Propulsor fan array
MD Moore, IA Villa, D Jedamski, X Fei - US Patent 11,802,485, 2023 - Google Patents
A propulsor fan array having reduced noise emission is disclosed. The propulsor fan array
includes a plurality of propulsor fans that collectively generate thrust. Each of the propulsor …
includes a plurality of propulsor fans that collectively generate thrust. Each of the propulsor …
Multi-spool gas turbine engine architecture
E Durocher, K Morgan, L Mitrovic, J Dubreuil… - US Patent …, 2021 - Google Patents
A multi-spool gas turbine engine comprises a low pressure (LP) spool and a high pressure
(HP) spool independently rotatable about a central axis extending through an accessory …
(HP) spool independently rotatable about a central axis extending through an accessory …
Attritable engine additively manufactured inlet cap
LA Binek, JR Boyer, EJ Butcher, M Winter… - US Patent …, 2023 - Google Patents
A turbine engine has: a compressor; a combustor; a turbine, a gas flowpath passing
consecutively through the compressor, combustor, and turbine; and inlet member along the …
consecutively through the compressor, combustor, and turbine; and inlet member along the …
Propulsor wing trailing edge exhaust area control
MD Moore, IA Villa, D Jedamski - US Patent 12,006,891, 2024 - Google Patents
US12006891B2 - Propulsor wing trailing edge exhaust area control - Google Patents
US12006891B2 - Propulsor wing trailing edge exhaust area control - Google Patents Propulsor …
US12006891B2 - Propulsor wing trailing edge exhaust area control - Google Patents Propulsor …
Propulsor fan and drive system
MD Moore, IA Villa, D Jedamski, X Fei - US Patent 12,000,309, 2024 - Google Patents
A propulsor fan and drive system having reduced noise emission is disclosed. The propulsor
fan includes a blade fan having a plurality of blades. The blade fan is tensioned at the tips of …
fan includes a blade fan having a plurality of blades. The blade fan is tensioned at the tips of …
Attritable engine additively manufactured inlet cap
LA Binek, JR Boyer, EJ Butcher, M Winter… - US Patent …, 2022 - Google Patents
A turbine engine has: a compressor; a combustor; a turbine, a gas flowpath passing
consecutively through the compressor, combustor, and turbine; and inlet member along the …
consecutively through the compressor, combustor, and turbine; and inlet member along the …
Gas turbine
K Pirker, C Lauer - US Patent 10,428,656, 2019 - Google Patents
The present invention relates to a gas turbine, in particular an aircraft engine gas turbine
having a shaft and a bladed turbine rotor joined therewith that has a first rotor segment …
having a shaft and a bladed turbine rotor joined therewith that has a first rotor segment …