Inventor
MOLLMANN DANIEL EDWARD
US22 patents
⚠️ This page may combine multiple inventors who share the name “MOLLMANN DANIEL EDWARD”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
GEN ELECTRIC
19 patentsUS6445995B1Sep 3, 2002
Vibration sensing in gas turbine engine
GEN ELECTRIC56 citations96
US7780410B2Aug 24, 2010
Method and apparatus for gas turbine engines
GEN ELECTRIC49 citations94
US6491497B1Dec 10, 2002
Method and apparatus for supporting rotor assemblies during unbalances
GEN ELECTRIC71 citations94
US7090464B2Aug 15, 2006
Methods and apparatus for assembling rotatable machines
GEN ELECTRIC20 citations90
US7260892B2Aug 28, 2007
Methods for optimizing turbine engine shell radial clearances
GEN ELECTRIC31 citations89
US7972109B2Jul 5, 2011
Methods and apparatus for fabricating a fan assembly for use with turbine engines
GEN ELECTRIC19 citations83
US6908285B2Jun 21, 2005
Methods and apparatus for assembling rotatable machines
GEN ELECTRIC17 citations81
US10422348B2Sep 24, 2019
Unsymmetrical turbofan abradable grind for reduced rub loads
GEN ELECTRIC2 citations73
US10920607B2Feb 16, 2021
Metallic compliant tip fan blade
GEN ELECTRIC3 citations72
US7416389B2Aug 26, 2008
Methods and apparatus for assembling rotatable machines
GEN ELECTRIC6 citations71
US11421877B2Aug 23, 2022
Vibration control for a gas turbine engine
GEN ELECTRIC0 citations62
US11111815B2Sep 7, 2021
Frangible gas turbine engine airfoil with fusion cavities
GEN ELECTRIC1 citations62
US12421864B2Sep 23, 2025
Controlling excitation loads associated with open rotor aeronautical engines
GEN ELECTRIC1 citations60
US7920973B2Apr 5, 2011
System and method for converting clearance data into vibration data
GEN ELECTRIC6 citations57
US7685876B2Mar 30, 2010
Methods and systems for balancing a rotatable member
GEN ELECTRIC5 citations54
US12116903B2Oct 15, 2024
Composite airfoils with frangible tips
GEN ELECTRIC0 citations52
US11434781B2Sep 6, 2022
Frangible gas turbine engine airfoil including an internal cavity
GEN ELECTRIC0 citations52
US12491988B2Dec 9, 2025
Controlling excitation loads associated with open rotor aeronautical engines
GEN ELECTRIC0 citations47
US12221893B2Feb 11, 2025
Controlling excitation loads associated with open rotor aeronautical engines
GEN ELECTRIC0 citations47