Modularity of an aircraft turbomachine
US-2024003303-A1 · Jan 4, 2024 · US
US8998564B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8998564-B2 |
| Application number | US-201113047950-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 15, 2011 |
| Priority date | Mar 15, 2011 |
| Publication date | Apr 7, 2015 |
| Grant date | Apr 7, 2015 |
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An example method of reducing loads on a connection shaft includes disengaging a connection shaft from a motor-generator such that the connection shaft is not rotatably coupled to the motor-generator. The method communicates a fluid away from the motor-generator through a communication path established within the connection shaft. An example turbomachine connection shaft is configured to selectively rotatably couple a turbomachine rotor and a motor-generator. The connection shaft establishes a communication path that selectively vents the motor-generator.
Opening claim text (preview).
We claim: 1. A turbomachine connection shaft assembly, comprising: a connection shaft that is configured to selectively rotatably couple a turbomachine rotor and a motor-generator, the connection shaft establishing a communication path that selectively vents a fluid from the motor-generator, the communication path established within the connection shaft. 2. The turbomachine connection shaft assembly of claim 1 , wherein the fluid moves from the communicati…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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