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公开(公告)号:US10890110B2
公开(公告)日:2021-01-12
申请号:US16469154
申请日:2018-04-19
申请人: ISTANBUL TEKNIK UNIVERSITESI , MITOS MIKRODALGA GORUNTULEME SISTEMLERI MUHENDISLIK SANAYI VE TICARET LIMITED SIRKETI
发明人: Guray Ali Canli , Ibrahim Akduman , Ismail Kurtoglu , Mehmet Cayoren , Hasan Ercan , Haluk Ali Yumlu
IPC分类号: F02B55/02 , F01C1/00 , F01C20/28 , F01C21/08 , F01M1/16 , F02B53/10 , F02B53/12 , F02B55/08 , F02B55/14 , F01C1/063 , F01C21/02 , F02B53/00
摘要: An internal combustion engine, includes a 1st rotor having two blades, rotating in the circular volume of the motor body block with variable angular speed; a 2nd rotor having two blades, rotating in the circular volume of the motor body block with variable angular speed, a rolling bearing provided between the 1st rotor and the 2nd rotor enables rotation of the 1st rotor and the 2nd rotor on each other; a 1st unidirectional rolling bearing between the 1st rotor and the back cover enables rotation of the 1st rotor and the 2nd rotor at different times and at different extents; a 3rd unidirectional rolling bearing transferring the 2nd rotor's rotation movements to the output shaft is provided on the internal collar of the 2nd rotor; a 4th unidirectional rolling bearing transferring the 1st rotor's rotation movements to the output shaft is provided on the internal collar of the 1st rotor.
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公开(公告)号:US11535375B2
公开(公告)日:2022-12-27
申请号:US16628731
申请日:2018-07-06
申请人: ISTANBUL TEKNIK UNIVERSITESI , MITOS MIKRODALGA GORUNTULEME SISTEMLERI MUHENDISLIK SANAYI VE TICARET LIMITED SIRKETI
发明人: Guray Ali Canli , Ibrahim Akduman , Ismail Kurtoglu , Mehmet Cayoren , Pelin Yavuz Gundogdu , Ibrahim Ozkol , Hasan Ercan , Muhammet Tarik Tamyurek
IPC分类号: B64C29/02 , B64D27/02 , B64C39/02 , B64B1/40 , B64B1/58 , B64C3/38 , B64C5/00 , B64C19/00 , B64C39/08 , B64D27/04 , B64D27/24 , B64D35/04 , B64C3/10 , B64C3/16 , B64C17/06
摘要: An autonomous unmanned aerial vehicle for land, sea and air use. The autonomous unmanned aerial vehicle is more specifically related to an unmanned aerial vehicle, wherein the autonomous unmanned aerial vehicle is configured to vertically take off and vertically land, fly with fixed wings and stay in the air silently for a long time by means of a balloon inflated behind it.
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