19017029. GAS TURBINE ENGINE (General Electric Company)
GAS TURBINE ENGINE
Organization Name
Inventor(s)
Brandon Wayne Miller of Liberty Township OH US
Randy M. Vondrell of Newport KY US
David Marion Ostdiek of Liberty Township OH US
Craig William Higgins of Liberty Township OH US
Alexander Kimberley Simpson of Cincinnati OH US
Syed Arif Khalid of West Chester OH US
GAS TURBINE ENGINE
This abstract first appeared for US patent application 19017029 titled 'GAS TURBINE ENGINE
Original Abstract Submitted
A gas turbine engine includes: a turbomachine comprising a compressor section, a combustion section, and a turbine section arranged in serial flow order, the turbomachine defining an engine inlet to an inlet duct, a fan duct inlet to a fan duct, and a core inlet to a core duct; a primary fan driven by the turbomachine; and a secondary fan located downstream of the primary fan within the inlet duct, the gas turbine engine defining a thrust to power airflow ratio between 3.5 and 100 and a core bypass ratio between 0.1 and 10, wherein the thrust to power airflow ratio is a ratio of an airflow through a bypass passage over the turbomachine plus an airflow through the fan duct to an airflow through the core duct, wherein the core bypass ratio is a ratio of the airflow through the fan duct to the airflow through the core duct.
- General Electric Company
- Brandon Wayne Miller of Liberty Township OH US
- Randy M. Vondrell of Newport KY US
- David Marion Ostdiek of Liberty Township OH US
- Craig William Higgins of Liberty Township OH US
- Alexander Kimberley Simpson of Cincinnati OH US
- Syed Arif Khalid of West Chester OH US
- F02K3/065
- F02C3/06
- CPC F02K3/065