FIELD: aircraft engineering.
SUBSTANCE: proposed device comprises the assembly to allow abutment of folded airfoils on aircraft airframe and lock. Said lock is composed of spring-loaded pushers. This device consists of a resilient band with tips composed of several parts each being provided with tensioner. Tips of every pair of adjacent parts and pushers are fitted in grooves made in airfoil suspension assemblies and locked by pyro locks of lock assembly. Said pushers are fitted at band tips as far as they go.
EFFECT: better aircraft aerodynamics.
2 cl, 3 dwg
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RU2820900C2 |
