US Patent 12129802 Selective power distribution for an aircraft propulsion system
All edits
Edits on 30 Oct, 2024
Golden AI
Edits made to:
Infobox (+17 properties)
Article (+723 characters)
US Patent 12129802 Selective power distribution for an aircraft propulsion system
Article
Patent abstract
An assembly is provided for an aircraft propulsion system. This assembly includes a compressor section, a combustor section, a turbine section and a flowpath extending sequentially through the compressor section, the combustor section and the turbine section. The assembly also includes a turbine rotor, a propulsor rotor and an auxiliary turbine. The turbine rotor is within the turbine section. The turbine rotor is configured to rotatably drive the propulsor rotor. The auxiliary turbine includes an auxiliary turbine rotor. The auxiliary turbine rotor is configured to rotatably drive the propulsor rotor with the turbine rotor. The auxiliary turbine is configured to receive bleed gas from the flowpath.
Infobox
Is a
Patent Applicant
Patent Jurisdiction
Patent Number
Patent Inventor Names
Paul R. Hanrahan0
Date of Patent
October 29, 2024
0Patent Application Number
179036810
Date Filed
September 6, 2022
0Patent Citations
Patent Primary Examiner
Find more entities like US Patent 12129802 Selective power distribution for an aircraft propulsion system
Use the Golden Query Tool to find similar entities by any field in the Knowledge Graph, including industry, location, and more.
