P

Inventor

NAUDET JACKY

FR28 patents
⚠️ This page may combine multiple inventors who share the name “NAUDET JACKY”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

SNECMA

24 patents
US5328327AJul 12, 1994

Stator for directing the inlet of air inside a turbo-engine and method for mounting a vane of said stator

SNECMA68 citations96
US5039277AAug 13, 1991

Variable stator vane with separate guide disk

SNECMA61 citations96
US4844694AJul 4, 1989

Fastening spindle and method of assembly for attaching rotor elements of a gas-turbine engine

SNECMA72 citations96
US4604030AAug 5, 1986

Compressor with variable incidence stator vanes

SNECMA81 citations96
US4730983AMar 15, 1988

System for attaching a rotor blade to a rotor disk

SNECMA64 citations95
US4706354ANov 17, 1987

Method of manufacturing a root pivot assembly of a variable incidence turbo-machine blade

SNECMA53 citations95
US6011617AJan 4, 2000

System for inspecting internal zones of a machine by optical fibre endoscopy

SNECMA23 citations92
US5277544AJan 11, 1994

Blade control rod and system of such rods

SNECMA29 citations92
US4595339AJun 17, 1986

Centripetal accelerator for air exhaustion in a cooling device of a gas turbine combined with the compressor disc

SNECMA30 citations92
US7500644B2Mar 10, 2009

Device for maintaining and positioning harnesses on a turbo-jet engine

SNECMA98 citations91
US5314303AMay 24, 1994

Device for checking the clearances of a gas turbine compressor casing

SNECMA38 citations90
US5161949ANov 10, 1992

Rotor fitted with spacer blocks between the blades

SNECMA64 citations90
US5288206AFeb 22, 1994

Turbo aero engine equipped with means facilitating adjustment of plays of the stator and between the stator and rotor

SNECMA41 citations89
US4750746AJun 14, 1988

Device for attaching a seal member to a shaft

SNECMA36 citations87
US5466122ANov 14, 1995

Turbine engine stator with pivoting blades and control ring

SNECMA27 citations85
US7438492B2Oct 21, 2008

Link between two mechanical members

SNECMA13 citations78
US5224820AJul 6, 1993

Operating mechanism for variably settable blades of a turbomachine

SNECMA20 citations78
US5319850AJun 14, 1994

Method of fixing stemmed blade for a flow-straightening stage of a gas turbine engine

SNECMA9 citations73
US5236304AAug 17, 1993

Stemmed blade for a flow-straightening stage of a gas turbine engine and method of fixing said blade

SNECMA10 citations73
US4787820ANov 29, 1988

Turbine plant compressor disc with centripetal accelerator for the induction of turbine cooling air

SNECMA13 citations73
US5096377AMar 17, 1992

Turboshaft engine casing joint with reinforced axial restraint

SNECMA13 citations71
US5000659AMar 19, 1991

Temporary locking system for variably settable stator blades

SNECMA10 citations71
US4732536AMar 22, 1988

Turbo-machine compressor with variable incidence stator vanes

SNECMA14 citations69
US5919032AJul 6, 1999

Bladed disk with three-root blades

SNECMA15 citations67

SNECMA MOTEURS

4 patents