| 摘要 |
FIELD: transport.SUBSTANCE: invention relates to aircraft engineering, particularly, to designs of aircraft control devices. Mounting assembly (4) for cyclic pitch control lever (5) includes supporting structure (6) and instrument panel (20) attached to each other, connecting facilities (30) to connect the lever (5) with supporting structure (6). The connecting facilities (30) include longitudinally (32) elongated arm (31) one end (33) of which serves for supporting lever (5), guiding facilities (46, 48, 49) to connect the arm (31) with possibility of longitudinal movement to move the end (33) to/from supporting structure (6), and turning facility (49) to connect the arm (31) with supporting structure (6) with possibility to turn around horizontal axis (10) to adjust height of the mentioned end (33). The assembly (4) additionally contains the first detachable retaining facility (60) being manually actuated to stop arm (31) rotation relative to supporting structure (6) in required angular position, and the second detachable retaining facility (64) being manually actuated to stop arm (31) longitudinal movement relative to supporting structure (6). The first and the second detachable retaining facilities (60, 64) are mutually independent.EFFECT: possibility to adjust control devices according to body height and constitution of helicopter crew members.9 cl, 4 dwg |
