Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: This invention is regarding an instrument (1) that is intended for use in the medical field for imaging and early diagnosis of larynx cancer. The instrument described in the invention involves LED illumination (1.1.3), which are driven at a frequency that is related to the fundamental frequency of the patient sound, a microphone (1.1.4) to acquire the fundamental frequency of the patient; an indirect laryngoscope section (1.1) that consists of a semi transparent mirror (1.1.1), and a power section (1.3) that provides the electrical current that is necessary to power up the instrument for early diagnosis of larynx cancer.

Abstract: A tissue identification device for determining the presence and borders of the cancerous tissues includes a measurement probe having a concentric, 2 port coaxial structure and enabling the 1 Port and 2 Port scattering parameters of the target tissue to be measured. An S parameter measurement unit is associated with the measurement probe via an RF/Microwave cable and allows the S parameters of the tissue to be measured. A computer identifies the tissue by means of an application software block and a tissue identification software block therein in line with the measurement results from the S parameter measurement unit. A hand tool carrying the measurement probe thereon during the measurement process operates simultaneously with the computer by being in communication therewith.