FIELD: aeronautical engineering; tanker aeroplanes. SUBSTANCE: tanker aeroplane includes fuselage with operator's cabin in tail section, observation window for operator, wings, engines mounted on wing, alighting gear, tail unit, fuel system, fueling system including rigid refueling probe secured in lower portion of tail compartment of fuselage for lowering and telescopic extension which consists of two concentric tubes with fuel sensors at ends; tail unit is made in form of two stabilizers of vertical tail mounted on tips of horizontal tail. Refueling system includes additional raising probes secured on fuselage symmetrically relative to its longitudinal axis for turning in vertical plane relative to attachment unit; compartments for rope winches are provided on fuselage at points located at maximum distance from attachment units. Extension and retraction of each probe are effected by means of power hydraulic cylinder. EFFECT: enhanced efficiency and reliability. 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TANKER AEROPLANE | 1994 |
|
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