| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a tilt rotor aircraft and a tilt fan aircraft which take off and land vertically and in a short distance, and take off and land from an aircraft carrier, and a V/STOL aircraft of a turboshaft engine. <P>SOLUTION: Right and left engines are engaged with a variable ducted rotor provided in right and left main wings of a barycenter part by shaft interlock, and are configured to perform vertical, forward, and backward inclined rise from tilt control of duct equipment, and make adjustment control which can circle right and left from hovering, and in switching from a ring rotor upon cruise flight and fan flight to jet flight, a jet blowout amount increases gradually, a drive shaft to the ring rotor and a fan is stopped rotating by a clutch and a brake, and a ducted ring rotor and fan equipment are airtightly performed by slide doors of an upper and lower face of the main wings. <P>COPYRIGHT: (C)2013,JPO&INPIT |
