CN2416481Y

CN2416481Y - Shell for striking airplane and air paraboy

Info

Publication number: CN2416481Y
Application number: CN 00207371
Authority: CN
Inventors: 李国红
Original assignee: Individual
Current assignee: Individual
Priority date: 2000-04-07
Filing date: 2000-04-07
Publication date: 2001-01-24
Anticipated expiration: 2010-04-07

Abstract

The utility model relates to a military weapon of national defence, particularly a shell for striking an airplane and an air paraboy. The head part of a bullet of the shell is provided with an impact fulcrum. Three igniting circuits which are composed of fulcrum contacts, an igniting trigger, an igniting electric source, a one second delaying mains switch, remote-controlled receiver contacts and an automatic destruction timer are arranged in the impact fulcrum. An automatic display circuit which is composed of a shell case mains switch, connection leads, a mileage displayer and a mileage fixing remote-controlled receiver is arranged in a shell case. The shell can randomly uses a controller to select a bullet explosion occasion. The utility model is provided with the contact type trigger, a self destruction device, the automatic displayer and a bullet flying mileage recording device.

Description

Be used to hit aircraft and aerial paratrooper's shell

The utility model relates to national defence troops' weapon, particularly a kind of shell that is used to hit aircraft and aerial paratrooper.

Except that guided missile, hitting aerial target particularly when a group of planes or paratrooper in the prior art, all kinds of shells still can not be adjusted to changed conditions and be selected the blast opportunity of bullet, have influenced the hazard boundary of bullet therefrom.

The purpose of this utility model is exactly in order to overcome above-mentioned weak point of the prior art, and provide a kind of can select the warhead detonation chance with remote controller arbitrarily and have the contact ignition and self-desttruction equipment and show bullet flight mileage automatically be used to hit aircraft and paratrooper's shell in the air.

The purpose of this utility model is achieved in that it is made up of bullet, shell case, the collision fulcrum is equipped with in the bullet head outside, the inboard is provided with the pair of contact of this fulcrum, the igniting blasting device also be housed in the bullet, ignite power supply, 1 second power switch of time-delay, receiver of remote-control sytem contact, destroy timer automatically, said igniting blasting device, ignite branch road that 1 second power switch three of power supply, time-delay constitutes respectively with fulcrum contact, receiver of remote-control sytem contact, destroy timer automatically and form three ignition loops in parallel; The backguy of 1 second power switch of time-delay is fixed on the shell case, the shell case power switch is housed in the shell case, the backguy of this switch is fixed on the bullet, cartridge case base is equipped with fixedly receiver of remote-control sytem of mileage display and the mileage that is connected with this display, said shell case power switch by connection lead and mileage display and mileage fixedly receiver of remote-control sytem form automatic show circuit; With the fixing remote control transmitter that cooperates of receiver of remote-control sytem of said receiver of remote-control sytem contact and mileage.

The utility model compared with prior art has the following advantages and good effect:

1, select warhead detonation opportunity with remote controller arbitrarily, aerial field, far and near target all can be adjusted to changed conditions and be reached best hazard boundary, particularly a group of planes, numerous paratrooper are had more very good lethal power.

(do not refer to not launch) when 2, this shell does not use, all ignition power circuits are all disconnected, and store, transport, use all safe and reliable.

3, after this shell emission, the mileage display on the shell case can constantly show the distance of bullet and firing base operation, after warhead detonation, can fix the distance of demonstration firing base to warhead detonation point exactly again on shell case.

4, the self-desttruction equipment that has of this shell can make the shell that departs from objectives ignite automatically under unlikely situation about damaging, and also can avoid shell to fall into the enemy simultaneously and cause and divulge a secret.

The explanation of accompanying drawing drawing:

Fig. 1 is a structural representation of the present utility model.

Fig. 2 is bullet of the present utility model, the structural representation when playing separable state.

Below in conjunction with drawings and Examples in detail the utility model is described in detail.

The utility model embodiment by collision fulcrum 1, fulcrum contact 2, bullet 3, igniting blasting device 4, ignite power supply 5, time-delay 1 second power switch 6, time-delay power switch backguy 7 in 1 second, shell case power switch 8, shell case 9, connect lead 10, fixedly receiver of remote-control sytem 11, mileage display 12, route protection shell 13, shell case power switch backguy 14 of mileage, destroy timer 15, receiver of remote-control sytem contact 16, remote control transmitter 17 etc. automatically and form.Bullet 3 heads of the present utility model outside installation shock fulcrum 1, the inboard is provided with the pair of contact 2 of this fulcrum 1, igniting blasting device 4, ignite power supply 5, time-delay 1 second power switch 6, receiver of remote-control sytem contact 16, destroy timer 15 automatically and also be installed in the bullet 3, said igniting blasting device 4, ignite branch road that 1 second power switch 6 three of power supply 5, time-delay constitute respectively with fulcrum contact 2, receiver of remote-control sytem contact 16, destroy timer 15 automatically and form three ignition loops in parallel.The power switch backguy 7 in 1 second of delaying time is fixed on the shell case 9, shell case power switch 8 is installed in the shell case 9, the backguy 14 of this switch is fixed on the bullet 3, shell case 9 bottoms dress peace mileage display 12 and the mileage that is connected with this display be receiver of remote-control sytem 11 fixedly, and said shell case power switch 8 is by the fixing receiver of remote-control sytem 11 formation loops of connection lead 10 and mileage display 12 and mileage.When the utility model breaks away from shell case 9 once emission bullet 3, delay time 1 second power switch 6 and shell case power switch 8 just opened (connection) immediately, mileage display 12 promptly constantly shows the flying distance of bullet 3 at this moment, the remote control manipulator of firing base is according to the distance of radar test aircraft and firing base like this, the distance that shows according to mileage display 12 just can be firing base best strike aircraft and paratrooper's remote control blast opportunity is provided again.When bullet 3 explosion times, when promptly remote control transmitter 17 sent initiation command, mileage fixedly receiver of remote-control sytem 11 promptly provided instruction, made mileage display 12 stop to show and fixing current demonstration record.Simultaneously, the connection of 1 second power switch 6 of time-delay provides precondition for realizing three kinds of detonation waies.The ignition loop of three parallel connections described in the utility model has provided three kinds of detonation waies, one, and firing base makes bullet 3 blasts with remote control transmitter 17 closed receiver of remote-control sytem contacts 16, conducting ignition loop; Its two, rely on the collision fulcrum 1 at bullet 3 tops and 2 conductings of fulcrum contact thereof to ignite the loop and make bullet 3 blasts; Its three, ignite the loop by automatic destruction timer 15 conductings and make bullet 3 blasts.

Shell case power switch 8 of the present utility model and connection lead 10 thereof are arranged in the route protection shell 13, and this route protection shell 13 is installed in the shell case 9.

Claims

1, a kind of shell that is used to hit aircraft and aerial paratrooper comprises bullet (3), shell case (9), it is characterized in that:

Collision fulcrum (1) is equipped with in a, bullet (3) the head outside, the inboard is provided with the pair of contact (2) of this fulcrum, igniting blasting device (4) also be housed in the bullet (3), ignite power supply (5), 1 second power switch (6) of time-delay, receiver of remote-control sytem contact (16), destroy timer (15) automatically, said igniting blasting device (4), ignite branch road that 1 second power switch (6) three of power supply (5), time-delay constitutes respectively with fulcrum contact (2), receiver of remote-control sytem contact (16), destroy timer (15) automatically and form three ignition loops in parallel;

The backguy (7) of b, 1 second power switch of time-delay is fixed on the shell case (9), shell case power switch (8) is housed in the shell case (9), the backguy of this switch (14) is fixed on the bullet (3), mileage display (12) is equipped with and the fixing receiver of remote-control sytem (11) of the mileage that is connected with this display in shell case (9) bottom, said shell case power switch (8) by connection lead (10) and mileage display (12) and mileage fixedly receiver of remote-control sytem (11) form automatic show circuit;

C, with the fixing remote control transmitter (17) that cooperates of receiver of remote-control sytem (11) of said receiver of remote-control sytem contact (16) and mileage.

2, the shell that is used to hit aircraft and aerial paratrooper according to claim 1 is characterized in that shell case power switch (8) and connects lead (10) being arranged in the route protection shell (13), and this route protection shell (13) is contained in the shell case (9).