| 摘要 |
#CMT# #/CMT# The device has a flexible inflatable structure (1) that holds a weightless airfoil (2) for forming an auto-stable plane profile wing (3). The structure has a flanging beam (4), which modifies the lobe and the profile of an inflatable thrust wing (5) according to the respective flight tension to change the characteristics in flight phase. The structure and the plane of the weightless airfoil are separable by a Velcro(RTM: hook and loop fasteners). #CMT#USE : #/CMT# Device for modifying the lobe and the profile of an inflatable thrust wing by the variation of its flight incidence for traction of nautical and terrestrial vehicle and for practicing the free flight. #CMT#ADVANTAGE : #/CMT# The structure is deformable under the action of the beam. The device modifies the lobe and the profile of the inflatable thrust wing in a simple manner, and modifies the characteristics in flight phase in a simple manner. The device allows the lobe and the profile of the inflatable thrust wing to be decreased, when the user decreases the incidence of the wing in flight, and allows the lobe and the profile of the inflatable thrust wing to be increased, when the user increases incidence of the wing in flight in a simple manner. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a perspective view of a lobe and profile modifying device. 1 : Flexible inflatable structure 2 : Weightless airfoil 3 : Auto-stable plane profile wing 4 : Flanging beam 5 : Inflatable thrust wing. |
