BT

Bret M. Teller

RTX (Raytheon): 24 patents #335 of 15,912Top 3%
Overall (All Time): #171,365 of 4,157,543Top 5%
24
Patents All Time

Issued Patents All Time

Patent #TitleCo-InventorsDate
11661852 Turbine blade trailing edge cooling feed Nicholas M. LoRicco, Parth Jariwala, Alex J. Schneider, Matthew S. Gleiner, Jeffrey T. Morton 2023-05-30
11168571 Airfoil having dead-end tip flag cavity David A. Niezelski, Timothy J. Jennings, John McBrien, Thomas N. Slavens 2021-11-09
11148191 Core arrangement for turbine engine component Matthew S. Gleiner, James Tilsley Auxier 2021-10-19
11143037 Turbine blade cooling hole arrangement Alex J. Schneider, Timothy J. Jennings, David A. Niezelski, Jeffrey T. Morton, Nicholas M. LoRicco 2021-10-12
11041390 Turbine airfoil having film cooling hole arrangement Christopher Cosher, Allan N. Arisi, Karl A. Mentz 2021-06-22
10871083 Turbine vane for gas turbine engine Christopher Cosher, Alex J. Schneider 2020-12-22
10844729 Turbine vane for gas turbine engine Allan N. Arisi 2020-11-24
10830054 Internally cooled airfoil James Tilsley Auxier, Parth Jariwala 2020-11-10
10815803 BOAS thermal protection Scott D. Lewis, Dominic J. Mongillo, Mark F. Zelesky, Russell Deibel, Matthew S. Gleiner 2020-10-27
10677071 Turbine vane for gas turbine engine Allan N. Arisi 2020-06-09
10641100 Gas turbine engine airfoil cooling passage configuration James Tilsley Auxier, Parth Jariwala, Mark F. Zelesky 2020-05-05
10508552 Internally cooled airfoil James Tilsley Auxier, Parth Jariwala 2019-12-17
10502067 Dual-fed airfoil tip Dominic J. Mongillo, Parth Jariwala, Mark F. Zelesky, James Tilsley Auxier 2019-12-10
10408071 BOAS thermal protection Scott D. Lewis, Dominic J. Mongillo, Mark F. Zelesky, Russell Deibel, Matthew S. Gleiner 2019-09-10
10406596 Core arrangement for turbine engine component Matthew S. Gleiner, James Tilsley Auxier 2019-09-10
10364680 Gas turbine engine component having platform trench Mark F. Zelesky, Scott D. Lewis, Brandon W. Spangler, Ricardo Trindade 2019-07-30
10337332 Airfoil having pedestals in trailing edge cavity James Tilsley Auxier 2019-07-02
10227875 Gas turbine engine component with combined mate face and platform cooling Scott D. Lewis, Brandon M. Rapp, Jeffrey S. Beattie, Matthew Andrew Hough, Jeffrey Michael Jacques +1 more 2019-03-12
10180067 Mate face cooling holes for gas turbine engine component Jeffrey S. Beattie, Scott D. Lewis, Mark F. Zelesky, Ricardo Trindade, Jeffrey Michael Jacques +1 more 2019-01-15
9797260 Engine component with wear surface protection Graham Ryan Philbrick, Ken Lagueux 2017-10-24
9243500 Turbine blade platform with U-channel cooling holes Mark F. Zelesky, Ricardo Trindade, Scott D. Lewis, Jeffrey S. Beattie, Jeffrey Michael Jacques +1 more 2016-01-26
7478994 Airfoil with supplemental cooling channel adjacent leading edge Frank J. Cunha, Edward F. Pietraszkiewicz, David M. Kontrovitz, Jeffrey R. Levine, Young H. Chon +1 more 2009-01-20
7131818 Airfoil with three-pass serpentine cooling channel and microcircuit Frank J. Cunha, Young H. Chon, Dominic J. Mongillo, Edward F. Pietraszkiewicz 2006-11-07
7097424 Micro-circuit platform Frank J. Cunha, Keith A. Santeler 2006-08-29