Fuel supply system for hydrogen aircraft, and tank internal pressure adjustment method
US-2024263745-A1 · Aug 8, 2024 · US
US9017010B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9017010-B2 |
| Application number | US-201213362389-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 31, 2012 |
| Priority date | Jan 31, 2012 |
| Publication date | Apr 28, 2015 |
| Grant date | Apr 28, 2015 |
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An example turbomachine geared architecture support assembly includes a subpart having a more compliant portion and a less compliant portion. The less compliant portion includes a stop that limits axial movement of a geared architecture within a turbomachine.
Opening claim text (preview).
I claim: 1. A turbomachine geared architecture support assembly, comprising: a support having a more compliant portion and a less compliant portion, wherein the less compliant portion includes a stop that limits axial movement of a geared architecture within a turbomachine, the stop configured to be spaced from a rigid member during normal operation of a turbomachine that includes the geared architecture, the stop further configured to contact the rigid member during abnormal oper…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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