Inventor
SCHILLING JAN C
US30 patents
⚠️ This page may combine multiple inventors who share the name “SCHILLING JAN C”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
GEN ELECTRIC
29 patentsUS6039542AMar 21, 2000
Panel damped hybrid blade
GEN ELECTRIC185 citations98
US5846050ADec 8, 1998
Vane sector spring
GEN ELECTRIC99 citations98
US5174525ADec 29, 1992
Structure for eliminating lift load bending in engine core of turbofan
GEN ELECTRIC123 citations98
US6033186AMar 7, 2000
Frequency tuned hybrid blade
GEN ELECTRIC91 citations97
US5190441AMar 2, 1993
Noise reduction in aircraft propellers
GEN ELECTRIC147 citations97
US6206631B1Mar 27, 2001
Turbomachine fan casing with dual-wall blade containment structure
GEN ELECTRIC62 citations96
US6139264AOct 31, 2000
Compressor interstage seal
GEN ELECTRIC68 citations96
US5993152ANov 30, 1999
Nonlinear vane actuation
GEN ELECTRIC77 citations96
US5490764AFeb 13, 1996
Unshrouded blading for high bypass turbofan engines
GEN ELECTRIC60 citations96
US5340280AAug 23, 1994
Dovetail attachment for composite blade and method for making
GEN ELECTRIC80 citations96
US5299914AApr 5, 1994
Staggered fan blade assembly for a turbofan engine
GEN ELECTRIC59 citations96
US6004101ADec 21, 1999
Reinforced aluminum fan blade
GEN ELECTRIC72 citations95
US5947688ASep 7, 1999
Frequency tuned hybrid blade
GEN ELECTRIC55 citations95
US5630319AMay 20, 1997
Dome assembly for a multiple annular combustor
GEN ELECTRIC55 citations95
US5102302AApr 7, 1992
Fan blade mount
GEN ELECTRIC47 citations95
US4913623AApr 3, 1990
Propeller/fan-pitch feathering apparatus
GEN ELECTRIC61 citations95
US4190397AFeb 26, 1980
Windage shield
GEN ELECTRIC75 citations93
US6357222B1Mar 19, 2002
Method and apparatus for reducing thermal stresses within turbine engines
GEN ELECTRIC41 citations92
US6233823B1May 22, 2001
Method of making plastically formed hybrid airfoil
GEN ELECTRIC16 citations92
US6099257AAug 8, 2000
Plastically formed hybrid airfoil
GEN ELECTRIC23 citations92
US6042334AMar 28, 2000
Compressor interstage seal
GEN ELECTRIC40 citations92
US5439354AAug 8, 1995
Hollow airfoil impact resistance improvement
GEN ELECTRIC28 citations92
US5354176AOct 11, 1994
Fan blade mount
GEN ELECTRIC25 citations92
US5282358AFeb 1, 1994
Gas turbine engine dual inner central drive shaft
GEN ELECTRIC41 citations92
US5205513AApr 27, 1993
Method and system for the removal of large turbine engines
GEN ELECTRIC40 citations92
US5165856ANov 24, 1992
Fan blade mount
GEN ELECTRIC32 citations92
US5188505AFeb 23, 1993
Structural ring mechanism for containment housing of turbofan
GEN ELECTRIC35 citations91
US5820346AOct 13, 1998
Blade damper for a turbine engine
GEN ELECTRIC39 citations85
US5503532AApr 2, 1996
Diffusion bonded airfoil and method
GEN ELECTRIC14 citations74