A review on nearly isothermal compression technology
Compressors can be described as the heart of a vapor compression refrigeration system,
circulating the working fluid in the system. Significant benefits can be gained from improving …
circulating the working fluid in the system. Significant benefits can be gained from improving …
Heats pipes for temperature homogenization: A literature review
N Blet, S Lips, V Sartre - Applied Thermal Engineering, 2017 - Elsevier
Heat pipes offer high effective heat transfer in a purely passive way. Other specific properties
of heat pipes, like temperature homogenization, can be also reached. In this paper, a …
of heat pipes, like temperature homogenization, can be also reached. In this paper, a …
Geared turbofan gas turbine engine architecture
DB Kupratis, FM Schwarz - US Patent 10,794,292, 2020 - Google Patents
A gas turbine engine typically includes a fan section, a compressor section, a combustor
section and a turbine section. A speed reduction device such as an epicyclical gear …
section and a turbine section. A speed reduction device such as an epicyclical gear …
Flexible support structure for a geared architecture gas turbine engine
ME Mccune, J Husband - US Patent 10,590,802, 2020 - Google Patents
(57) ABSTRACT A gas turbine engine includes a fan shaft that drives a fan that has fan
blades. A fan shaft support that supports the fan shaft defines a fan shaft support transverse …
blades. A fan shaft support that supports the fan shaft defines a fan shaft support transverse …
Flexible support structure for a geared architecture gas turbine engine
ME McCune, J Husband - US Patent 10,227,893, 2019 - Google Patents
(57) ABSTRACT A gas turbine engine according to an example of the present disclosure
includes, among other things, a fan shaft driving a fan having fan blades. A fan shaft support …
includes, among other things, a fan shaft driving a fan having fan blades. A fan shaft support …
Thrust efficient turbofan engine
J Sabnis - US Patent 10,047,699, 2018 - Google Patents
A disclosed turbofan engine includes a gas generator section for generating a gas stream
flow. A speed reduction device is driven by the power turbine. A propulsor section includes a …
flow. A speed reduction device is driven by the power turbine. A propulsor section includes a …
Fundamental gear system architecture
WG Sheridan - US Patent 10,221,770, 2019 - Google Patents
A fan drive gear system for a gas turbine engine includes a gear system that provides a
speed reduction between a fan drive turbine and a fan and a mount flexibly supporting …
speed reduction between a fan drive turbine and a fan and a mount flexibly supporting …
Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
WG Sheridan, KL Hasel - US Patent 9,816,443, 2017 - Google Patents
(57) ABSTRACT A gas turbine engine includes an engine centerline longitu dinal axis and a
fan section including a fan with fan blades and rotatable about the engine centerline …
fan section including a fan with fan blades and rotatable about the engine centerline …
Geared turbomachine fan and compressor rotation
WG Sheridan, ME McCune - US Patent 10,584,660, 2020 - Google Patents
An exemplary gas turbine engine includes a fan section including a fan rotor and at least
one fan blade. A fan pressure ratio across the at least one fan blade is less than 1.45 …
one fan blade. A fan pressure ratio across the at least one fan blade is less than 1.45 …
Geared architecture for high speed and small volume fan drive turbine
ME McCune, J Husband, FM Schwarz… - US Patent …, 2017 - Google Patents
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