CN108716878A - A kind of dynamic flying target Damage proficiency testing system and its test method - Google Patents
A kind of dynamic flying target Damage proficiency testing system and its test method Download PDFInfo
- Publication number
- CN108716878A CN108716878A CN201810345999.1A CN201810345999A CN108716878A CN 108716878 A CN108716878 A CN 108716878A CN 201810345999 A CN201810345999 A CN 201810345999A CN 108716878 A CN108716878 A CN 108716878A
- Authority
- CN
- China
- Prior art keywords
- fuse mounting
- bullet
- target
- mounting device
- solid bullet
- 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.)
- Granted
Links
- 238000012360 testing method Methods 0.000 title claims abstract description 23
- 230000009187 flying Effects 0.000 title claims abstract description 20
- 238000010998 test method Methods 0.000 title claims abstract description 11
- 239000007787 solid Substances 0.000 claims abstract description 52
- 238000004064 recycling Methods 0.000 claims abstract description 17
- 239000002360 explosive Substances 0.000 claims abstract description 15
- 239000002184 metal Substances 0.000 claims abstract description 13
- 238000004458 analytical method Methods 0.000 claims abstract description 7
- 238000009434 installation Methods 0.000 claims description 13
- 238000005474 detonation Methods 0.000 claims description 8
- 230000015556 catabolic process Effects 0.000 claims description 7
- 238000010304 firing Methods 0.000 claims description 4
- 239000000843 powder Substances 0.000 claims description 4
- 239000003380 propellant Substances 0.000 claims description 4
- 238000000034 method Methods 0.000 abstract description 11
- 238000012795 verification Methods 0.000 abstract description 11
- 230000003068 static effect Effects 0.000 abstract description 7
- 238000004088 simulation Methods 0.000 abstract description 4
- 230000000694 effects Effects 0.000 abstract description 3
- 238000002474 experimental method Methods 0.000 description 4
- 239000002689 soil Substances 0.000 description 3
- 238000013461 design Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 239000002351 wastewater Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B35/00—Testing or checking of ammunition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B35/00—Testing or checking of ammunition
- F42B35/02—Gauging, sorting, trimming or shortening cartridges or missiles
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The present invention provides a kind of dynamic flying target Damage proficiency testing system and its test methods, it is related to injuring verification field, the present invention recycles mound according to by bullet successively in the horizontal direction, injure member and fuse mounting device, protection shield, cannon is alternatively arranged, solid bullet is by Canon launching, emit solid bullet with zero angle, when solid bullet, which is hit, injures the switch target in member and fuse mounting device, contact fuze ignites high explosive anti-tank cartridge warhead and forms metal jet, hit the mark bullet, subsequent solid bullet falls into recycling mound, solid bullet is recycled, it can carry out analysis calculating.Test method of the present invention is simple, operability is strong, and test result is verified to achieve preferable test effect close to truth, solves the problems, such as that traditional simulation or static authentication methods test result deviation are larger；The pilot system of the present invention is of low cost, and cost is significantly reduced compared to using rocket sled skimulated motion mesh calibration method.
Description
Technical field
The present invention relates to the verification test system for injuring verification field more particularly to a kind of Kill capability and its experiment sides
Method.
Background technology
In view of giant earth drill such as GBU-57, GBU-28, to China core position, there are grave dangers, carry out for many years
Research is injured to such target, since the giant earth drill volume such as GBU-57, GBU-28 is big, weight is big, the big (GBU-28 of wall thickness
For 57mm, GBU-57 110mm), movement velocity it is high (600m/s), early period mainly uses theory analysis and static, dynamic value
The methods of emulation is studied, while also having carried out static Kill capability verification experimental verification using the static state method of injuring.But it is above logical
The obtained result of method and actual difference for crossing emulation or static authentication are larger.In addition, prizing skimulated motion target using rocket
Method compared to emulation or static authentication methods more close to true effect, but rocket sled is expensive and it is easily damaged by explosive
It is bad, limit being widely used for it.
Invention content
For overcome the deficiencies in the prior art, the present invention provides a kind of examination that dynamic flying target Damage is verified in energy realization
Experiment device and its test method, for verifying the Kill capability for injuring member to dynamic flying target, and it is at low cost, the period is short, easily
In realization.
The technical solution adopted by the present invention to solve the technical problems is：
A kind of dynamic flying target Damage Proficiency testing system, including recycling mound injure member and fuse installation dress
Set, protection shield, solid bullet and cannon, in the horizontal direction successively according to by bullet recycle mound, injure member and fuse installation dress
Set, protection shield, cannon are alternatively arranged, solid bullet is by Canon launching.
The injure member and fuse mounting device includes switch target installation part, injures member and fuse mounting cylinder fixed frame,
Member and fuse mounting cylinder and fixed supporting leg are injured, wherein member and fuse mounting cylinder fixed frame are injured above fixed supporting leg, and with
Fixed supporting leg is fixedly connected；Switch target installation part injuring member and fuse mounting cylinder fixed frame above, and with injure member and fuse
Mounting cylinder fixed frame is fixedly connected；It injures member and fuse mounting cylinder and is fixedly connected with first and fuse mounting cylinder fixed frame is injured.
Using cannon as the emitter of imitating shell, it is simulated target to select with sized solid bullet, by high explosive anti-tank cartridge warhead
It is fixed on and injures on member and fuse mounting device, so that gun laying is injured the target on member and fuse mounting device using boresight fixture assembly
Mark emits solid bullet with zero angle, solid bullet with required speed by injuring member and fuse mounting device, when solid
Bullet is hit when injuring the switch target in member and fuse mounting device, and contact fuze, which ignites high explosive anti-tank cartridge warhead and forms metal, to be penetrated
Stream, hit the mark bullet, and subsequent solid bullet falls into recycling mound, and solid bullet is recycled, and observes damage effectiveness, you can carries out
Analysis calculates.
The present invention also provides a kind of test method of dynamic flying target Damage proficiency testing system is related to, detailed step is such as
Under：
Step 1：By a kind of dynamic flying target Damage proficiency testing system of the present invention, it is sequentially arranged recycling soil
Heap injures member and fuse mounting device, protection shield, solid bullet and cannon；
Step 2：Adjustment cannon firing angle is zero degree, and locking adjuster takes aim at target with borescope, and target is to injure member and fuse
The switch target cross searching of mounting device；
Step 3：Member and position and the height of fuse mounting device are injured according to the adjustment of target situation is taken aim at, and is fixed；Together
When high explosive anti-tank cartridge warhead is fixed on injure member and fuse mounting device on；
Step 4：The filling of ball cartridge ball and propellant powder is carried out on cannon；
Step 5：Solid bullet is fired, solid bullet hits the switch target for injuring member and fuse mounting device, detonation chain
Open-minded, solid bullet detonation generates metal jet, and metal jet high-speed motion hits solid bullet；
Step 6：Solid bullet falls into recycling mound, recycles solid bullet observation breakdown situation, and measure and analyze.
The beneficial effects of the present invention are the present invention test method is simple, operability is strong, test result is verified to be connect
Be bordering on truth, achieve preferable test effect, solve traditional simulation or static authentication methods test result deviation compared with
Big problem；The pilot system of the present invention is of low cost, is significantly reduced compared to using rocket sled skimulated motion mesh calibration method
Cost.
Description of the drawings
Fig. 1 is the dynamic flying target Damage verification test device of the present invention.
Fig. 2 injures member and fuse mounting device for the present invention's.
Fig. 3 is the breakdown test design sketch of the present invention.
Wherein, 1-bullet recycle mound, 2-injure member and fuse mounting device, 3-protection shields, 4-bullets, 5-
130mm cannons, 6-switch targets, 7-switch target installation parts, 8-injure member and fuse mounting cylinder fixed frame, and 9-injure member and draw
Believe that 10-cable of mounting cylinder, 11-fixed supporting legs, 12- enter hole pattern, 13- goes out hole pattern.
Specific implementation mode
Present invention will be further explained below with reference to the attached drawings and examples.
A kind of dynamic flying target Damage Proficiency testing system, including recycling mound injure member and fuse installation dress
Set, protection shield, solid bullet and cannon, in the horizontal direction successively according to by bullet recycle mound, injure member and fuse installation dress
Set, protection shield, cannon are alternatively arranged, solid bullet is by Canon launching.
The injure member and fuse mounting device includes switch target installation part, injures member and fuse mounting cylinder fixed frame,
Member and fuse mounting cylinder and fixed supporting leg are injured, wherein member and fuse mounting cylinder fixed frame are injured above fixed supporting leg, and with
Fixed supporting leg is fixedly connected；Switch target installation part injuring member and fuse mounting cylinder fixed frame above, and with injure member and fuse
Mounting cylinder fixed frame is fixedly connected；It injures member and fuse mounting cylinder and is fixedly connected with first and fuse mounting cylinder fixed frame is injured.
Using cannon as the emitter of imitating shell, it is simulated target to select with sized solid bullet, by high explosive anti-tank cartridge warhead
It is fixed on and injures on member and fuse mounting device, so that gun laying is injured the target on member and fuse mounting device using boresight fixture assembly
Mark emits solid bullet with zero angle, solid bullet with required speed by injuring member and fuse mounting device, when solid
Bullet is hit when injuring the switch target in member and fuse mounting device, and contact fuze, which ignites high explosive anti-tank cartridge warhead and forms metal, to be penetrated
Stream, hit the mark bullet, and subsequent solid bullet falls into recycling mound, and solid bullet is recycled, and observes damage effectiveness, you can carries out
Analysis calculates.
The present invention also provides a kind of test method of dynamic flying target Damage proficiency testing system is related to, detailed step is such as
Under：
Step 1：By a kind of dynamic flying target Damage proficiency testing system of the present invention, it is sequentially arranged recycling soil
Heap injures member and fuse mounting device, protection shield, solid bullet and cannon；
Step 2：Adjustment cannon firing angle is zero degree, and locking adjuster takes aim at target with borescope, and target is to injure member and fuse
The switch target cross searching of mounting device；
Step 3：Member and position and the height of fuse mounting device are injured according to the adjustment of target situation is taken aim at, and is fixed；Together
When high explosive anti-tank cartridge warhead is fixed on injure member and fuse mounting device on；
Step 4：The filling of ball cartridge ball and propellant powder is carried out on cannon；
Step 5：Solid bullet is fired, solid bullet hits the switch target for injuring member and fuse mounting device, detonation chain
Open-minded, solid bullet detonation generates metal jet, and metal jet high-speed motion hits solid bullet；
Step 6：Solid bullet falls into recycling mound, recycles solid bullet observation breakdown situation, and measure and analyze.
For experimental study of the member to the dynamic flyings target Damage ability such as giant earth drill is injured, especially to GBU-
57, the dynamic Kill capability verification experimental verification of the large-scale big wall thickness target such as GBU-28, still belong to the first time development.
The experimental rig that object movement simulation can be provided at this stage is mainly rocket sled because its experimentation cost it is expensive and
For rocket sled easily by reasons such as explosive wastewater damages, which should not use rocket sled be verified.Therefore, it designs and uses
It is a kind of to realize the test method and device that verification is injured to the dynamic flyings target simulation such as giant earth drill, and tested
Verification, demonstrates this method and the feasibility of experimental rig, and realized for the first time at home to the big wall thickness target of dynamic flying
Breakdown verification.
The present invention is using 130mm big guns (according to target difference, other bore cannons may be used) the solid bullet conduct of transmitting
Simulated target simulates the speed and wall thickness of giant earth drill, and high explosive anti-tank cartridge warhead, which is installed on, to be injured on member and fuse mounting device
To implement jet stream breakdown to simulated target, 130mm target bullets are recycled after experiment, measure and are calculated according to blow hole dimension analysis
Its Kill capability.
The experimental rig of the present invention includes 130mm cannons, injures member and fuse mounting device and recycling mound composition, with
130mm cannons are the emitter of imitating shell, select the solid bullet simulated targets of 130mm.Certain angle is pressed by high explosive anti-tank cartridge warhead
Degree is fixed on distance to be injured on member and fuse mounting device.130mm gun layings are made to injure member using boresight fixture assembly when experiment
And the target on fuse mounting device, 130mm target bullets are emitted with zero angle.130mm bullets are at a desired speed by ruining
Wound member and fuse mounting device, when 130mm bullets, which are hit, injures the switch target in member and fuse mounting device, contact fuze draws
Quick-fried high explosive anti-tank cartridge warhead forms metal jet, hits 130mm simulated target bullets, and subsequent 130mm targets bullet falls into recycling soil
Bullet is dug out recycling, observes damage effectiveness, and carry out analysis meter calculation by heap.
The detailed step of the test method of the present embodiment is as follows：
Step 1：As shown in Figure 1, the arrangement of each experimental rig is carried out, protection shield distance 130mm cannon gun muzzle 45m are injured
Member and fuse mounting device (as shown in Figure 2) are apart from gun muzzle 50m, and recycling mound is apart from gun muzzle 100m；
Step 2：130 cannon inspections are carried out, after items check, 130 cannon firing angles of adjustment are zero degree, and mechanical lock is seted the tone
Engagement positions take aim at target with borescope, and target is to injure the switch target cross searching of member and fuse mounting device；
Step 3：Member and position and the height of fuse mounting device are injured according to the adjustment of target situation is taken aim at, and is fixed；
Step 4：After completing preceding paragraph preparation, installation warhead, fuse simultaneously check that acknowledgement state is normal；
Step 5：Carry out the solid ammunition of 130mm cannons, propellant powder filling；
Step 6：130mm cannons are fired, are fired shells, bullet hits switch target, and detonation chain is open-minded, and bullet detonation generates
Metal jet, metal jet high-speed motion hit 130mm bullets；
Step 7：130mm bullets observation breakdown situation (as shown in Figure 3) is recycled, and measures, analyze；
Step 8：Carry out each device as required removes receipts；
By above 8 steps, it can be achieved that dynamic flying target Damage proficiency testing.
Claims (2)
1. a kind of dynamic flying target Damage proficiency testing system, it is characterised in that：
The dynamic flying target Damage Proficiency testing system, including recycling mound, injure member and fuse mounting device,
Protection shield, solid bullet and cannon, in the horizontal direction successively according to by bullet recycle mound, injure member and fuse mounting device,
Protection shield, cannon are alternatively arranged, and solid bullet is by Canon launching；
The injure member and fuse mounting device includes switch target installation part, injures member and fuse mounting cylinder fixed frame, injures
Member and fuse mounting cylinder and fixed supporting leg, wherein injure member and fuse mounting cylinder fixed frame above fixed supporting leg, and with fixation
Supporting leg is fixedly connected；Switch target installation part is being injured above member and fuse mounting cylinder fixed frame, and is being installed with first and fuse is injured
Cylinder fixed frame is fixedly connected；It injures member and fuse mounting cylinder and is fixedly connected with first and fuse mounting cylinder fixed frame is injured；
Using cannon as the emitter of imitating shell, it is simulated target to select with sized solid bullet, and high explosive anti-tank cartridge warhead is fixed
On injuring member and fuse mounting device, gun laying is set to injure the target on member and fuse mounting device using boresight fixture assembly,
Emit solid bullet with zero angle, solid bullet, by injuring member and fuse mounting device, works as ball cartridge with required speed
Ball is hit when injuring the switch target in member and fuse mounting device, and contact fuze ignites high explosive anti-tank cartridge warhead and forms metal jet,
Hit the mark bullet, and subsequent solid bullet falls into recycling mound, and solid bullet is recycled, and observes damage effectiveness, you can divided
Analysis calculates.
2. a kind of test method carried out using dynamic flying target Damage proficiency testing system described in claim 1, special
Sign is to include the following steps：
Step 1：By a kind of dynamic flying target Damage proficiency testing system of the present invention, it is sequentially arranged recycling mound, is ruined
Wound member and fuse mounting device, protection shield, solid bullet and cannon；
Step 2：Adjustment cannon firing angle is zero degree, and locking adjuster takes aim at target with borescope, and target is to injure member and fuse installation
The switch target cross searching of device；
Step 3：Member and position and the height of fuse mounting device are injured according to the adjustment of target situation is taken aim at, and is fixed；Simultaneously will
High explosive anti-tank cartridge warhead, which is fixed on, to be injured on member and fuse mounting device；
Step 4：The filling of ball cartridge ball and propellant powder is carried out on cannon；
Step 5：Solid bullet is fired, solid bullet hits the switch target for injuring member and fuse mounting device, and detonation chain is open-minded,
Solid bullet detonation generates metal jet, and metal jet high-speed motion hits solid bullet；
Step 6：Solid bullet falls into recycling mound, recycles solid bullet observation breakdown situation, and measure and analyze.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810345999.1A CN108716878B (en) | 2018-04-18 | 2018-04-18 | A kind of dynamic flying target Damage proficiency testing system and its test method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810345999.1A CN108716878B (en) | 2018-04-18 | 2018-04-18 | A kind of dynamic flying target Damage proficiency testing system and its test method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108716878A true CN108716878A (en) | 2018-10-30 |
| CN108716878B CN108716878B (en) | 2019-11-19 |
Family
ID=63899155
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810345999.1A Expired - Fee Related CN108716878B (en) | 2018-04-18 | 2018-04-18 | A kind of dynamic flying target Damage proficiency testing system and its test method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108716878B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109655054A (en) * | 2018-11-22 | 2019-04-19 | 西安近代化学研究所 | A kind of measurement method of antiship warhead strike target ship point of impact position |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2442104C1 (en) * | 2010-09-17 | 2012-02-10 | Сергей Михайлович Мужичек | Method and device for operational efficiency evaluation of ammunition destructive power |
| CN103673791A (en) * | 2013-12-13 | 2014-03-26 | 北京航天时代光电科技有限公司 | System for detecting and evaluating target high-speed impact damage |
| CN104713428A (en) * | 2013-12-11 | 2015-06-17 | 上海机电工程研究所 | Ground combined test device of directional fuze warhead total system and test method thereof |
| CN106771320A (en) * | 2016-11-23 | 2017-05-31 | 北京航天控制仪器研究所 | A kind of rocket sledge image speed measurement method |
-
2018
- 2018-04-18 CN CN201810345999.1A patent/CN108716878B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2442104C1 (en) * | 2010-09-17 | 2012-02-10 | Сергей Михайлович Мужичек | Method and device for operational efficiency evaluation of ammunition destructive power |
| CN104713428A (en) * | 2013-12-11 | 2015-06-17 | 上海机电工程研究所 | Ground combined test device of directional fuze warhead total system and test method thereof |
| CN103673791A (en) * | 2013-12-13 | 2014-03-26 | 北京航天时代光电科技有限公司 | System for detecting and evaluating target high-speed impact damage |
| CN106771320A (en) * | 2016-11-23 | 2017-05-31 | 北京航天控制仪器研究所 | A kind of rocket sledge image speed measurement method |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109655054A (en) * | 2018-11-22 | 2019-04-19 | 西安近代化学研究所 | A kind of measurement method of antiship warhead strike target ship point of impact position |
| CN109655054B (en) * | 2018-11-22 | 2023-02-10 | 西安近代化学研究所 | Method for measuring impact point position of anti-ship warhead hitting target ship |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108716878B (en) | 2019-11-19 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Driels | Weaponeering: conventional weapon system effectiveness | |
| CN105841559B (en) | A kind of air artillery equivalent loading test device for hanging | |
| CN102226672B (en) | Overload test guard box of air bomb | |
| CN107084640B (en) | A kind of simulating training shell automatic transmitting system | |
| CN109655358A (en) | It is a kind of for rock or the impact test apparatus and test method of concrete sample | |
| CN111551458B (en) | Test device and method for simulating multi-blade targeting | |
| CN108716878B (en) | A kind of dynamic flying target Damage proficiency testing system and its test method | |
| CN105823374B (en) | Red blue force's system of live shell rivalry-drilling | |
| RU2339907C1 (en) | Method of ammunition adjustment and test ground to this effect | |
| CN207123216U (en) | A kind of pneumatic transmitter of cartridge type for launching simulation dummy round | |
| CN203561295U (en) | Simulated rocket projectile for emplacement reconnaissance radar training | |
| CN104236384A (en) | Testing method for simulating launching impact overload in chamber | |
| RU184371U1 (en) | Target installation | |
| RU2602162C2 (en) | Method of firing jet projectiles multiple artillery rocket system in counter-battery conditions | |
| CN107152895A (en) | A kind of conformal radar surveys height/global location set composite | |
| JPH07159095A (en) | Shooting simulator | |
| RU2228512C2 (en) | Method and device for tests of mine launcher shot | |
| CN212431926U (en) | Shell launching simulation device beneficial to training | |
| CN212082151U (en) | Multi-functional transmission trainer based on modular design | |
| CN113074576B (en) | Underwater cannon test system and test method thereof | |
| RU2205352C2 (en) | Providing ground complex for tests of combat equipment of antiaircraft missiles and projectiles | |
| CN107179018A (en) | A kind of cartridge type ejection emitter for launching simulation dummy round | |
| CN116481375B (en) | Simulation test device of gun-sled combined emission system | |
| CN202485567U (en) | Pre-split warhead | |
| CN114018109B (en) | Method for determining danger area of falling area of flying test of armor-breaking snap projectile shooting range |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20191119 |