 Blade local heating constant-speed fly-off test technology used for casing containment test
CN107515154A (en) * 2017-08-26 2017-12-26 大连理工大学 A kind of experimental provision and its evaluation method using zap pit three-dimensional appearance volume as the fabric ballistic performance of index

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112710567A (en) * 2020-12-23 2021-04-27 中国人民解放军陆军工程大学 Temperature-controllable ballistic impact experimental device
CN113492998A (en) * 2021-01-15 2021-10-12 西北工业大学 Experimental device and experimental method for simulating projectile multi-angle impact of aircraft fuel tank
CN113492998B (en) * 2021-01-15 2023-09-01 西北工业大学 Experimental device and experimental method for simulating multi-angle impact of projectile on fuel tank of aircraft

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Application publication date: 20181130