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Multi-pointer controller for controlling time and direction of curve flight

A technology of flight time and control curve, applied in the field of aviation science and technology, can solve the problems of losing function, being attacked by anti-missile system, and weak electricity is easily damaged by strong electromagnetic interference of the enemy.

Active Publication Date: 2014-04-30
盐城市荣意来纺机有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] In the era when the United States and Russia dominated missile technology, our country has not been able to compete with it. Missiles that can do curved flight to avoid anti-missile attacks. Recently, it was reported that Russia has developed a curved flight that has no anti-missile system to attack. missiles, but their control curve flight principle is mainly based on navigation, and modern warfare often has unpredictable situations, such as once the war starts, the satellite system is destroyed by the enemy and loses the automatic navigation function, or it is always controlled by navigation It will be discovered by the enemy very early and be attacked by the anti-missile system. In addition, another fatal weakness of navigation control is that they are all operated by weak current control. This weak electrode is easily damaged by the enemy's strong electromagnetic interference and loses its effect; it is best It is a device that does not need navigation and weak electricity to control, but can automatically control its curved flight without being tracked by the enemy through radio waves or damaged by the enemy's strong electromagnetic interference, so that it will not be damaged in the early and middle stages of missile launch. It is intercepted; as we all know, the missile is actually a parabola from launching to locking the attack target, that is to say, it is a line connecting two points between the launch point and the target point. If there is no anti-missile interception, the missile does not need to make a curved movement. However, in order to avoid anti-missile interception, it is necessary to make the missile advance in an irregular curve. It is easy to make such a curve. How to make the missile move forward in a curve and at the same time make the missile reset back to the point-to-point connection of the originally scheduled strike target On the track, this is the most critical; Wei Boqing's invention "201310230221.3 Watch Rotary Needle Ever-changing Curve Flight Automatic Return Direction Control Device" solved the problem of curved flight reset, another invention of Wei Boqing "201310458435.6 Clock Rotary Needle Strong Electricity Power-assisted rotation and automatic return direction controller" solves the problem of power conversion with strong electricity,

Method used

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  • Multi-pointer controller for controlling time and direction of curve flight
  • Multi-pointer controller for controlling time and direction of curve flight
  • Multi-pointer controller for controlling time and direction of curve flight

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Embodiment Construction

[0030] exist figure 1 In the embodiment shown in -11: the multi-pointer controller used to control the flight time and direction of the curve includes a B-axis 4-gear system with a helical spring leaf 40 as the rotating power, and two sets of three transmission gears are respectively housed C-axis 6-gear system and D-axis 8-gear system, two sets of E-axis 21 gear systems and F-axis 14 gear systems each equipped with two transmission gears, one set has five concentric central shafts that are nested together and each One end of the central shaft is equipped with a transmission gear and the other end is equipped with a pointer system with a heavy pointer; its characteristic is: a B-axis 4 gear system equipped with a helical spring 40 as the rotating power, and one end of the helical spring 40 is installed on the B-axis 4 , the other end is installed on the inner wall of the helical spring turntable 38 coaxial with the B-axis 4, and the helical spring turntable 38 is rotated so th...

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Abstract

The invention relates to a multi-pointer controller for controlling the time and the direction of curve flight. The controller comprises a B shaft gear system which is provided with spiral spring strips to be used as the rotating power, a C shaft gear system and a D shaft gear system which are respectively provided with three transmission gears, a E shaft gear system and an F shaft gear system which are respectively provided with two transmission gears, and a pointer system which is provided with five concentric center shafts sheathed together, wherein one end of each center shaft is provided with a transmission gear, and the other end of each center shaft is provided with a heavy pointer. The controller is characterized in that rotary spiral spring rotating discs of the B shaft gear system enable the spiral spring strips to tightly rotate around B shafts, thereby forming the restoring force of the spiral spring strips, i.e. the power to drive the spiral spring rotating discs; the tighter the spiral spring strips rotate, the bigger the restoring force of the spiral spring strips is; the faster the rotating speed of the spiral spring rotating discs in an anti-clockwise direction is, the less the time for rotating one circle for the spiral spring rotating discs; a timing control rotating disc is limited by a limit rod of the timing control rotating disc to only rotate one circle with 360 degrees.

Description

technical field [0001] The invention relates to a multi-pointer controller for controlling the time and direction of curved flight, which is suitable for the automatic control of curved flight and reset of all aircraft, and belongs to the field of aviation science and technology. Background technique [0002] In the era when the United States and Russia dominated missile technology, our country has not been able to compete with it. Missiles that can do curved flight to avoid anti-missile attacks. Recently, it was reported that Russia has developed a curved flight that has no anti-missile system to attack. missiles, but their control curve flight principle is mainly based on navigation, and modern warfare often has unpredictable situations, such as once the war starts, the satellite system is destroyed by the enemy and loses the automatic navigation function, or it is always controlled by navigation It will be discovered by the enemy very early and be attacked by the anti-mi...

Claims

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Application Information

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IPC IPC(8): F41G3/00
Inventor 魏伯卿
Owner 盐城市荣意来纺机有限公司
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