FIELD: aircraft engineering.
SUBSTANCE: proposed berth comprises rectangular mounting frame, control member parts locating and locking system. The latter comprises assy for location of small suspension bracket, assy for location of large suspension bracket and means for location and locking of aerodynamic body. The latter comprises the following components with appropriate location surfaces: retainers of the body lengthwise edge, proximal relative to suspension brackets; two body retainers at crosswise lateral edges on the side of the body proximal section relative to suspension brackets; two body retainers at crosswise lateral edges on the side of the body distal section relative to suspension brackets. Assemblies for location of both large and small brackets and retainers of body proximal lengthwise edge are arranged on one of the frame sides (reference side). Every said assy comprises mounting pin fitted in holders and arranged coaxially with mounting pin of the other assy. Every said retainer comprises locating support and means to press the body against aid support. Body retainers at crosswise lateral sides on the body proximal section side are opposed at mounting frame lateral sides adjoining the frame reference side. Retainers at crosswise lateral sides on the body distal section side are opposed at mounting frame lateral sides adjoining the frame reference side.
EFFECT: higher efficiency of assembly.
6 cl, 8 dwg
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Authors
Dates
2014-03-10—Published
2012-11-01—Filed