RM

Robert E. Malecki

RTX (Raytheon): 26 patents #297 of 15,912Top 2%
Overall (All Time): #151,916 of 4,157,543Top 4%
26
Patents All Time

Issued Patents All Time

Showing 25 most recent of 26 patents

Patent #TitleCo-InventorsDate
11970974 Gas turbine engine mounted above wing and with camber Andrew Stephen Hahn, Marc J. Muldoon, Jesse M. Chandler, Joseph B. Staubach 2024-04-30
11781447 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size Wesley K. Lord, Yuan J. Qiu, Becky E. Rose, Jonathan Gilson 2023-10-10
11781505 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size Wesley K. Lord, Yuan J. Qiu, Becky E. Rose, Jonathan Gilson 2023-10-10
11391216 Elongated geared turbofan with high bypass ratio Frederick M. Schwarz 2022-07-19
11286811 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size Wesley K. Lord, Yuan J. Qiu, Becky E. Rose, Jonathan Gilson 2022-03-29
11236701 Convergent divergent exit nozzle for a gas turbine engine Dmitriy B. Sidelkovskiy, Oleg Petrenko, Steven H. Zysman 2022-02-01
11015550 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size Wesley K. Lord, Yuan J. Qiu, Becky E. Rose, Jonathan Gilson 2021-05-25
10724541 Nacelle short inlet Yuan J. Qiu, Wesley K. Lord 2020-07-28
10479519 Nacelle short inlet for fan blade removal Yuan J. Qiu, Steven H. Zysman, Wesley K. Lord 2019-11-19
10450898 Track fairing assembly for a turbine engine nacelle Dmitriy B. Sidelkovskiy, Steven H. Zysman 2019-10-22
10436120 Exhaust nozzle for an elongated gear turbofan with high bypass ratio Frederick M. Schwarz 2019-10-08
10436121 Elongated geared turbofan with high bypass ratio Frederick M. Schwarz 2019-10-08
10371092 Convergent divergent exit nozzle for a gas turbine engine Dmitriy B. Sidelkovskiy, Oleg Petrenko, Steven H. Zysman 2019-08-06
10330047 Asymmetric fan nozzle in high-BPR separate-flow nacelle Wesley K. Lord 2019-06-25
10316757 Exhaust nozzle arrangement for geared turbofan Frederick M. Schwarz 2019-06-11
10301971 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size Wesley K. Lord, Yuan J. Qiu, Becky E. Rose, Jonathan Gilson 2019-05-28
10295420 Nacelle deflection measurement assembly Joshua V. Wood, Michael Joseph Murphy, Justin R. Urban, William W. Rice, David W. Lamarre 2019-05-21
10294871 Exhaust nozzle arrangement for geared turbofan Frederick M. Schwarz 2019-05-21
10145335 Turbomachine thrust reverser Robert L. Gukeisen, Claude Mercier 2018-12-04
10054059 Nacelle and compressor inlet arrangements Frederick M. Schwarz 2018-08-21
10006404 Gas turbine engine thrust reverser system 2018-06-26
9995180 Non-circular aft nacelle cowling geometry Michael Joseph Murphy 2018-06-12
9932933 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size Wesley K. Lord, Yuan J. Qiu, Becky E. Rose, Jonathan Gilson 2018-04-03
9920653 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size Wesley K. Lord, Yuan J. Qiu, Becky E. Rose, Jonathan Gilson 2018-03-20
9249731 Nacelle bifurcation for gas turbine engine Dmitriy B. Sidelkovskiy, Oleg Petrenko 2016-02-02