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Aircraft gas turbine thrust reverser, has detour elements arranged at peripheral region of cowl, and lever swingably arranged at rear end region of detour elements, where lever enables pivoting doors with displacement of detour elements
Aircraft gas turbine thrust reverser, has detour elements arranged at peripheral region of cowl, and lever swingably arranged at rear end region of detour elements, where lever enables pivoting doors with displacement of detour elements
The reverser has detour elements (29) arranged at a peripheral region of a cowl and displaceable along an axial direction of an engine i.e. gas turbine engine (10). A lever (33) is swingably arranged at a rear end region of the detour elements. The lever enables pivoting doors (30) with displacement of the detour elements. A pivotal axis of the doors is formed along a circumferential direction at the detour elements. The detour elements are secured at an annular element (31), and a bearing (32) of the lever is arranged at the annular element.
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