Safety Analysis of Helicopter Autorotation Landing Execution on Conditions of Providing Skid Landing Gear Static Strength


Citar

Texto integral

Acesso aberto Acesso aberto
Acesso é fechado Acesso está concedido
Acesso é fechado Somente assinantes

Resumo

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.

Sobre autores

V. Ligai

PAO Kazan Helicopters

Email: ndv7350@mail.ru
Rússia, ul. Tetsevskaya 14, Kazan, 420085 Tatarstan

D. Nedel’ko

PAO Kazan Helicopters

Autor responsável pela correspondência
Email: ndv7350@mail.ru
Rússia, ul. Tetsevskaya 14, Kazan, 420085 Tatarstan

L. Korotkov

PAO Kazan Helicopters

Email: ndv7350@mail.ru
Rússia, ul. Tetsevskaya 14, Kazan, 420085 Tatarstan

Arquivos suplementares

Arquivos suplementares
Ação
1. JATS XML

Declaração de direitos autorais © Allerton Press, Inc., 2017