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Inventor profile of:

Daniel E. Molnar, JR.

City:

Indianapolis, Indiana

Country:

United States

Published Applications:

Last publication date:

2026-05-21

Top Assignees for applications by Daniel E. Molnar, JR.

The entities that hold a legal rights for patent applications filed by inventor Molnar, JR. Daniel E.:

Rolls-Royce North American Technologies, Inc. 30 Indianapolis, IN United States
ROLLS-ROYCE CORPORATION 21 INDIANAPOLIS, IN United States

Recent patent applications by Molnar, JR. Daniel E.

Daniel E. Molnar, JR. from Indianapolis, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2026-05-21

US20260139689A1

Mechanical engineering

FAN CASING OR LINER WITH INTERCHANGEABLE TIP TREATMENT SEGMENTS

#2 | 2026-05-21

US20260139606A1

Mechanical engineering

FAN WITH VARIABLE DEPTH GROOVE CASING TREATMENT

#3 | 2026-05-19

US18951580

Mechanical engineering

Fan with variable depth groove casing treatment

#4 | 2025-12-30

US18988283

Mechanical engineering

Electric generator in turbine engine

#5 | 2025-12-25

US20250389224A1

Mechanical engineering

INLETS FOR GAS TURBINE ENGINE FANS WITH DISTORTION TOLERANCE

#6 | 2025-11-27

US20250364872A1

Electricity

ELECTRIC GENERATOR BEHIND FAN IN TURBINE ENGINE

#7 | 2025-06-19

US20250198302A1

Mechanical engineering

TURBINE-POWERED SYSTEM WITH THERMOELECTRIC COOLING

#8 | 2025-04-29

US18660069

Mechanical engineering

Adjustable fan track liner with groove array active fan tip treatment for distortion tolerance

#9 | 2025-04-29

US18537256

Mechanical engineering

Turbine engine fan case with bleed air for tip injection and heat exchanger cooling

#10 | 2025-03-25

US18600620

Mechanical engineering

Adjustable fan track liner with slotted array active fan tip treatment for distortion tolerance

#11 | 2025-02-04

US18660073

Mechanical engineering

Adjustable fan track liner with dual grooved array active fan tip treatment for distortion tolerance

#12 | 2025-01-28

US18758996

Mechanical engineering

Active fan tip treatment using rotating drum array with axial channels in fan track liner for distortion tolerance

#13 | 2025-01-28

US18660065

Mechanical engineering

Adjustable fan track liner with dual slotted array active fan tip treatment for distortion tolerance

#14 | 2024-12-17

US18759050

Mechanical engineering

Active fan tip treatment using rotating drum array in fan track liner with axial and circumferential channels for distortion tolerance

#15 | 2024-12-12

US20240410293A1

Mechanical engineering

Electric Generator Behind Fan in Turbine Engine

#16 | 2024-11-19

US18537071

Mechanical engineering

Circumferentially variable flow control in fan outlet guide vane assemblies for distortion management and stall margin in gas turbine engines

#17 | 2024-09-26

US20240322646A1

Electricity

ELECTRIC GENERATOR BEHIND FAN IN TURBINE ENGINE

#18 | 2024-09-19

US20240309886A1

Mechanical engineering

Segmented variable fan outlet guide vane with gear assembly

#19 | 2024-09-19

US20240309775A1

Mechanical engineering

SEGMENTED VARIABLE FAN OUTLET GUIDE VANE WITH SEGMENT INTERFACE COMPONENTS

#20 | 2024-09-19

US20240309774A1

Mechanical engineering

SEGMENTED VARIABLE FAN OUTLET GUIDE VANE WITH PASS THROUGH ACTUATION MECHANISMS

#21 | 2024-09-19

US20240309773A1

Mechanical engineering

Segmented variable fan outlet guide vane with cam assembly and unique actuation mechanisms

#22 | 2024-09-19

US20240309772A1

Mechanical engineering

SEGMENTED VARIABLE FAN OUTLET GUIDE VANE WITH UNIQUE ACTUATION MECHANISMS

#23 | 2024-09-19

US20240309767A1

Mechanical engineering

SEGMENTED VARIABLE FAN OUTLET GUIDE VANE WITH CAM ASSEMBLY AND PASS THROUGH ACTUATION MECHANISMS

#24 | 2024-09-10

US18234650

Mechanical engineering

Adjustable air flow plenum with movable closure for a fan of a gas turbine engine

#25 | 2024-09-03

US18234656

Mechanical engineering

Adjustable air flow plenum with sliding doors for a fan of a gas turbine engine

#26 | 2024-08-20

US18234663

Mechanical engineering

Adjustable depth tip treatment with axial member with pockets for a fan of a gas turbine engine

#27 | 2024-07-25

US20240246688A1

Performing operations; transporting

Multiple intake distortion adaptive fan for gas turbine engine

#28 | 2024-06-27

US20240209796A1

Mechanical engineering

Distributed electric tip fans for distortion tolerance of turbofan engines

#29 | 2024-06-27

US20240209795A1

Mechanical engineering

Distributed electric and hybrid fans for distortion tolerance of turbofan engines

#30 | 2024-06-25

US18234657

Mechanical engineering

Adjustable depth tip treatment with rotatable ring with pockets for a fan of a gas turbine engine

#31 | 2024-04-30

US18234654

Mechanical engineering

Adjustable air flow plenum with pivoting vanes for a fan of a gas turbine engine

#32 | 2024-04-23

US18234661

Mechanical engineering

Adjustable air flow plenum with circumferential movable closure for a fan of a gas turbine engine

#33 | 2023-12-05

US18089029

Mechanical engineering

Electric fan array for distortion tolerance of turbofan engines

#34 | 2023-06-29

US20230203952A1

Mechanical engineering

Fan blade with internal shear-thickening fluid damping

#35 | 2023-01-24

US17561632

Mechanical engineering

Fan blade with internal magnetorheological fluid damping

#36 | 2021-04-29

US20210123347A1

Mechanical engineering

Gas turbine engine blades with airfoil plugs for selected tuning

InventorID:

5063861 ⎘