In-flight measured propulsion mass flow and thrust on aircraft
| dc.contributor.author | Lowe, K. Todd | en |
| dc.contributor.author | Byun, Gwi Bo | en |
| dc.contributor.author | Krejmas, Albert | en |
| dc.contributor.inventor | Lowe, Todd | en |
| dc.contributor.inventor | Byun, Gwi Bo | en |
| dc.contributor.inventor | Krejmas, Albert | en |
| dc.date.accessioned | 2024-12-12T20:41:54Z | en |
| dc.date.available | 2024-12-12T20:41:54Z | en |
| dc.date.issued | 2024-10-22 | en |
| dc.description.abstract | An aircraft includes a gas turbine engine and an optically-based measurement system. The gas turbine engine is configured to ingest a first mass flow and to exhaust a second mass flow. The optically-based measurement system is configured to determine the first and second mass flows in response to performing an imaging process on the gas turbine engine. | en |
| dc.description.version | Published version | en |
| dc.format.mimetype | application/pdf | en |
| dc.identifier.orcid | Lowe, Kevin [0000-0002-0147-4641] | en |
| dc.identifier.patentnumber | 12123313B2 | en |
| dc.identifier.uri | https://hdl.handle.net/10919/123786 | en |
| dc.language.iso | en | en |
| dc.rights | In Copyright | en |
| dc.rights.uri | http://rightsstatements.org/vocab/InC/1.0/ | en |
| dc.title | In-flight measured propulsion mass flow and thrust on aircraft | en |
| dc.type | Patent | en |
| dc.type.dcmitype | Text | en |
| pubs.organisational-group | Virginia Tech | en |
| pubs.organisational-group | Virginia Tech/Engineering | en |
| pubs.organisational-group | Virginia Tech/Engineering/Aerospace and Ocean Engineering | en |
| pubs.organisational-group | Virginia Tech/All T&R Faculty | en |
| pubs.organisational-group | Virginia Tech/Engineering/COE T&R Faculty | en |
| pubs.patent-status | Regular | en |