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Inventor profile of:

Inga Mahle

City:

Munich

Country:

Germany

Published Applications:

16

Last publication date:

2019-01-17

Top Assignees for applications by Inga Mahle

The entities that hold a legal rights for patent applications filed by inventor Mahle Inga:

Recent patent applications by Mahle Inga

Inga Mahle from Munich, DE has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2019-01-17
US20190017384A1
Mechanical engineering

Turbomachine airfoil array

 #2 | 2018-11-15
US20180328185A1
Mechanical engineering

Contouring of an airfoil array platform

 #3 | 2018-11-15
US20180328184A1
Mechanical engineering

Endwall contouring for a turbomachine

 #4 | 2018-10-18
US20180298761A1
Mechanical engineering

Contouring a blade/vane cascade stage

 #5 | 2018-09-06
US20180252107A1
Mechanical engineering

Contouring a blade/vane cascade stage

 #6 | 2018-08-09
US20180223670A1
Mechanical engineering

Contouring a blade/vane cascade stage

 #7 | 2017-06-08
US20170159465A1
Mechanical engineering

Guide vane segment for a turbomachine

 #8 | 2017-06-08
US20170159444A1
Mechanical engineering

Blade channel, blade cascade and turbomachine

 #9 | 2017-06-08
US20170159443A1
Mechanical engineering

CONTOURED SURFACE ANNULAR SECTION OF A GAS TURBINE

 #10 | 2015-10-08
US20150285080A1
Mechanical engineering

Gas turbine blade

 #11 | 2015-01-15
US20150016985A1
Mechanical engineering

Gas turbine stage

 #12 | 2014-02-13
US20140044551A1
Mechanical engineering

Blade cascade with side wall contours and continuous-flow machine

 #13 | 2013-10-10
US20130266426A1
Mechanical engineering

Sealing system for a turbomachine

 #14 | 2013-06-20
US20130156563A1
Mechanical engineering

Turbomachine and turbomachine stage

 #15 | 2013-03-14
US20130064657A1
Mechanical engineering

Intermediate housing of a gas turbine having an outer bounding wall having a contour that changes in the circumferential direction upstream of a supporting rib to reduce secondary flow losses

 #16 | 2012-08-09
US20120201688A1
Mechanical engineering

Blade channel having an end wall contour and a turbomachine
InventorID:

476415 ⎘