Emission method and device
A technology of launching device and spinner, which is applied to weapons without explosives, throwing weapons, offensive equipment, etc., can solve the problems of high power, long range, short mover, etc., and achieve powerful effects
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0046] Such as figure 1 As shown, the rotator 1 adopts a light alloy disc with a radius of 30 meters, which is firmly supported by a support frame below, and the total weight can be controlled below 200 tons. The aircraft 2 is fixed on the edge by the controller 3. The controller adopts wireless The remote controller can also use a photoelectric controller. The controller can control the take-off direction and angle of the aircraft at any time. The motor 5 can make the rotator rotate through the transmission system 4. The transmission system can be a chain or a gear or a gearbox. Assuming that the weight of the aircraft is 50 Ton below, then select the generating set 6 of 2000 kilowatts-5000 kilowatts for use, can satisfy the take-off condition of 1 or more aircrafts. When in use, the power supply drives the rotator to rotate through the motor. When the rotating speed of the rotator exceeds 30 rpm, the take-off speed of the aircraft can be reached, and the controller is turned...
Embodiment 2
[0048] Such as figure 1 As shown, if the object to be launched is a missile or other objects with different purposes, the rotator can be designed and motors with different rotating speeds can be selected according to different purposes, which is easily done by those skilled in the art. Assuming that a 50kg missile is launched, a rotator with a radius of 5-10 meters can be used, and the motor can use 80,000 rpm, so the launch speed can reach more than 30km / s, and its power is enough to destroy any target in outer space. The object to be launched can be placed in the desired position of the rotator according to the specific situation. The launch timing and direction of the missile can be controlled at any time through the controller.
Embodiment 3
[0050] Such as figure 2 , image 3 As shown, the rotator adopts a concave body 7, and the rotator cover 8 is fixed above the concave rotator by a fixed bracket and does not rotate with the rotator. There is a slight gap between the rotator cover 8 and the rotator 7 so as not to affect the rotator 7. Rotation is as the criterion, and outlet 10 is arranged on rotator cover 8, and degausser 9 is arranged at the outlet, and outlet and degausser can be one group, also can be more than one group. The concave rotator 7 and the rotator cover 8 adopt super-strong magnetic materials, and there are steel projectiles 11 in the concave rotator 7, so that the concave rotator 7 and the rotator cover 8 have a magnetic attraction effect on the projectiles. Assuming that the concave rotator 7 adopts a radius It is a parabolic structure of 1 meter and a depth of 1 meter, with 100,000 grains of 2-gram heavy projectiles inside, a motor of 80,000 rpm, a generator set of 2000 kilowatts-5000 kilowa...
PUM
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com