DJ

Daniel E. Molnar, Jr.

RA Rolls-Royce North America: 38 patents #7 of 447Top 2%
Rolls-Royce Plc: 36 patents #1,293 of 2,886Top 45%
AP American Panel: 1 patents #13 of 21Top 65%
LC L-3 Communications: 1 patents #229 of 507Top 50%
RD Rolls-Royce Deutschland: 1 patents #254 of 638Top 40%
CO Comcast: 1 patents #2,409 of 4,447Top 55%
Overall (All Time): #51,517 of 4,157,543Top 2%
51
Patents All Time

Issued Patents All Time

Showing 25 most recent of 51 patents

Patent #TitleCo-InventorsDate
12428974 Segmented variable fan outlet guide vane with unique actuation mechanisms Robert W. Heeter, Gregory J. Hebert 2025-09-30
12398648 Segmented variable fan outlet guide vane with cam assembly and pass through actuation mechanisms Robert W. Heeter, Gregory J. Hebert 2025-08-26
12398655 Segmented variable fan outlet guide vane with segment interface components Robert W. Heeter, Gregory J. Hebert 2025-08-26
12388322 Electric generator behind fan in turbine engine Robert W. Heeter, Brian S. Maners 2025-08-12
12320260 Segmented variable fan outlet guide vane with cam assembly and unique actuation mechanisms Robert W. Heeter, Gregory J. Hebert 2025-06-03
12292056 Segmented variable fan outlet guide vane with gear assembly Robert W. Heeter, Gregory J. Hebert 2025-05-06
12286930 Turbine engine fan case with bleed air for tip injection and heat exchanger cooling Robert W. Heeter, Jonathan M. Rivers 2025-04-29
12286936 Adjustable fan track liner with groove array active fan tip treatment for distortion tolerance Robert W. Heeter, Jonathan M. Rivers 2025-04-29
12258870 Adjustable fan track liner with slotted array active fan tip treatment for distortion tolerance Robert W. Heeter, Jonathan M. Rivers 2025-03-25
12215712 Adjustable fan track liner with dual grooved array active fan tip treatment for distortion tolerance Robert W. Heeter, Jonathan M. Rivers 2025-02-04
12209541 Adjustable fan track liner with dual slotted array active fan tip treatment for distortion tolerance Robert W. Heeter, Jonathan M. Rivers 2025-01-28
12209502 Active fan tip treatment using rotating drum array with axial channels in fan track liner for distortion tolerance Robert W. Heeter, Jonathan M. Rivers 2025-01-28
12168983 Active fan tip treatment using rotating drum array in fan track liner with axial and circumferential channels for distortion tolerance Robert W. Heeter, Jonathan M. Rivers 2024-12-17
12146413 Circumferentially variable flow control in fan outlet guide vane assemblies for distortion management and stall margin in gas turbine engines Robert W. Heeter, William B. Bryan, Gregory J. Hebert 2024-11-19
12085021 Adjustable air flow plenum with movable closure for a fan of a gas turbine engine Robert W. Heeter, Jonathan M. Rivers 2024-09-10
12078070 Adjustable air flow plenum with sliding doors for a fan of a gas turbine engine Robert W. Heeter, Jonathan M. Rivers 2024-09-03
12065979 Distributed electric and hybrid fans for distortion tolerance of turbofan engines Robert W. Heeter, Kathryn A. Sontag, Michael Meyer 2024-08-20
12065258 Multiple intake distortion adaptive fan for gas turbine engine Robert W. Heeter, Kathryn A. Sontag, Michael Meyer 2024-08-20
12066035 Adjustable depth tip treatment with axial member with pockets for a fan of a gas turbine engine Robert W. Heeter, Michael S. Krautheim 2024-08-20
12025059 Distributed electric tip fans for distortion tolerance of turbofan engines Robert W. Heeter, Kathryn A. Sontag, Michael Meyer 2024-07-02
12018621 Adjustable depth tip treatment with rotatable ring with pockets for a fan of a gas turbine engine Robert W. Heeter, Michael S. Krautheim 2024-06-25
12012865 Tailored material property tuning for turbine engine fan blades Michael George Glavicic, Matthew Jordan, Michael Meyer 2024-06-18
11970985 Adjustable air flow plenum with pivoting vanes for a fan of a gas turbine engine Robert W. Heeter, Jonathan M. Rivers, Michael S. Krautheim 2024-04-30
11965528 Adjustable air flow plenum with circumferential movable closure for a fan of a gas turbine engine Robert W. Heeter, Jonathan M. Rivers 2024-04-23
11946379 Turbine engine fan case with manifolded tip injection air recirculation passages Robert W. Heeter 2024-04-02