Abstract: Intake and exhaust valve seat inserts for aircraft cylinder heads. The inserts are configured for low pressure loss as inlet air and hot exhaust gas passes through the respective valve seat inserts. In an embodiment, the intake and exhaust valve seat inserts may have a plurality of faces or facets, at prescribed angles, in order to minimize pressure loss of gases passing therethrough. In an embodiment, rather than a plurality of faces or facets, the intake valve seat sidewall, and/or the exhaust valve seat sidewall may be provided in the configuration of a smooth curve approximating a set of selected angles, as if the component were made with a plurality of facets.

Abstract: An aircraft cylinder head with low pressure loss inlet passageways and exhaust passageways. In an embodiment, the combustion air inlet passageway includes a multi-lobed configuration that reduces pressure drop through the inlet passageway. In an embodiment, the hot exhaust gas passageway provides a shaped design that increases flow velocity yet reduces pressure drop. In an embodiment, an improved intake valve is provided, shaped to reduce creation of turbulence as inlet air flows past the inlet valve. In an embodiment, an improved exhaust valve is provided, shaped to reduce pressure losses as exhaust gases exit the cylinder.

Abstract: Intake and exhaust valve seat inserts for aircraft cylinder heads. The inserts are configured for low pressure loss as inlet air and hot exhaust gas passes through the respective valve seat inserts. In an embodiment, the intake and exhaust valve seat inserts may have a plurality of faces or facets, at prescribed angles, in order to minimize pressure loss of gases passing therethrough. In an embodiment, rather than a plurality of faces or facets, the intake valve seat sidewall, and/or the exhaust valve seat sidewall may be a provided in the configuration of a smooth curve approximating a set of selected angles, as if the component were made with a plurality of facets.

Abstract: An aircraft cylinder head with low pressure loss inlet passageways and exhaust passageways. In an embodiment, the combustion air inlet passageway includes a multi-lobed configuration that reduces pressure drop through the inlet passageway. In an embodiment, the hot exhaust gas passageway provides a shaped design that increases flow velocity yet reduces pressure drop. In an embodiment, an improved intake valve is provided, shaped to reduce creation of turbulence as inlet air flows past the inlet valve. In an embodiment, an improved exhaust valve is provided, shaped to reduce pressure losses as exhaust gases exit the cylinder.