JB

Jeffrey S. Beattie

RTX (Raytheon): 26 patents #297 of 15,912Top 2%
Overall (All Time): #153,751 of 4,157,543Top 4%
26
Patents All Time

Issued Patents All Time

Showing 1–25 of 26 patents

Patent #TitleCo-InventorsDate
10907481 Platform cooling core for a gas turbine engine rotor blade Matthew Andrew Hough 2021-02-02
10822952 Feature to provide cooling flow to disk Jason D. Himes, Matthew Andrew Hough, Christopher Corcoran 2020-11-03
10563525 Blade feature to support segmented coverplate Matthew Andrew Hough, Christopher Corcoran 2020-02-18
10533453 Engine component having platform with passageway Matthew Andrew Hough, Tracy A. Propheter-Hinckley, San Quach 2020-01-14
10364682 Platform cooling core for a gas turbine engine rotor blade Matthew Andrew Hough 2019-07-30
10301958 Gas turbine engine with seal having protrusions Matthew Andrew Hough, Christopher Corcoran 2019-05-28
10253642 Gas turbine engine with disk having periphery with protrusions Matthew Andrew Hough 2019-04-09
10247023 Seal damper with improved retention Jeffrey Michael Jacques 2019-04-02
10227875 Gas turbine engine component with combined mate face and platform cooling Scott D. Lewis, Brandon M. Rapp, Matthew Andrew Hough, Bret M. Teller, Jeffrey Michael Jacques +1 more 2019-03-12
10226814 Cast component having corner radius to reduce recrystallization Max Asterlin, John R. Gunn 2019-03-12
10203196 Inspecting one or more apertures of a component using moldable material Gordon Miller Reed, James Romanelli, James M. Koonankeil, Kevin J. Klinefelter, Markus W. Fritch +1 more 2019-02-12
10180067 Mate face cooling holes for gas turbine engine component Scott D. Lewis, Mark F. Zelesky, Ricardo Trindade, Bret M. Teller, Jeffrey Michael Jacques +1 more 2019-01-15
10167722 Disk outer rim seal Matthew Andrew Hough 2019-01-01
10100648 Damper seal installation features David A. Niezelski, Joshua Daniel Winn 2018-10-16
9938837 Gas turbine engine airfoil trailing edge passage and core for making same Jeffrey R. Levine, Malcolm C. Staddon 2018-04-10
9932834 Rotor blade with a conic spline fillet at an intersection between a platform and a neck Matthew Andrew Hough 2018-04-03
9587495 Mistake proof damper pocket seals Jeffrey Michael Jacques 2017-03-07
9546556 Turbine blade root profile Jeffrey Michael Jacques 2017-01-17
9422817 Turbine blade root with microcircuit cooling passages Jeffrey Michael Jacques, Justin D. Piggush 2016-08-23
9279331 Gas turbine engine airfoil with dirt purge feature and core for making same Jeffrey R. Levine 2016-03-08
9243500 Turbine blade platform with U-channel cooling holes Mark F. Zelesky, Ricardo Trindade, Bret M. Teller, Scott D. Lewis, Jeffrey Michael Jacques +1 more 2016-01-26
8942837 Method for inspecting a manufacturing device James Romanelli, Jesse R. Boyer, Robert E. Erickson, Randall W. Joyner, Daniel A. Snyder +2 more 2015-01-27
8356978 Turbine airfoil platform cooling core Matthew A. Devore, Matthew S. Gleiner, Douglas C. Jenne 2013-01-22
8257045 Platforms with curved side edges and gas turbine engine systems involving such platforms Brandon W. Spangler, Scott D. Hjelm 2012-09-04
8240987 Gas turbine engine systems involving baffle assemblies Brandon W. Spangler 2012-08-14