CPC F01D 25/24 (2013.01) [F01D 5/28 (2013.01); F01D 25/005 (2013.01); F02C 7/25 (2013.01); F05D 2230/31 (2013.01); F05D 2230/90 (2013.01); F05D 2240/14 (2013.01); F05D 2250/283 (2013.01); F05D 2300/133 (2013.01)] | 19 Claims |
1. An engine casing comprising:
an inner shell circumferentially surrounding blades of a fan, a compressor, or a turbine;
an outer shell positioned around the inner shell;
a fire retardant material between the inner shell and the outer shell; and
an internal structure coupled to the inner shell and the outer shell, wherein a volumetric ratio of the internal structure and the fire retardant material between the inner shell and the outer shell is based on at least one of an area of implementation within an axial flow engine or a size of the axial flow engine.
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10. An apparatus comprising:
means for producing aerodynamic forces;
a casing positioned around the means for producing aerodynamic forces, the casing including a cavity between an inner radial surface of the casing and an outer radial surface of the casing;
means for retarding fire inside the cavity; and
means for providing structural support coupled to the inner radial surface and the outer radial surface, wherein a volumetric ratio of the means for providing structural support and the means for retarding fire within the cavity is based on at least one of an area of implementation of the casing in an axial flow engine or a size of the axial flow engine.
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