Erscheint 6 Ausgaben pro Jahr
ISSN Druckformat: 1948-2590
ISSN Online: 1948-2604
COMPARATIVE WEIGHT ANALYSIS OF FUSELAGE SECTIONS WITH DIFFERENT STRUCTURE LAYOUTS
ABSTRAKT
The results of forming a methodology and calculation algorithm to estimate the weight efficiency of fuselage sections with an advanced structure layout based on comparative analysis with alternative structure layouts are presented. Application of the developed methodology to estimate the weight efficiency of a lattice composite fuselage section of a passenger aircraft is shown.
-
Final Report Summary, ALASCA (Advanced Lattice Structures for Composite Airframes), Grant agreement ID: 265881, https://cordis.europa.eu/project/rcn/97744/reporting/en.
-
Final Report Summary, POLARBEAR (Production and Analysis Evolution for Lattice Related Barrel Elements under Operations with Advanced Robustness), Grant agreement ID: 605448, https://cordis.europa.eu/project/rcn/111110/reporting/en.
-
Fomin, V., Shanygin, A., and Zamula, G., Multilevel Approach for Strength and Weight Analyses of Composite Airframe Structures, in Proc. of 27th International Congress of the Aeronautical Sciences, Nice, France, Sept. 19-24, 2010.
-
Fomin, V., Multi-Modeling Approach in Pre-Designing of Fuselage Wing Section Consisted of Stiffened Composite Panels, in Proc. of 3rd Aircraft Structural Design Conference of Royal Aeronautical Society, Delft, Netherlands, 2012.
-
Dubovikov, E., Novel Approach and Algorithm for Searching Rational Nonconventional Airframe Concepts of New Generation Aircrafts, in Proc. of 28th International Congress of the Aeronautical Sciences, Brisbane, Australia, 2012.
-
Dubovikov, E., Fomin, V., Kondakov, I., Shanygin, A., and Zichenkov, M., Shell of Sealed Fuselage Compartment from Composites, Russian Patent RU 2558493, Federal Service for Intellectual Property, Russian Federation, 2015.
-
Chernov, A., Dubovikov, E., Fomin, V., Kondakov, I., and Shanygin, A., System of Protection of Airframe Load-Bearing Composite Elements, Russian Patent RU 2558494, Federal Service for Intellectual Property, Russian Federation, 2015.
-
Dubovikov, E., Fomin, V., Kondakov, I., and Shanygin, A., Weight Analysis of Alternative Fuselage Barrels on the Basis of the Multilevel Algorithm, in Proc. of the 3rd EASN Association International Workshop on Aerostructures, Milan, Italy, October 9-11, 2013.
-
Fomin, V., Ierusalimsky, K., Karpova, G., and Zamula, G., Analyzing the Effect of Skin Post-Buckling on General Stresses, Strains and Stability of Composite Structures, NASA Technical Report NCC1-233 ID 20010000336, 1998.
-
Fomin, V.P., Computing Cylindrical Stiffened Skins Accounting for Non-Linear Behavior of Structural Elements, Uch. Zap. TsAGI, 11(1):72-80, 1980.
-
Zamula, G.N. and Iyerusalimskii, K.M., To Stability Computation of Ribbed Cylindrical Skins, Uch. Zap. TsAGI, 12(3):83-94, 1981.
-
Dubovikov, E. and Fomin, V., Strength Analysis Technique for High Loaded Elements of Composite Airframes, in Proc. of 29th Congress of the International Council of Aeronautical Sciences (ICAS-2014), Saint Petersburg, Russia, 2014 (CD-ROM).
-
Kondakov, I.O., Development and Validation of Numerical Method for Strength Analysis of Lattice Composite Fuselage Structure, Nauch. Vestn. MGTU GA, 19(6):137-146, 2016.
-
Dubovikov, E., Fomin, V., and Kondakov, I., FE Modeling of Lattice Composite Fuselage Elements for General and Local Strength Analyses, in Proc. of 3rd EASN Association International Workshop on AeroStructures, Milano, Italy, 2013.