FIELD: testing.
SUBSTANCE: invention relates to static strength tests, namely to static tests of thin aerofoils of an aircraft. When implementing the method, a hole is made in the aerofoil, a tie-rod is drawn into the hole, the ends of the tie-rod are brought out beyond the sides of the aerofoil, wherein first end of tie-rod is secured on first side of aerofoil while load is applied to second end of tie-rod. Device comprises a tie-rod located in the hole of the aerofoil, so that the ends of the tie-rod protrude beyond the sides of the aerofoil, wherein said first end is secured at aerofoil first side while said second end is intended for load application.
EFFECT: improved strength properties of aerofoils of aircraft in places of load application during static tests of thin aerofoils without load-bearing elements, as well as increased reliability of test results.
6 cl, 4 dwg
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Authors
Dates
2024-07-30—Published
2024-02-20—Filed