Inventor · disambiguated record
Razvan Virgil Florea
Also filed as: FLOREA RAZVAN · FLOREA RAZVAN VIRGIL
6 granted patents·4 pending applications·17 citations·filing 2004–2018
76Inventor score
Top patents by PatentIndex Score
10 records- 0169US11498660B2Embedded engines in hybrid blended wing bodyUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 15, 2022·2 cites·17 claims
- 0259US10415505B2Non-axisymmetric fan flow pathUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 17, 2019·2 cites·12 claims
- 0359US9291101B2Gas turbine engine inlet wall designUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 22, 2016·3 cites·10 claims
- 0459US7610179B2Coupled parametric design of flow control and duct shapeUNITED TECHNOLOGIES CORP·Filed 2004·Granted Oct 27, 2009·8 cites·14 claims
- 0557US10968747B2Airfoil with thickened root and fan and engine incorporating sameRAYTHEON TECH CORP·Filed 2013·Granted Apr 6, 2021·2 cites·16 claims
- 0645US2016122005A1Embedded engines in hybrid blended wing bodyUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 0739US10220939B2Active airflow system and method of reducing drag for aircraftSIKORSKY AIRCRAFT CORP·Filed 2016·Granted Mar 5, 2019·0 cites·7 claims
- 0838US2015354501A1Non-Axisymmetric Exit Guide Vane DesignUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 0934US2016144972A1Blended Wing Body Boundary Layer Ingesting Inlet Design IntegrationUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 1032US2017096212A1Drag reduction of high speed aircraftSIKORSKY AIRCRAFT CORP·Filed 2016·Application pending·0 cites
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