FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering, particularly to means of lifting cargo by aircraft. Deflector device (3) for aircraft (A) is configured to be mounted on fuselage (2) of aircraft (A) to protect protruding element (1) from contact with external object (ER). Protruding element (1) is mounted on fuselage (2). Deflector device (3) comprises proximal anchor element (7), remote anchor element (6) and deflector inclined member (8) extending from proximal anchor element (7) towards remote deflector anchor element (6) along longitudinal direction (X) of deflector device (3). Proximal anchor element (7) includes connecting end member (39), which has sliding support (15) on which the innermost end (37) is located. Sliding support (15) has an axis (LT) of linear translational movement.
EFFECT: possibility to easily mount / dismantle the deflector device on an aircraft is reached.
15 cl, 9 dwg
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Authors
Dates
2018-03-26—Published
2016-12-16—Filed