000001935 001__ 1935
000001935 005__ 20141118153449.0
000001935 04107 $$acze
000001935 046__ $$k2011-05-09
000001935 100__ $$aNesládek, M.
000001935 24500 $$aFEM ANALYSES FOR DESIGN VERIFICATION OF AIRCRAFT ENGINE PARTS 

000001935 24630 $$n17.$$pEngineering Mechanics 2011
000001935 260__ $$bInstitute of Thermomechanics AS CR, v.v.i., Brno
000001935 506__ $$arestricted
000001935 520__ $$2eng$$aThe presented paper documents the concept and some major results of the heat transfer and stress analyses performed on a cylinder and a cylinder head of an aircraft piston engine. Both stress and temperature fields were computed by the FEM software Abaqus/CAE. The stresses in the assembly were calculated as a consequence of major mechanical loads together with the influence of the steady state temperature field on deformation. Several modifications of geometry were considered in the sense of their influence on cooling performance and strength. It should be noted that these analyses are preliminary and were performed for the purpose of supporting the engine design optimization. In the future prospects, it is assumed that all these models will be calibrated by data measured on the engine prototype in order to get more relevant results for the planned engine series.

000001935 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000001935 653__ $$aFEM analysis, aircraft piston engine, cylinder, cylinder head.

000001935 7112_ $$aEngineering Mechanics 2011$$cSvratka (CZ)$$d2011-05-09 / 2011-05-12$$gEM2011
000001935 720__ $$aNesládek, M.$$iŠpaniel, M.
000001935 8560_ $$ffischerc@itam.cas.cz
000001935 8564_ $$s1059226$$uhttps://invenio.itam.cas.cz/record/1935/files/p097.pdf$$y
             Original version of the author's contribution as presented on book, page 427.
            
000001935 962__ $$r1835
000001935 980__ $$aPAPER