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Inventor profile of:

Predrag TODOROVIC

City:

Berlin

Country:

Germany

Published Applications:

62

Last publication date:

2024-11-28

Top Assignees for applications by Predrag TODOROVIC

The entities that hold a legal rights for patent applications filed by inventor TODOROVIC Predrag:

Recent patent applications by TODOROVIC Predrag

Predrag TODOROVIC from Berlin, DE has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2024-11-28
US20240392803A1
Mechanical engineering

ENGINE HAVING CENTRIFUGAL COMPRESSOR, ANNULAR COMBUSTION CHAMBER AND A GUIDE CHANNEL ARRANGEMENT HAVING DIFFERENT GUIDE CHANNEL ELEMENTS

 #2 | 2021-06-24
US20210190004A1
Mechanical engineering

Exhaust nozzle of a gas turbine engine

 #3 | 2021-06-24
US20210190003A1
Mechanical engineering

Exhaust nozzle of a gas turbine engine

 #4 | 2021-06-24
US20210190002A1
Mechanical engineering

Exhaust nozzle of a gas turbine engine

 #5 | 2021-06-24
US20210190001A1
Mechanical engineering

Exhaust nozzle of a gas turbine engine

 #6 | 2021-06-24
US20210189999A1
Mechanical engineering

Exhaust nozzle of a gas turbine engine

 #7 | 2021-06-24
US20210189998A1
Mechanical engineering

Exhaust nozzle of a gas turbine engine

 #8 | 2021-06-24
US20210189958A1
Mechanical engineering

Asymmetric submerged air intake

 #9 | 2021-06-17
US20210180514A1
Mechanical engineering

JET ENGINE AIR INLET ARRANGEMENT AND METHOD FOR MANUFACTURE THEREOF

 #10 | 2021-03-18
US20210079870A1
Mechanical engineering

Propelling nozzle for a turbofan engine on a supersonic aircraft

 #11 | 2020-11-12
US20200355303A1
Mechanical engineering

ARTICULATING ARRANGEMENT FOR PIPE

 #12 | 2020-10-29
US20200340407A1
Mechanical engineering

PRESSURE RELIEF DEVICE HAVING A PRESSURE RELIEF FLAP

 #13 | 2020-10-22
US20200332741A1
Mechanical engineering

THRUST NOZZLE FOR A TURBOFAN ENGINE ON A SUPERSONIC AIRCRAFT

 #14 | 2019-12-12
US20190376470A1
Mechanical engineering

JET ENGINE WITH A RADIALLY VARIABLE WALL

 #15 | 2019-01-17
US20190016064A1
Performing operations; transporting

STRUCTURAL ELEMENT OF AN AIRCRAFT PART AND METHOD FOR MANUFACTURING A STRUCTURAL ELEMENT

 #16 | 2018-10-04
US20180283276A1
Mechanical engineering

Nacelle for a turbofan engine

 #17 | 2018-08-30
US20180245540A1
Mechanical engineering

CONVERGENT-DIVERGENT NOZZLE FOR A TURBOFAN ENGINE OF A SUPERSONIC AIRCRAFT AND METHOD FOR REDUCING THE BASE DRAG BEHIND SUCH NOZZLE

 #18 | 2018-08-30
US20180245539A1
Mechanical engineering

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

 #19 | 2018-05-17
US20180135556A1
Mechanical engineering

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

 #20 | 2018-03-08
US20180066605A1
Mechanical engineering

Mixer assembly group for a turbofan engine

 #21 | 2018-02-15
US20180045069A1
Mechanical engineering

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

 #22 | 2017-07-27
US20170211422A1
Mechanical engineering

TURBOMACHINE WITH AN INSERT DEVICE THAT CAN BE ARRANGED INSIDE A RECESS OF A WALL

 #23 | 2017-01-05
US20170002685A1
Mechanical engineering

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

 #24 | 2016-10-20
US20160305371A1
Mechanical engineering

Engine cowling of an aircraft gas turbine

 #25 | 2016-10-06
US20160288916A1
Performing operations; transporting

Engine cowling of an aircraft gas turbine

 #26 | 2016-08-25
US20160245230A1
Mechanical engineering

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

 #27 | 2016-08-25
US20160245180A1
Mechanical engineering

Gas-turbine engine with oil cooler in the engine cowling

 #28 | 2016-06-09
US20160160757A1
Mechanical engineering

Air intake arrangement

 #29 | 2016-05-19
US20160138411A1
Mechanical engineering

Fully integrated air guide element

 #30 | 2016-05-12
US20160131079A1
Mechanical engineering

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

 #31 | 2016-04-28
US20160115903A1
Mechanical engineering

Aircraft gas turbine thrust-reversing device having a guide rail

 #32 | 2015-10-15
US20150292357A1
Mechanical engineering

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

 #33 | 2015-10-08
US20150285144A1
Mechanical engineering

Gas turbine inlet

 #34 | 2015-06-25
US20150176529A1
Mechanical engineering

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

 #35 | 2015-06-25
US20150176527A1
Mechanical engineering

AIRCRAFT GAS TURBINE COMPRISING AN ENGINE COWLING WITH A THRUST-REVERSER DEVICE

 #36 | 2015-06-18
US20150167498A1
Mechanical engineering

Joint between components

 #37 | 2015-02-26
US20150052908A1
Mechanical engineering

Bleed duct assembly for a gas turbine engine

 #38 | 2014-05-22
US20140140820A1
Mechanical engineering

Aeroengine sealing arrangement

 #39 | 2014-05-08
US20140127001A1
Mechanical engineering

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

 #40 | 2014-05-01
US20140116026A1
Mechanical engineering

Aeroengine thrust reverser arrangement

 #41 | 2014-05-01
US20140116025A1
Mechanical engineering

Aeroengine thrust reverser arrangement

 #42 | 2014-03-06
US20140064928A1
Mechanical engineering

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

 #43 | 2013-12-05
US20130318945A1
Mechanical engineering

Aviation gas turbine thrust reversing device

 #44 | 2013-11-21
US20130306403A1
Mechanical engineering

Gas turbine exhaust cone

 #45 | 2013-11-21
US20130306402A1
Mechanical engineering

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

 #46 | 2013-11-21
US20130306401A1
Mechanical engineering

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

 #47 | 2013-09-05
US20130230383A1
Mechanical engineering

Aircraft gas turbine with adjustable fan

 #48 | 2013-08-15
US20130205753A1
Mechanical engineering

Aircraft gas turbine thrust-reversing device

 #49 | 2013-07-18
US20130180227A1
Mechanical engineering

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

 #50 | 2013-01-31
US20130025962A1
Mechanical engineering

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

 #51 | 2013-01-10
US20130011246A1
Mechanical engineering

Gas-Turbine Aircraft Engine With Structural Surface Cooler

 #52 | 2013-01-10
US20130008147A1
Mechanical engineering

Aircraft gas turbine with variable bypass nozzle by deforming element

 #53 | 2012-11-29
US20120298802A1
Performing operations; transporting

De-icing device of an aircraft gas-turbine engine

 #54 | 2012-11-15
US20120285138A1
Mechanical engineering

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

 #55 | 2012-01-12
US20120006614A1
Mechanical engineering

Gas-turbine exhaust cone

 #56 | 2011-09-08
US20110215172A1
Performing operations; transporting

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

 #57 | 2011-06-16
US20110139925A1
Performing operations; transporting

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

 #58 | 2011-05-26
US20110121136A1
Performing operations; transporting

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

 #59 | 2011-01-13
US20110005858A1
Performing operations; transporting

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

 #60 | 2010-09-09
US20100224348A1
Mechanical engineering

Method for the manufacture of an ejector nozzle tube

 #61 | 2010-09-09
US20100223905A1
Mechanical engineering

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

 #62 | 2009-04-23
US20090103975A1
Mechanical engineering

Attaching element
InventorID:

19804 ⎘