KR20090016833A - Wireless electric ignition rocket bin launch system - Google Patents

Abstract

The present invention relates to a wireless electric ignition rocket bin system, and more particularly to combat the birds by using sound effects to prevent dangerous situations that may occur in the aircraft due to birds inhabiting the airfield. The present invention relates to a launcher system configured, and in particular, in the present invention, it is possible to automatically ignite the bins mounted inside the launching guns by wireless electric ignition system rather than the fuse, as well as to install the bins more safely and securely. While there is a separate radio controller and a reception operation unit has a feature that can be used from a long distance.

Description

Wireless electric ignition rocket bin system {Birds extirpation rocket device}

The present invention relates to a wireless electric ignition rocket bin system, and more particularly to combat the birds by using sound effects to prevent dangerous situations that may occur in the aircraft due to birds inhabiting the airfield. The present invention relates to a launcher system configured, and in particular, in the present invention, it is possible to automatically ignite the bins mounted inside the launching guns by wireless electric ignition system rather than the fuse, as well as to install the bins more safely and securely. And a separate radio controller and a wireless rocket bomber launch system configured to be used at a long distance through a receiving operation unit.

In general, when an aircraft takes off and lands or flies at low altitudes, dangerous scenes frequently occur such as a bird on the runway or a nearby area being sucked into the propeller of the aircraft, causing the device to be damaged and colliding with the aircraft. In this case, if the aircraft is damaged, it can cause huge economic and time loss due to maintenance or repair of the damaged part and flight cancellation.

In order to prevent such damage from birds, the airfield generally uses a method of firing a rifle to combat birds, but the area of the rifle is less than the huge area of the airfield, so the bird's fighting effect is insignificant. As time goes by, algae become chronic and try to approach gradually. Unlike the past, the eradication effect is gradually producing a problem that the effect is gradually lowered.

On the other hand, in order to prevent damage caused by algae's loss of crops in orchards, agricultural areas or grain yards, a method of combating by installing a binge or noise or an acoustic device is used. In an effort to prevent birds from being approached, all of them are insufficient to be practical measures for combating birds, and a simpler and more practical alternative is required.

Examples of the above-mentioned workarounds include, but are not limited to, recently suspended triangular mirrors, reflecting sunlight, hanging nemesis models, turning on radios to inform the presence of birds' sonic generators and people using large amplifiers, flash lamps; Ultrasonic radiation; Roar and explosion; Magnetism rotates to generate a rotating magnetic field; Infrared light firing; A variety of devices have been provided, such as electrical sunlight consisting of rotating sunlight reflection, but these devices are not only effective in terms of their effectiveness, but also because of their complicated and many components, which can lead to increased manufacturing costs and high frequency of failure. It has a drawback that is remarkable.

The present invention has been made in order to solve the above problems, by implementing a wireless electro-ignition fired artillery to meet the original purpose of combating algae to accommodate a number of bins more robust and safe airfield It is an object of the present invention to provide a wireless electric ignition rocket bin system configured to combat the algae inhabiting the runway or the runway.

In order to achieve the above object, the wireless electric ignition type rocket bin control system of the present invention is equipped with a wireless controller that can remotely control the receiving operation unit, and the LED is installed after the bin is installed, the power supply is turned on to confirm the contact confirmation and preparation status It consists of a receiving operation unit, and provided a predetermined support plate so that a plurality of launch pads can be arranged side by side, each launch pad has a stopper bundle, and an electric ignition rocket is injected into the launch pad and launched. It is a wireless electric ignition rocket bin launch system that can be configured as a dragon bin.

According to the wireless electric ignition rocket drink tank launching system of the present invention implemented in the above manner, after the launch gun is configured in an extremely simple and simple manner, it is more efficient by confirming and igniting a bird at a distance through a wireless device in advance. And there is an effect that can ensure the safety of the user.

Hereinafter, the configuration of the present invention will be described in detail with reference to the accompanying drawings.

1 is a perspective view of a wireless electric ignition rocket bin launch system configured in accordance with a preferred embodiment of the present invention, Figure 2 is a circuit diagram showing the operating procedure of the radio controller configured in accordance with a preferred embodiment of the present invention, 3 is a circuit diagram showing an operation procedure of the receiving operation unit configured in accordance with a preferred embodiment of the present invention, Figure 4 is a circuit diagram showing an operation procedure of a firing gun constructed in accordance with a preferred embodiment of the present invention. FIG. 5 is an internal configuration diagram illustrating the rocket bin in accordance with the present invention in more detail, and FIG. 6 (a) (b) shows stepwise use of a bundle of stoppers which appears in a series of processes in which the bin is accommodated in a launch pad. State diagram.

The present invention relates to a wireless electric ignition rocket launching system that can control the access of birds by inducing a first explosion on the ground and a second explosion in the air by incorporating a rocket system that hops into the air to explosives. will be.

As shown in FIG. 1, the present invention includes a firing gun 30 capable of firing a plurality of bins 40 and a receiving operation unit 20 capable of applying power to the ignition device 43 of the bin 40. ) And a wireless controller 10 capable of remotely controlling the reception operation unit 20.

The launching gun 30 is fixed to the plurality of launching guns 30 on a predetermined support plate 36, as shown in (a) (b) of Figure 6, the support formed bent '' The plate 36 is erected at a predetermined inclination angle with the ground by two pairs of supporting legs formed at different lengths. As a result, the projectile 30 is directed to the ground at a predetermined angle so that the projectile 41 of the ignited bin 40 is raised to the ground.

The launching gun 30 is preferably manufactured in consideration of the size and shape of the bin (40), of course, to establish a suitable space that can accommodate the bin, of course, Figure 6a (b) A predetermined plug 32 is formed on the bottom surface of the launching gun so that electric power can be supplied to the inner space of the launching gun so that the electric power applied through the wire connection unit 31 reaches the plug 32 through the wire. The wire connection unit 31 is configured to be connected to the reception operation unit 20 in a wired manner as shown in FIG. 1.

On the other hand, the reception operation unit 20 is equipped with an LED, if the power supply is 0N after installation of the explosion bin, the status display unit 21 to see the contact confirmation and readiness at a glance, and the data transmission, reception status and receiving unit selection of the receiving unit , LED display unit 22 indicating ignition preparation, etc., read the received commands to the microcomputer board to perform commands according to the conditions, and the microcomputer controller 23 for various lamp LCD display and control work, DC 12V 4.5V, charging A power supply section 24 formed of a battery and a wireless transmission section 25 in which a communication radio section for packet communication is incorporated.

The reception operation unit 20 is operated by the operation of the radio controller 10 for remote control.

The wireless controller 10 is equipped with an LCD display, the status display unit 11 that can be seen at a glance the state occurring by the receiver as well as the regulator itself; Switch operation unit 12 which can select each receiving unit, the first to tenth bin 40 can be controlled by the soft touch button; It can be seen at a glance the wireless transmission and reception operation, the operation state of the ignition ready switch inside the controller, LED display unit 13 to display whether or not to select for each receiver by the LCD on the button; A microcomputer control unit 14 which reads all signals to the microcomputer board and determines various lamp LCD displays and control operations according to a satisfactory condition; A power saving mode 15 in which the power of the LCD and the radio is automatically turned off when the user's button input is not for several seconds (set value); A power supply unit 16 formed of DC9-12V and a rechargeable battery; It consists of; a wireless transceiver for embedding a communication radio part for packet communication.

On the other hand, the firing gun 30 that can be used by inserting the ignition bin 40 for the bird rocket ignited by the electric ignition system, not the fuse, until the ignition is made after the bin 40 is inserted into the firing gun. A control unit 34 having a stopper bundle 33 for fixing the bin 40, a power unit 35 capable of supplying power to a power supply unit at the lower part of the bin when the bin 40 is inserted, and Consists of a wire connection portion 31 that connects the portion coming from the power supply portion of the lower end of the launch pad with the receiver.

Referring to Figure 5 briefly described with reference to the configuration of the bin 40 is applied to the present invention, while the bin 40 is configured in a cylindrical shape through which the inside is penetrated by squeezing papers stacked in multiple layers, Inner space PE packing 44; Propellant 42; Projectiles (41); stacked in order to receive, and the upper and lower sides of the projectiles 41 was further provided with a packing made of thin paper. In addition, the upper side of the PE packing 44 is provided with a separate ignition device 43 to ignite the propellant 42 of the bin 40, in particular of the PE packing 44 The bottom surface is formed to penetrate a predetermined space so that the above-described plug 32 can be inserted and inserted therein, whereby the plug 32 drawn from the bottom surface of the PE packing 44 is connected to the ignition device 43 to apply electricity. It was to be able to supply.

The PE packing 36 has a locking jaw 45 formed on the outer circumference in a shape as shown in FIG. 5, which is a means for fixing the stopper bundle 20, which is a main part of the present invention.

The bin 40 having the above-described configuration is such that the propellant is primarily exploded by the application of electricity and there is no shortage of raising the projectile 41 of the bin 40 to the ground. In addition, the propellant 42 is further provided with a projectile 41 formed in another cylindrical body as described above, the projectile 41 is the inside of the bin due to the explosion of the propellant 42. It is a configuration that is separated from the bins while vertically rising along the space, the projectile 41 ascended into the air is another explosion due to the bin (not shown) accommodated inside.

And, each side of the launch pad is a stopper bundle 33, which is the main part of the present invention as shown in Fig. 6 is configured with a bundle cover, the stopper bundle 33 is a Utility Model Registration Application No. 20-2007-0013433 of the present application It is described in detail in the issue.

Hereinafter, a detailed operation and effects related to the wireless electric ignition type rocket bin launching system of the present invention will be described.

The present invention has been invented for the purpose of combating birds in advance by using the sound (explosion) effect in order to prevent dangerous situations that may occur in the aircraft due to birds near the aerodrome, in particular the existing ignition It is known that the ignition method by the wireless system that actively improves the method, so that the user can ignite several bins more safely and accurately from a long distance, it is a more efficient rocket bins launch pad.

First, the wireless electric ignition type rocket bomber launching system of the present invention will be described in detail with reference to FIGS. 1, 2, 3, and 4 as follows.

It is preferable to form a plurality of firing artillery 30 of the present invention, the explosion bin 40 inserted into the firing artillery 30 is a structure capable of firing the projectile 41, respectively.

The projectile 41 may be wired with the reception operation unit 20 so as to be able to launch wirelessly at a long distance, and may receive power, and the reception operation unit 20 may be operated by the radio controller 10. Can be. That is, the operator can freely perform the firing operation of the projectile 41 accommodated in the bin 40 by adjusting the radio controller 10 at a distance of 1 km-3 km as shown in FIG. Through the projectiles 41 can be launched continuously and each.

The LED display unit 13 of the radio controller 10 immediately displays the projected projectile 41 that can be easily identified by the operator.

As a result, after fixing a plurality of launching guns 30 near the airfield runway or runway, and then connected to the receiving operation unit 20, the explosion bin inserted into the launching gun 30 by adjusting the radio controller 10 of the operator. There is a feature that can ignite the 40 to automatically launch the projectile (41).

The explosion bin 40 fixed to the firing gun 30 through the above process is stimulated by the plug 32 and the ignition device 43 by the application of electricity through the wire connection portion 31 propellant of the explosion bin. 42 is ignited, and the firing is terminated by raising the projectile 41 due to the ignition propellant.

Embodiment described above is configured to help the understanding of the present invention, it is only one embodiment that can be applied to the present invention, the scope of the present invention is not limited to the above-described embodiment.

1 is a perspective view of a wireless electric ignition rocket bin launch system constructed in accordance with a preferred embodiment of the present invention.

Figure 2 is a circuit diagram showing an operating procedure of the radio controller configured according to an embodiment of the present invention.

Figure 3 is a circuit diagram showing the operating procedure of the receiving operation unit configured in accordance with a preferred embodiment of the present invention.

Figure 4 is a circuit diagram showing the operating procedure of the firing gun constructed by the preferred instant of the present invention.

Figure 5 is an internal configuration showing in more detail the rocket bins applied to the present invention.

Figure 6 (a) (b) is a step-by-step state of use of the stopper bundle appears in a series of processes in which the bin is accommodated inside the launch pad.

* Description of the symbols for the main parts of the drawings *

10. Wireless Controller 11. Status Display

12. Switch Control Unit 13. LED Display

14. Microcomputer control unit 15. Power saving mode

16. Power Supply 17. Wireless Transceiver

20. Receiving operation part 21. Status display part

22. LED display unit 23. Microcomputer control unit

24. Power Supply 25. Wireless Transceiver

30. Balsa 31. Wire connection section

32. Plug 33. Stopper bundle 34. Control part 35. Power part

36. Support plate 40. Bin

41. Projectile 42. Propellant

43. Ignition device 44. PE packing

Claims (5)

PE packing by forming a cylindrical body penetrating the inside; Propellant; In the rocket bin barrel launch pad for raising the bin by the ignition by sequentially stacking and receiving; After being accommodated inside the bin, the projectile to be fired is configured to be adjusted through a receiving unit capable of applying power to the ignition device of the bin and a wireless controller capable of remotely controlling the receiving unit. A wireless electric ignition rocket bomber launch system.  The method of claim 1, The reception operation unit is equipped with an LED, and after the installation of the bin, turn on the power status indicator that can see the contact confirmation and readiness at a glance, and the LED display unit indicating the data transmission, reception status and receiving unit selection, ignition preparation, etc. Microcomputer control unit that reads the received command to the microcomputer board and executes the command according to the conditions and performs various lamp LCD display and control work, DC 12V 4.5V, power unit formed of charging battery, and wireless communication unit for packet communication Wireless electro-ignition rocket explosion bin launch system, characterized in that configured to be formed as a built-in wireless transmitter. The method of claim 1, The wireless controller is equipped with an LCD display, a status display unit that can be seen at a glance the state of reception as well as the regulator itself, each receiver can be selected and the number 1 to 10 bins are controlled by a soft touch button You can see the control panel, wireless transmit / receive operation inside the controller, operation status of the ignition ready switch at a glance. Microcomputer control unit to determine various lamp LCD display and control operation accordingly, power saving mode in which the power of LCD and radio are automatically turned off when the user does not press the button for a few seconds (setting value), and DC9-12V charging battery Characterized in that the power supply, and configured to be formed as a wireless transceiver for the communication radio part for the closed-kit communication built-in Wireless electric ignition swill barrel rocket launching system. The method of claim 1, The firing gun includes a control unit having a stopper bundle for holding the bin and holding the bin until the ignition occurs, and a power unit capable of supplying power to the power supply of the lower part of the bin when the bin is inserted, respectively. Wireless ignition type rocket explosion barrel launch system, characterized in that configured to be formed by a wire connection unit for connecting the signal from the power supply unit at the bottom of the launch pad with the receiver. The method of claim 1, The bin is composed of a cylindrical shape through which the paper is compressed in several layers and penetrates the inside, and the PE packing, the propellant, and the projectile are sequentially stacked in the inner space, and the ignition apparatus is located above the PE packing. It is possible to ignite the propellant of the explosion bin, and to insert the plug into the bottom of the PE packing and the plug is connected to the ignition device is configured to supply the applied electricity to ignite the gunpowder Wireless ignition rocket bins launch system, characterized in that.

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