Business objective for the life cycle of aircraft
Journal Title: INCAS BULLETIN - Year 2019, Vol 11, Issue 0
Abstract
A structural-parametric analysis of the development of the global aviation market has been done and by the example of the development of the domestic helicopter industry, it was shown that the main revenue in the life cycle of aviation technology lies in the area of aviation service. The graphical model of the business objective in the development and operation of helicopters shows the need to maximize the service life of aircraft and reduce downtime. One of the forms that show these features was leasing with the inclusion of services in affiliated centers. At the request of the lessee, the leasing company may also provide additional services for advertising, recruitment, etc. Wet lease is mainly used by companies that manufacture special equipment or are engaged in wholesale activities in the field of aviation, i.e. in fact, they are monopolists. One of the ways to diversify sources of income is the sale of licenses for the production and maintenance of helicopters in the framework of the product lifecycle. Lost sales of helicopters for a holding company must be replenished through monopolization of the service and regulation of prices in this market. In general, the provision of service is a high-tech and profitable business. It requires constant monitoring and quality control of services at all stages of the life cycle of a helicopter. Income growth will be associated with an increase in the term and area of the business goal.
Authors and Affiliations
Mikhail Yu. KUPRIKOV, Lev N. RABINSKIY, Nikita M. KUPRIKOV
Keywords
Related Articles
- EP ID EP612833
- DOI 10.13111/2066-8201.2019.11.S.15
- Views 105
- Downloads 0
Aerodynamic performance prediction of Darrieus-type wind turbines
The prediction of Darrieus wind turbine aerodynamic performances provides the necessary design and operational data base related to the wind potential. In this sense it provides the type of turbine suitable to the area w...
About some relevant aspects regarding WENO type schemes on the shock tube problem
The paper is a continuation of the efficiency and accuracy analysis of different high order numerical schemes previously published by the authors [1-3]. After the analysis of advection equation and the scalar conservatio...
MDO approach for a two-stage microlauncher
The paper focuses on the multidisciplinary optimisation and preliminary design of a two-stage microlauncher capable of inserting a small 50 kg payload into Low Earth Orbit. The microlauncher is obtained using a MDO appro...
Book Review: Reviewed by Alexandra Emilia FORTIS. Advances in Flight Control SystemsEdited by Agneta BALINT Published by InTech, Croatia, 2011, pp. 296 ISBN 978-953-307-218-0, DOI: 10.5772/587
Numerical simulation of a DFB - fiber laser sensor (part 1)
This paper presents the preliminary results obtained in developing a numerical simulation analysis of fiber optic bending sensitivity aiming to improve the design of fiber lasers. The developed numerical simulation metho...