Fluid dynamic device with thrust control shroud
A fluid power and thrust control technology, applied in the field of aircraft, can solve problems such as loud noise, achieve the effects of saving manufacturing costs, increasing the dynamic speed, improving responsiveness and controllability
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[0065] see figure 1 , which shows an aircraft 100 invented by the applicant which is intended for use in a variety of applications. The aircraft 100 is approximately 2.4 meters wide and includes a central load bearing space 110 that provides an operator (not shown) with a cockpit operating area 111 while maximizing the fluid available to enter the drum rotor fan 120 area of flow (i.e. airflow). The operator may sit in the cockpit 111 facing forward (as indicated by arrow 112). Airflow reaching the drum rotor fan 120 flows through the central region of the aircraft (that is, through the central load bearing space 110 ) and is radially exhausted by the rotor fan 120 . Radial airflow is redirected downward by shroud 130 . The mask 130 is formed of a flexible material. The lower portion of the shroud includes a rigid outer rim 140 . The rim 140 can be moved by the operator so that the shroud 130 can be deflected thereby changing the position of the exit area of the shroud...
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