Gas turbine engine component having vascular engineered lattice structure
DJ Mongillo, TA Propheter-Hinckley… - US Patent …, 2018 - Google Patents
A component according to an exemplary aspect of the present disclosure includes, among
other things a wall and a vascular engineered lattice structure formed inside of the wall. The …
other things a wall and a vascular engineered lattice structure formed inside of the wall. The …
Multi-branch furcating flow heat exchanger
DJ Erno, WD Gerstler - US Patent 10,995,996, 2021 - Google Patents
A heat exchanger is provided. The heat exchanger (40) provides a first plurality of tubes (50)
and a second plurality of flow passages (52) which furcate near one of the first (42) and …
and a second plurality of flow passages (52) which furcate near one of the first (42) and …
Gas turbine engine component having vascular engineered lattice structure
MF Zelesky, JH Wagner… - US Patent …, 2018 - Google Patents
A component according to an exemplary aspect of the present disclosure includes, among
other things, a wall and a vascular engineered lattice structure formed inside of the wall. The …
other things, a wall and a vascular engineered lattice structure formed inside of the wall. The …
Gas turbine engine component having vascular engineered lattice structure
DJ Mongillo, TA Propheter-Hinckley - US Patent 10,570,746, 2020 - Google Patents
Continuation-in-part of application No. A component according to an exemplary aspect of
the PCT/US2013/032202, filed on Mar. 15, 2013. present disclosure includes, among other …
the PCT/US2013/032202, filed on Mar. 15, 2013. present disclosure includes, among other …
Branched airfoil core cooling arrangement
MA Devore, ED Kaufman - US Patent 8,449,254, 2013 - Google Patents
An example airfoil cooling arrangement includes a airfoil wall having a first face and a
second face opposite the first face. The airfoil wall establishes a channel that is configured to …
second face opposite the first face. The airfoil wall establishes a channel that is configured to …
Turbine engine component wall having branched cooling passages
CP Lee - US Patent 9,234,438, 2016 - Google Patents
In accordance with a first aspect of the present invention, a component wall in a turbine
engine is provided. The compo nent wall comprises a Substrate and at least one cooling pas …
engine is provided. The compo nent wall comprises a Substrate and at least one cooling pas …
Fractal fluid passages apparatus
K Adriany, E Bayat, N Garrett, R Pedersen… - US Patent …, 2019 - Google Patents
US10267515B2 - Fractal fluid passages apparatus - Google Patents US10267515B2 - Fractal
fluid passages apparatus - Google Patents Fractal fluid passages apparatus Download PDF …
fluid passages apparatus - Google Patents Fractal fluid passages apparatus Download PDF …
Fractal heat transfer device
A Poltorak - US Patent 10,041,745, 2018 - Google Patents
A heatsink comprising a heat exchange device having a plurality of heat exchange elements
each having a surface boundary with respect to a heat transfer fluid, having successive …
each having a surface boundary with respect to a heat transfer fluid, having successive …
Cooling module design and method for cooling components of a gas turbine system
CP Lee, HA Zuniga, JA Morrison, BJ Kolsrud… - US Patent …, 2016 - Google Patents
A cooling arrangement in a gas turbine system (120). The arrangement includes a plurality
of flow network units (208) to transfer heat to cooling fluid, at least one unit including first …
of flow network units (208) to transfer heat to cooling fluid, at least one unit including first …
Multi-lobed cooling hole array
J Xu - US Patent 8,522,558, 2013 - Google Patents
A gas turbine engine component includes a wall having first and second wall surfaces and
first and second cooling holes extending through the wall. The first and second cooling …
first and second cooling holes extending through the wall. The first and second cooling …