Inventor

TODOROVIC PREDRAG

DE50 patents

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

TODOROVIC PREDRAG

ROLLS ROYCE DEUTSCHLAND LTD & CO KG

Nacelle for a turbofan engine

Aircraft gas turbine having a core engine casing with cooling-air tubes

Gas-turbine engine with oil cooler in the engine cowling

Asymmetric submerged air intake

Convergent-divergent nozzle for a turbofan engine of a supersonic aircraft and method for adjusting the nozzle throat surface in a nozzle of a turbofan engine

Engine cowling of an aircraft gas turbine

Engine cowling of an aircraft gas turbine

Joint between components

Aeroengine thrust reverser arrangement

Mixer assembly group for a turbofan engine

Gas turbine inlet

Aircraft gas turbine thrust-reversing device having a guide rail

Aircraft gas turbine comprising a thrust-reverser device with cascade elements and an integrated rack and pinion drive

Air intake arrangement

Propelling nozzle for a turbofan engine on a supersonic aircraft

Exhaust nozzle of a gas turbine engine

Mixer for an engine manufactured from at least one composite material, manufacturing method and manufacturing device

Exhaust nozzle of a gas turbine engine

Exhaust nozzle of a gas turbine engine

Exhaust nozzle of a gas turbine engine

Exhaust nozzle of a gas turbine engine

Exhaust nozzle of a gas turbine engine

Fully integrated air guide element

Aeroengine thrust reverser arrangement

Aeroengine sealing arrangement

Bleed duct assembly for a gas turbine engine

Guide vane of a gas turbine engine, in particular of an aircraft engine

Device of a turbomachine for actuating a setting device and turbomachine with such a device

Engine cowling of a gas turbine with thrust-reversing device and adjustable outlet nozzle

Engine cowling of a gas turbine with thrust-reversing device and cross-sectionally adjustable outlet nozzle

TODOROVIC PREDRAG

Gas turbine exhaust cone

Gas-turbine engine with telescope-type air inlet of the engine cowling (nacelle)

Aircraft gas-turbine engine with oil cooler in the engine cowling

Air ejector nozzle tube for an oil heat exchanger of an aircraft engine

Gas-turbine exhaust cone with three-dimensionally profiled partition wall and plate-type wall element

Gas-turbine exhaust cone

Noise-reduced aircraft engine and method for reducing noise emissions of an aircraft engine

Scoop of a running-gap control system of an aircraft gas turbine

Aviation gas turbine thrust reversing device

Method for the production of a sound absorber, especially for a gas turbine exhaust cone

De-icing device of an aircraft gas-turbine engine

Sound absorber for a gas turbine exhaust cone, and method for the production thereof

Aircraft de-icing device and engine nacelle of an aircraft gas turbine with de-icing device

Aircraft gas turbine with variable bypass nozzle by deforming element

Method for the manufacture of an ejector nozzle tube

ROLLS ROYCE DEUTSCHLAND

Aircraft gas turbine with adjustable fan

Fastening element and de-icing device of an aircraft gas-turbine engine

Aircraft gas turbine thrust-reversing device

Engine casing of an aircraft gas turbine having sound-absorbing elements in the fan inflow region

LISIEWICZ STEPHAN

Arrangement for the suspension of a jet engine to a supporting structure