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Inventor profile of:

Daniel Edward Mollmann

City:

Cincinnati, Ohio

Country:

United States

Published Applications:

Last publication date:

2026-02-05

Top Assignees for applications by Daniel Edward Mollmann

The entities that hold a legal rights for patent applications filed by inventor Mollmann Daniel Edward:

GENERAL ELECTRIC COMPANY 16 Schenectady, NY United States
General Electric Company 3 Evendale, OH United States
General Electric Company Polska sp. z o.o 2 Warsaw, Poland
GENERALE ELECTRIC COMPANY 1 Evendale, OH United States
GENERALE ELECTRIC COMPANY POLSKA SP. Z O.O 1 Warsaw, Poland

Recent patent applications by Mollmann Daniel Edward

Daniel Edward Mollmann from Cincinnati, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2026-02-05

US20260036064A1

Mechanical engineering

CRUSHABLE BEARING RING FOR A FAN ASSEMBLY

#2 | 2026-01-15

US20260015950A1

Mechanical engineering

CONTROLLING EXCITATION LOADS ASSOCIATED WITH OPEN ROTOR AERONAUTICAL ENGINES

#3 | 2025-05-08

US20250146426A1

Mechanical engineering

CONTROLLING EXCITATION LOADS ASSOCIATED WITH OPEN ROTOR AERONAUTICAL ENGINES

#4 | 2024-02-15

US20240052755A1

Mechanical engineering

Controlling excitation loads associated with open rotor aeronautical engines

#5 | 2024-02-15

US20240052753A1

Mechanical engineering

CONTROLLING EXCITATION LOADS ASSOCIATED WITH OPEN ROTOR AERONAUTICAL ENGINES

#6 | 2024-02-15

US20240051656A1

Performing operations; transporting

CONTROLLING EXCITATION LOADS ASSOCIATED WITH OPEN ROTOR AERONAUTICAL ENGINES

#7 | 2023-01-05

US20230003129A1

Mechanical engineering

Composite airfoils with frangible tips

#8 | 2020-04-16

US20200116045A1

Mechanical engineering

Frangible gas turbine engine airfoil with fusion cavities

#9 | 2020-04-16

US20200116044A1

Mechanical engineering

Frangible gas turbine engine airfoil including an internal cavity

#10 | 2019-02-28

US20190063747A1

Mechanical engineering

Vibration control for a gas turbine engine

#11 | 2018-07-12

US20180195527A1

Mechanical engineering

Unsymmetrical turbofan abradable grind for reduced rub loads

#12 | 2014-03-06

US20140064937A1

Mechanical engineering

FAN BLADE BRUSH TIP

#13 | 2013-06-20

US20130156592A1

Mechanical engineering

Fan blade with composite core and wavy wall trailing edge cladding

#14 | 2009-10-22

US20090263247A1

Mechanical engineering

Dual rotor vibration monitoring

#15 | 2008-07-03

US20080159868A1

Mechanical engineering

Method and apparatus for gas turbine engines

#16 | 2008-07-03

US20080159854A1

Mechanical engineering

Methods and apparatus for fabricating a fan assembly for use with turbine engines

#17 | 2008-06-26

US20080152498A1

Mechanical engineering

Methods and systems for balancing a rotatable member

#18 | 2008-06-26

US20080149049A1

Physics

System and method for converting clearance data into vibration data

#19 | 2008-06-05

US20080127734A1

Physics

VIBRATION MEASUREMENT SYSTEM AND GAS TURBINE ENGINE INCLUDING THE SAME

#20 | 2006-09-21

US20060210402A1

Mechanical engineering

Methods and apparatus for assembling rotatable machines

#21 | 2006-01-19

US20060013692A1

Mechanical engineering

Methods and apparatus for assembling rotatable machines

#22 | 2006-01-19

US20060010686A1

Mechanical engineering

Methods and apparatus for assembling rotatable machines

#23 | 2005-06-30

US20050138806A1

Mechanical engineering

Methods for optimizing turbine engine shell radial clearances

#24 | 2005-06-21

US10409392

Methods and apparatus for assembling rotatable machines

InventorID:

298291 ⎘