A vertical takeoff and landing aircraft of folding type

The present invention relates to a folding type vertical takeoff and landing air vehicle. Folding vertical takeoff and landing air vehicle of the present invention is to provide a receiving space therein consisting of the divided plurality of the side cover body for forming the upper and the lower cover and to the side of these upper and lower cover forming the top and bottom surfaces and; First and second fixed plate and the fixture to be placed in the upper and the lower stacking interval arranged to be fixed to the inside of the main body; The first and second plurality of full traction link times that one end is hinged to the edge side of the positive-reverse rotation plate and the rotary plate is located between a fixed plate and by a drive source; The times doedoe entire upper and having a plurality each of the lower side of the hinge connection to the other end of the traction link information, rotating the folded or spread to cross the upper and downward alternately arranged and a plurality of first which the side cover connected to the end along , and the link member to the second joint link; Is provided to the link which is located on the outside of the first and second joint link to rotate by a drive source is configured to include a propeller for generating a thrust. Thus, folding the vertical take-off and landing according to the present invention consisting of the craft so as to selectively collapse or expand by a link that supports the plurality of propeller to a drive source route in the stationary adjacent a plurality of propellers to cross each other propellers are laminated to each other as arranged in a structure so that the volume when folded by making it to be housed in the main body can be minimized there is an advantage to increase the ease of transportation and storage. That is, the advantage is to increase the degree of freedom for the installation and operation because it is a form of storage, as well as the handling and storage free it is possible to minimize the occupied area of ​​the installation space in the body when not in use can be expected. Particularly, when it is not in flight all including the propeller components are installed in the outdoor according to maintain the stored state in the main body unattended operation of a multi-purpose vehicle for close monitoring for and perform a variety of missions, including meteorological the advantage of the benefits that can be expected.