Email this article Safety Analysis of Helicopter Autorotation Landing Execution on Conditions of Providing Skid Landing Gear Static Strength
- Authors: Ligai V.A.1, Nedel’ko D.V.1, Korotkov L.V.1
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Affiliations:
- PAO Kazan Helicopters
- Issue: Vol 60, No 4 (2017)
- Pages: 523-527
- Section: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230277
- DOI: https://doi.org/10.3103/S1068799817040079
- ID: 230277
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Abstract
The requirements for skid landing gear static strength ensuring are examined based on the comparative analysis of the Airworthiness Standards requirements. Probabilistic principle of determining the safety factor of the skid landing gear is presented. The analysis of the experimental data on bench and flight tests is performed for calculating the actual value of this factor.
About the authors
V. A. Ligai
PAO Kazan Helicopters
Email: ndv7350@mail.ru
Russian Federation, ul. Tetsevskaya 14, Kazan, 420085 Tatarstan
D. V. Nedel’ko
PAO Kazan Helicopters
Author for correspondence.
Email: ndv7350@mail.ru
Russian Federation, ul. Tetsevskaya 14, Kazan, 420085 Tatarstan
L. V. Korotkov
PAO Kazan Helicopters
Email: ndv7350@mail.ru
Russian Federation, ul. Tetsevskaya 14, Kazan, 420085 Tatarstan
