Assessment of conservatism level in an aircraft turbine engine design
US10592622B1 · kind B1 · utility
6Cited by
2References
18Claims
0Family size
Assignee
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Key dates
| Filing date | Oct 2, 2017 |
| Grant date | Mar 17, 2020 |
| Priority date | — |
| Expiry date | Jun 29, 2038 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG06F2119/04
- WIPO fieldComputer technology
- WIPO sectorElectrical engineering
Abstract
A system and method of analyzing an engine model is disclosed. The system and method include performing a Dynamic Systems Analysis on the engine model that includes modifying a transient allowance of the engine model to determine an optimal balance between performance and operability and assessing the conservatism level of the engine model.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.