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Inventor profile of:

Rudolf Stanka

City:

Rattenkirchen

Country:

Germany

Published Applications:

31

Last publication date:

2024-03-28

Top Assignees for applications by Rudolf Stanka

The entities that hold a legal rights for patent applications filed by inventor Stanka Rudolf:

Recent patent applications by Stanka Rudolf

Rudolf Stanka from Rattenkirchen, DE has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2024-03-28
US20240102398A1
Mechanical engineering

MODULE FOR A TURBOMACHINE

 #2 | 2023-08-17
US20230258097A1
Mechanical engineering

ROTOR BLADE FOR A GAS TURBINE

 #3 | 2019-11-28
US20190360347A1
Mechanical engineering

Turbine center frame having a specifically designed annular space contour

 #4 | 2019-02-07
US20190040750A1
Mechanical engineering

Blade or vane for turbomachine with different diffusion protective coatings and method for manufacture thereof

 #5 | 2018-12-06
US20180347388A1
Mechanical engineering

Gas turbine with axially moveable outer sealing ring with respect to housing against a direction of flow in an assembled state

 #6 | 2018-12-06
US20180347384A1
Mechanical engineering

SEALING SYSTEM WITH WELDED-ON SEALING PLATE, TURBOMACHINE, AND MANUFACTURING METHOD

 #7 | 2018-11-29
US20180340435A1
Mechanical engineering

Seal arrangement for a turbomachine, method for manufacturing a seal arrangement and turbomachine

 #8 | 2018-11-08
US20180320535A1
Mechanical engineering

Wear-resistant shield for a rotating blade of a gas turbine

 #9 | 2018-09-27
US20180274367A1
Mechanical engineering

Turbomachine component arrangement

 #10 | 2017-08-24
US20170241279A1
Mechanical engineering

Guide vane segment for a turbomachine

 #11 | 2017-06-08
US20170159609A1
Mechanical engineering

TURBOFAN AIRCRAFT ENGINE WITH REDUCED NOISE EMISSION

 #12 | 2017-06-08
US20170159573A1
Mechanical engineering

REDUCED NOISE TURBOFAN AIRCRAFT ENGINE

 #13 | 2017-06-08
US20170159482A1
Mechanical engineering

Run-in coating for an outer air seal of a turbomachine

 #14 | 2017-06-08
US20170159466A1
Mechanical engineering

Guide vane segment with radical securing elements

 #15 | 2017-06-08
US20170159461A1
Mechanical engineering

Stacking of rotor blades on centroids

 #16 | 2017-04-20
US20170107843A1
Mechanical engineering

Module for a gas turbine

 #17 | 2016-02-04
US20160032826A1
Mechanical engineering

TURBOFAN AIRCRAFT ENGINE

 #18 | 2016-01-21
US20160017797A1
Mechanical engineering

Turbofan aircraft engine

 #19 | 2015-07-09
US20150192028A1
Mechanical engineering

Gas turbine

 #20 | 2015-07-09
US20150192026A1
Mechanical engineering

Gas turbine

 #21 | 2015-04-09
US20150098799A1
Mechanical engineering

Component support and turbomachine

 #22 | 2015-03-12
US20150071769A1
Mechanical engineering

Method for disassembly and assembly of a rotor of a gas turbine

 #23 | 2015-01-29
US20150030434A1
Mechanical engineering

Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine

 #24 | 2015-01-15
US20150016985A1
Mechanical engineering

Gas turbine stage

 #25 | 2015-01-15
US20150016969A1
Mechanical engineering

Turbomachine, sealing segment, and guide vane segment

 #26 | 2014-10-09
US20140301853A1
Mechanical engineering

Securing blade assortment

 #27 | 2014-10-09
US20140301840A1
Mechanical engineering

Guide vane arrangement

 #28 | 2013-09-26
US20130251532A1
Mechanical engineering

Securing device for axially securing a blade root of a turbomachine blade

 #29 | 2013-07-25
US20130189111A1
Mechanical engineering

Rotor for a turbomachine

 #30 | 2008-11-27
US20080292457A1
Mechanical engineering

Device for suspending guide blades

 #31 | 2008-07-10
US20080166221A1
Mechanical engineering

Apparatus and method for active gap monitoring for a continuous flow machine
InventorID:

353338 ⎘