CN105841561A - Fuze emission safety simulation test platform - Google Patents

Fuze emission safety simulation test platform Download PDF

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Publication number
CN105841561A
CN105841561A CN201610228065.0A CN201610228065A CN105841561A CN 105841561 A CN105841561 A CN 105841561A CN 201610228065 A CN201610228065 A CN 201610228065A CN 105841561 A CN105841561 A CN 105841561A
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CN
China
Prior art keywords
rotation
fuze
fuse
platform
test platform
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
CN201610228065.0A
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Chinese (zh)
Inventor
周波
高森林
胡大治
杜研
刘泓佚
韩涛
赵玉玺
王索成
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.)
JILIN JIANGJI MINKE INDUSTRIAL CO LTD
Original Assignee
JILIN JIANGJI MINKE INDUSTRIAL 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 JILIN JIANGJI MINKE INDUSTRIAL CO LTD filed Critical JILIN JIANGJI MINKE INDUSTRIAL CO LTD
Priority to CN201610228065.0A priority Critical patent/CN105841561A/en
Publication of CN105841561A publication Critical patent/CN105841561A/en
Pending legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C21/00Checking fuzes; Testing fuzes

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Abstract

The invention discloses a fuze emission safety simulation test platform and belongs to the technical field of weapons of the military industry. The fuze emission safety simulation test platform is mainly used for comprehensive performance tests on projectile fuzes of various guns, simulates the inertia force and centrifugal force generated by a fuze in the projectile launching process, and is used for testing and checking the reliability of action of a fuze safety mechanism. The fuze emission safety simulation test platform is composed of a combined rotary platform and a measurement and control system. The fuze emission safety simulation test platform is characterized in that the test can be divided into three parts: independent revolution is used for testing the axial inertia force of the fuze, independent rotation is used for testing the radial centrifugal force of the fuze, and by the combination of the revolution and the rotation, the inertia force and centrifugal force generated by the fuze in the projectile launching process not only can be simulated, but also can be adjusted and controlled integrally in real time according to the technical requirements, wherein the revolution rate is 0-8000 r/min, and the rotation rate is 0-10000 r/min. By means of the fuze emission safety simulation test platform, comprehensive performance testing on the safety of various fuzes is achieved, the platform is reasonable in structure, test values are accurate, the detection process is easy and convenient to implement, and the safe and reliable fuze monitoring quality can be guaranteed.

Description

A kind of fuse emission security analogue test platform
Technical field
The invention belongs to military project weaponry technical field, it is specifically related to a kind of fuse emission security analogue test platform, the projectile fuze being mainly used in various cannon carries out the comprehensive performance test of inertia force and centrifugal force, is used for testing and examining the reliability of fuze safety mechanism effect.
Background technology
At present in the performance test of China's various cannon bomb fuse, by existing national military standard 573A " fuze environment and method for testing performance ", the test method of comprehensive recoil inertia force and rotary centrifugal force does not also have national standard, inertia force in the product for civilian use is individually carried out with the test of centrifugal force, and test speed is the lowest, do not reach the projectile fuze truth in actual transmission state, therefore, it is impossible to projectile fuze is carried out comprehensive performance test.
Summary of the invention
It is not enough for the invention aims to solve prior art, a kind of fuse emission security analogue test platform of design, it can analog cartridge double environmental forces suffered by fuse in emission process, i.e. recoil inertia force and the situation of rotary centrifugal force, is used for testing and examining the reliability of fuze safety mechanism effect.Test is divided into three parts: individually revolution be used for testing fuse axial inertia force, individually from being diverted to test fuse radial centrifugal force, revolution is combined with rotation, inertia force that integrated real-time Simulation fuse produces in emission process and centrifugal force.The key technical indexes: revolution speed is 8000r/min;Rotational velocity is 10000r/min.
Realizing the purpose of the present invention to be adopted the technical scheme that, it is provided that a kind of fuse emission security analogue test platform, it is by combining rotation platform and TT&C system forms.
Described combination rotation platform, it is turned by high speed vortex filament bevel gear mechanical differential, dynamic balancing, servo-actuated fuse cabin, revolution high-speed permanent magnetic servomotor, rotation high-speed permanent magnetic servomotor form.It include power shaft 1, mechanical differential 2, the axis of rotation 3, fuse cabin 4, friction top 5, trousers 6, turn 7, support 8, hollow shaft 9, its annexation: described power shaft 1, fitted together by the axis of rotation 3 that described mechanical differential 2 and said two are symmetrical, described fuse cabin 4 is installed on the described axis of rotation 3, described fuse cabin 4 is compressed by described friction top 5, described trousers 6 is arranged in the exit orifice of the described axis of rotation 3, described turning 7 is arranged on described support 8, and described support 8 is arranged on described hollow shaft 9.
Described TT&C system, it uses upper industrial computer to control technology and Automatic Measurement Technique, the various piece working order of combination rotation platform is carried out real-tune TT & C, and it includes revolution control part, revolution feedback fraction, rotation control part, rotation feedback fraction, data process and data acquisition, parameter input, running status instruction, data storage and display.
The present invention realizes the combination rotation test of revolution and rotation, and carry out combined in real time observing and controlling, it provides the benefit that can be by the technology requirement in various different fuse emission processs, set inertia force and set centrifugal force, and may be combined and test, solving the problem of fuse comprehensive performance test, platform structure is reasonable, test bit is accurate, and detection process is easy, can ensure that fuse quality monitoring is safe and reliable.
Accompanying drawing explanation
Fig. 1 is the structural representation that the present invention combines rotation platform.‘
In figure: 1 power shaft, 2 mechanical differentials, 3 axis of rotation, 4 fuse cabins, 5 glands, 6 trouserss, 7 turn, 8 supports, 9 hollow shafts.
Fig. 2 is TT&C system theory diagram.
Specific embodiments
Being further described the detailed description of the invention of the present invention with embodiment below in conjunction with the accompanying drawings, following example are only used for clearly illustrating technical scheme, and can not limit the scope of the invention with this.
It is not enough for the invention aims to solve prior art, a kind of fuse emission security analogue test platform of design, it can the double environmental forces suffered in emission process of analog cartridge fuse, i.e. recoil inertia force and the operative condition of rotary centrifugal force, it is used for testing and examining the reliability of fuze safety mechanism effect, test is divided into three parts, i.e. individually revolution is used for testing fuse axial inertia force, individually from being diverted to test fuse radial centrifugal force, revolution is combined with rotation, inertia force and centrifugal force that fuse produces in emission process can be simulated, and be adjusted in real time by technology requirement integration and control.The transmission of described hollow shaft 9 uses magneto high-speed electric expreess locomotive, and revolve round the sun rotating speed: 0-8000r/min;The transmission of the described axis of rotation 1 uses magneto high-speed electric expreess locomotive, rotation rotating speed: 0-10000r/min.
Realizing the purpose of the present invention and adopted the technical scheme that a kind of fuse emission security analogue test platform of offer, it is by combining rotation platform and TT&C system forms.Described combination rotation platform, it is turned by high speed vortex filament bevel gear mechanical differential, dynamic balancing, servo-actuated fuse cabin, revolution high-speed permanent magnetic servomotor, rotation high-speed permanent magnetic servomotor etc. form.It includes: 1 power shaft, 2 mechanical differentials, 3 axis of rotation, 4 fuse cabins, 5 glands, 6 trouserss, and 7 turn, 8 supports, 9 hollow shafts.Its annexation is: described power shaft 1, fitted together by the axis of rotation 3 that described mechanical differential 2 and said two are symmetrical, described fuse cabin 4 is installed on the described axis of rotation 3, described fuse cabin 4 is compressed by described friction top 5, in order to prevent high speed rotating from producing the interference of air-flow, described trousers 6 is arranged in the exit orifice of the described axis of rotation 3, described turning 7 is arranged on described support 8, and described support 8 is arranged on described hollow shaft 9, sees structural representation Fig. 1 of combination rotation platform.
Described TT&C system, it uses upper industrial computer to control technology and Automatic Measurement Technique, the various piece working order of combination rotation platform is carried out real-tune TT & C, it includes revolution control part, revolution feedback fraction, rotation control part, rotation feedback fraction, data process and data acquisition, parameter input, running status instruction, data storage, display, see theory diagram 2.
In order to ensure to combine safety during rotation platform operating, take the form of TT&C system and combination rotation platform isolated operation, be connected at a distance by controlling cable.
In order to ensure to combine safety during rotation platform operating, it is designed with the protective door automatically turned on, opens before and after test and be easily installed and dismantle testpieces, process of the test is closed for protecting the generation contingency injury to personnel.
Described turning 7 is that dynamic balancing is turned, and uses high-strength aluminum alloy manufacture.

Claims (4)

1. a fuse emission security analogue test platform, it, by combining rotation platform and TT&C system forms, is characterized in that: Test is divided into three parts: individually revolution is for testing the axial inertia force of fuse, individually from the radial direction being diverted to test fuse Centrifugal force, revolution combine with rotation, integration analog cartridge emission process in fuse generation inertia force and centrifugal force; Described combination rotation platform, it includes: power shaft (1), mechanical differential (2), the axis of rotation (3), fuse cabin (4), Friction top (5), trousers (6), turn (7), support (8), hollow shaft (9);Its annexation: described power shaft (1), fitted together by the axis of rotation (3) that described mechanical differential (2) is symmetrical with said two, the described axis of rotation (3) the described fuse cabin (4) of upper installation, described fuse cabin (4) is compressed by described friction top (5), described trousers (6) Be arranged in the exit orifice of the described axis of rotation (3), described in turn (7) be arranged on described support (8), described support (8) It is arranged on described hollow shaft (9);Described TT&C system, its upper industrial computer of employing controls technology and Automatic Measurement Technique, The various piece working order of combination rotation platform is carried out real-tune TT & C, and it includes: revolution controls part, revolution feedback section Point, rotation control part, rotation feedback fraction, data process and data acquisition, parameter input, running status instruction, count According to storing and display.
The most according to claim 1, a kind of fuse emission security analogue test platform, is characterized in that: the described axis of rotation (1) Transmission use magneto high-speed electric expreess locomotive, rotation rotating speed: 0-10000r/min.
The most according to claim 1, a kind of fuse emission security analogue test platform, is characterized in that: described hollow shaft (9) Transmission use magneto high-speed electric expreess locomotive, revolve round the sun rotating speed: 0-8000r/min.
The most according to claim 1, a kind of fuse emission security analogue test platform, is characterized in that: described support (8) It is dynamic balancing support, uses high-strength aluminum alloy manufacture.
CN201610228065.0A 2016-04-08 2016-04-08 Fuze emission safety simulation test platform Pending CN105841561A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610228065.0A CN105841561A (en) 2016-04-08 2016-04-08 Fuze emission safety simulation test platform

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610228065.0A CN105841561A (en) 2016-04-08 2016-04-08 Fuze emission safety simulation test platform

Publications (1)

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CN105841561A true CN105841561A (en) 2016-08-10

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109405674A (en) * 2018-11-15 2019-03-01 北京理工大学 A kind of small-bore guided munition environmental simulation test test macro and its test method

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4193297A (en) * 1963-07-31 1980-03-18 Us Navy Infrared fuze test simulator
CN203349714U (en) * 2013-06-19 2013-12-18 中国人民解放军军械工程学院 Multiple-freedom-degree full-automatic fuze electromagnetic irradiation test stand
CN103487081A (en) * 2013-09-22 2014-01-01 中国工程物理研究院总体工程研究所 Double-environment test device in quick-acceleration centrifugal field
CN104501668A (en) * 2014-12-26 2015-04-08 中国人民解放军总装备部军械技术研究所 Fuse linear inertia safety simulating releasing device
CN105823383A (en) * 2016-03-31 2016-08-03 吉林市江机民科实业有限公司 Fuse launching safety simulation test platform

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4193297A (en) * 1963-07-31 1980-03-18 Us Navy Infrared fuze test simulator
CN203349714U (en) * 2013-06-19 2013-12-18 中国人民解放军军械工程学院 Multiple-freedom-degree full-automatic fuze electromagnetic irradiation test stand
CN103487081A (en) * 2013-09-22 2014-01-01 中国工程物理研究院总体工程研究所 Double-environment test device in quick-acceleration centrifugal field
CN104501668A (en) * 2014-12-26 2015-04-08 中国人民解放军总装备部军械技术研究所 Fuse linear inertia safety simulating releasing device
CN105823383A (en) * 2016-03-31 2016-08-03 吉林市江机民科实业有限公司 Fuse launching safety simulation test platform

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109405674A (en) * 2018-11-15 2019-03-01 北京理工大学 A kind of small-bore guided munition environmental simulation test test macro and its test method
CN109405674B (en) * 2018-11-15 2020-06-02 北京理工大学 Small-caliber guided ammunition environment simulation test system and test method thereof

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Application publication date: 20160810