Firing device of soft launch type individual rocket projectile
A firing device and rocket technology, which is applied to weapon accessories, fuzes, offensive equipment, etc., can solve the problems of low overload of soft-launched individual rockets and cannot meet the needs of soft-launched individual rockets, and achieve The effect of convenient and reliable use, low cost, and controllable threshold
Pending Publication Date: 2019-04-02
北京恒星箭翔科技有限公司
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Problems solved by technology
The launch overload of soft-launched individual rockets is very low, and the "mechanical-fire cap" firing mode of the original system cannot meet the launch requirements of soft-launched individual rockets
Method used
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Embodiment Construction
[0043] The present invention will be described in detail below with reference to the drawings and embodiments.
[0044] This embodiment provides a firing device and firing method for soft-launched individual rockets, which can effectively control the firing problem of soft-launched individual rockets, and can avoid collisions caused by soft-launched individual rockets during daily service handling The rocket fired.
[0045] Such as Figure 1-6 As shown, the firing device is installed on the projectile body 6 and includes: an interlock component and a circuit control component;
[0046] The circuit control assembly includes a circuit board 3 with a firing control circuit, a battery 4 and a battery holder 5;
[0047] The battery holder 5 is a cylindrical cavity structure with an opening at one end and a via hole at the other end. The battery holder 5 is sleeved on the outer circumference of the battery 4, and the open end of the battery holder 5 is fixed on the elastic body 6; an extre...
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The invention discloses a firing device of a soft launch type individual rocket projectile. According to the firing device, the firing force of the soft launch type individual rocket projectile can beaccurately controlled through a firing mode of the mechanically and electrically integrated soft launch type individual rocket projectile composed of an interlocking component and a circuit control component, and the safety of the soft launch type individual rocket projectile during daily servicing treatment can be met; in addition, the firing mode combined by the interlocking component and the circuit control component is low in cost, high in reliability, strong in universality and can be widely used for the transformation of the soft launching of the individual rocket projectile; accordingto a firing force amplitude and a pulse width threshold value, a firing force threshold value response sliding block with a set weight and a spring with a set rigidity are arranged to realize the controllable firing force threshold value, and the usable range is wide and the application is convenient and reliable; the firing force threshold value response sliding block and the spring only respondto combined action of an oriented stress and the stroke of a firing mechanism during use, an impact of a non firing force of ammunition is effectively shielded during the daily servicing treatment, and the high insensitiveness of the links such as storage, transportation and carrying of the ammunition is realized.
Description
Technical field [0001] The invention relates to the field of ammunition firing control, in particular to a soft-launched single-soldier rocket firing device. Background technique [0002] Individual rockets are an infantry anti-tank attack weapon. It is simple to operate, light in weight, and powerful. Grassroots infantry units are still equipped with a large number of weapons and become a weapon for infantry to combat armor. However, due to its recoilless artillery launching method, the rockets are subject to high launch overload, and the tail smoke at the moment of launch is louder, and it cannot be launched in a semi-closed limited space, which limits the combat use of the weapon system. environment of. Especially in urban street fighting, it cannot give full play to its combat advantages. [0003] Soft-launched individual rockets are characterized by low launch overload and low smoke and flame noise. They can be used for combat in semi-confined spaces, and can effectively imp...
Claims
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IPC IPC(8): F42C15/24
CPCF42C15/24
Inventor 于剑桥蒋军
Owner 北京恒星箭翔科技有限公司