| 摘要 |
An air cushion aircraft comprises a centre wing section, consisting of a carrying profile (1), a deflectable forward section (2), a fuselage (3), lateral plates (4), three-dimensional parts of the wing (5), engines (6), a tail assembly (7), a streamlined body (10) with a rigid receiver (11) and power drives (12). The carrying profile (1) of the centre wing section is limited by a flexible inflatable screen pneumatically connected to the rigid receiver (11) and to the plates (4), the aft section of the receiver (11) is located in the tail, the lateral section of the receiver (11) is located in the plates (4), and the forward section of the receiver (11) has a gap with respect to the carrying profile (1) which may be overlapped by the deflectable forward section (2). |
