Title:
ROTATING MISSILE LAUNCHER
Document Type and Number:
Japanese Patent JP2021176464
Kind Code:
A
Abstract:
To provide a launcher capable of reducing friction resistance of a rotating missile shaft that is like a bamboo dragonfly and of easily performing high-speed rotation by using a bearing.SOLUTION: Bearings (2)(3) are installed at an upper end of a support body (1), provided with a rotating missile shaft setting hole (4), and is provided with a bearing (5) opposite the bearings (2)(3) with the rotating missile shaft setting hole (4) in between. A circular rubber string runway (6) is provided between the bearings (2)(3) and the bearing (5), circular rubber string removal prevention guides (7)(8) that are arch-shaped are installed near both ends of the circular rubber string runway (6), and reduction of friction resistance and an increase of speed of rotation when the circular rubber string (9) is pulled by using the bearings (2)(3)(5) are possible.
More Like This:
| WO/2012/025653 | LIFTING DEVICE FOR MODEL GLIDERS/SAILPLANES |
Inventors:
HIGUCHI HIDEO
Application Number:
JP2020098920A
Publication Date:
November 11, 2021
Filing Date:
May 07, 2020
Export Citation:
Assignee:
HIGUCHI HIDEO
International Classes:
A63H27/14; A63H27/127; F41F7/00
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