Zobrazeno 1 - 10
of 11
pro vyhledávání: '"D. V. Nedel'ko"'
Publikováno v:
Russian Aeronautics. 63:767-770
A general method using a radiophotonic system for measuring blade deformations of a helicopter main rotor model is presented. Characteristics of this system are considered and a comparison is carried out to other similar approaches with different ope
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::06ceb0538b8b64f505f5f8499dd194da
https://doi.org/10.3103/s1068799820040261
https://doi.org/10.3103/s1068799820040261
Publikováno v:
Russian Aeronautics. 61:655-661
Methodological fundamentals of mathematical modeling for the main parachute of a rescue system for a normal category airplane in an emergency situation are presented. The sample calculation process of a real parachute deployment is described and its
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::59347e5ba30bd30c80b5cc4674d005d5
https://doi.org/10.3103/s1068799818040232
https://doi.org/10.3103/s1068799818040232
Autor:
S. A. Alimov, D. V. Nedel’ko
Publikováno v:
Russian Aeronautics. 61:183-186
This paper presents the results of calculating the energy criterion being proposed by an example of two types of skid landing gear for a multipurpose helicopter of transport category.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2069dd8e7fcae037d0a7e58d590a23ca
https://doi.org/10.3103/s1068799818020058
https://doi.org/10.3103/s1068799818020058
Publikováno v:
Russian Aeronautics. 60:523-527
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
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1593f6acc6d237e75dd2430086ba327c
https://doi.org/10.3103/s1068799817040079
https://doi.org/10.3103/s1068799817040079
Publikováno v:
Russian Aeronautics (Iz VUZ). 55:353-356
The methodical grounds for helicopter operation with respect to the technical condition for the state of the art of aeronautical engineering are analyzed and generalized. The most essential engineering solutions on developing the systems for monitori
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1401d3bafe57eb8de1a7c8294c128181
https://doi.org/10.3103/s1068799812040058
https://doi.org/10.3103/s1068799812040058
Autor:
D. V. Nedel’ko, S. A. Mikhailov
Publikováno v:
Russian Aeronautics (Iz VUZ). 55:305-309
The existing technique of rating the external loads on a helicopter with skid type landing gear according to Airworthiness Standards [1] is analyzed and the results of comparing with design and experimental studies are presented. The main existing pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4ee2dc8c37513ba270d5e71197760934
https://doi.org/10.3103/s1068799812030130
https://doi.org/10.3103/s1068799812030130
Autor:
D. V. Nedel’ko, S. A. Mikhailov
Publikováno v:
Russian Aeronautics (Iz VUZ). 55:151-157
A new approach to the design-systematic provision of autorotation landing safety for a helicopter with skid type landing gear is proposed. We analyzed the existing simulation techniques and experimental studies regarding this problem. The main existi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::43896474ec322e69adaf7d0b48815d6d
https://doi.org/10.3103/s1068799812020067
https://doi.org/10.3103/s1068799812020067
Publikováno v:
Russian Aeronautics (Iz VUZ). 54:247-253
A technique is suggested for calculating the helicopter spatial motion and the stress-strain state of a skid landing gear in the course of landing with regard for the second landing impact; geometric, material and design nonlinearity of undercarriage
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0453b7763b33e7e18eb86bc41a3a5e19
https://doi.org/10.3103/s1068799811030032
https://doi.org/10.3103/s1068799811030032
Publikováno v:
Russian Aeronautics (Iz VUZ). 53:369-374
We compare the results of analyzing the stress strain state for the tubular skid landing gear with regard for the physically and geometrically nonlinear scheme of deformation; the analysis is carried out by the finite element method and with the aid
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::093683046f0b0d217d379460dc86e270
https://doi.org/10.3103/s106879981004001x
https://doi.org/10.3103/s106879981004001x
Publikováno v:
Russian Aeronautics (Iz VUZ). 53:9-15
A technique is proposed for calculating the stress strain state and power intensity of helicopter skid landing gear springs operating under conditions of dynamic loading taking into account a physically and geometrically nonlinear deformation scheme.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4c048938e10e78d1e59fe5a1adc761b1
https://doi.org/10.3103/s1068799810010022
https://doi.org/10.3103/s1068799810010022