F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
F01D 9/00 (2006.01) B64D 29/00 (2006.01) F01D 5/14 (2006.01) F02C 7/00 (2006.01)
Patent
CA 2588470
The invention relates to a static gas turbine component comprising an inner and an outer annular support member and a plurality of circumferentially spaced radial struts (21) arranged between said support members for transmitting structural loads. Each of a plurality of said struts (21) comprises a load carrying core (24) rigidly fixed to both the inner and the outer support member forming a unitary carcass with the support members, an impact resistant shell (25) surrounding the core (24) , and an energy absorbing material (26) arranged between the core (24) and the shell (25) .
La présente invention concerne un composant de turbine de gaz statique comprenant un élément de support annulaire intérieur et un support annulaire extérieur et une pluralité d~étais radiaux (21) espacés sur la circonférence disposés entre lesdits éléments de support pour transmettre les charges structurelles. Chacun des étais (21) comprend un noyau de support de charge (24) fixé de façon rigide à la fois à l~élément de support intérieur et à l~élément de support extérieur formant une carcasse unitaire avec les éléments de support, une coque résistante aux chocs (25) entourant le noyau (24) et un matériau absorbant l~énergie (26) disposé entre le noyau (24) et la coque (25).
Dennison Associates
Volvo Aero Corporation
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