Inventor

SANDELIS DENIS JEAN MAURICE

FR44 patents

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

SANDELIS DENIS JEAN MAURICE

SNECMA

Dual-injector fuel injector system

Device for injecting a mixture of air and fuel, and a combustion chamber and turbomachine provided with such a device

Fuel injection system with improved air/fuel homogenization

Fuel injection assembly for a gas turbine engine

Combustion chamber end wall with ventilation

Chamber endwall, method of producing it, combustion chamber comprising it, and turbine engine equipped therewith

Combustion chamber of a turbomachine

Gas turbine engine diffuser and combustion chamber and gas turbine engine comprising same

Control of cooling flows for high-temperature combustion chambers having increased permeability in the downstream direction

Device for guiding an element in an orifice in a wall of a turbomachine combustion chamber

Configuration of dilution openings in a turbomachine combustion chamber wall

Injection system for a turbine engine combustion chamber configured for direct injection of two coaxial fuel flows

Annular combustion chamber for a turbine engine

Turbomachine combustion chamber shell ring

Annular combustion chamber in a turbine engine

Annular combustion chamber with a perforated wall

Annular combustion chamber of a gas turbine engine

Device for injecting a mixture of air and fuel, and combustion chamber and turbomachine both equipped with such a device

Turbomachine combustion chamber arrangement having a collar deflector

Device for injecting a mixture of air and fuel, and combustion chamber and turbomachine provided with such a device

Transverse wall of a combustion chamber provided with multi-perforation holes

Fuel injector for a gas turbine engine combustion chamber

Annular combustion chamber

PIEUSSERGUES CHRISTOPHE

Sealing between a combustion chamber and a turbine nozzle in a turbomachine

Turbomachine combustion chamber

System for injecting a mixture of air and fuel into a turbomachine combustion chamber

Device for mounting an igniter plug in a combustion chamber of a gas turbine engine

Optimizing the angular positioning of a turbine nozzle at the outlet from a turbomachine combustion chamber

Separator for feeding cooling air to a turbine

Procedure for igniting a turbine engine combustion chamber

SANDELIS DENIS JEAN MAURICE

Device for injecting a mixture of air and fuel into a turbomachine combustion chamber

Arrangement of a semiconductor-type igniter plug in a gas turbine engine combustion chamber

Annular combustion chamber for a turbine engine

Turbine nozzle guide vane assembly in a turbomachine

Combustion chamber for a turbomachine including improved air inlets

CAYRE ALAIN

Combustion chamber of a turbomachine including cooling grooves

Optimizing an anti-coke film in an injector system for a gas turbine engine

Turbomachine combustion chamber

LAINS DOMINIQUE MAURICE JACQUES

Afterburner chamber for a turbomachine

Fuel injection systems in a turbomachine combustion chamber

BUNEL JACQUES MARCEL ARTHUR

Guiding a sparkplug in a turbine engine combustion chamber

SOCOIETE NATIONALE D ETUDE ET

Dual head combustion chamber

CAMERIANO LAURENT BERNARD

Fuel injection system for a combustion chamber of a turbomachine

SAFRAN AIRCRAFT ENGINES

Measuring comb for measuring parameters of the gases exiting a turbomachine working section