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Inventor profile of:

Eric W. Malmborg

City:

Amston, Connecticut

Country:

United States

Published Applications:

32

Last publication date:

2023-09-28

Top Assignees for applications by Eric W. Malmborg

The entities that hold a legal rights for patent applications filed by inventor Malmborg Eric W.:

Recent patent applications by Malmborg Eric W.

Eric W. Malmborg from Amston, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2023-09-28
US20230304407A1
Mechanical engineering

Airfoil with body and cover panel

 #2 | 2022-05-12
US20220145763A1
Mechanical engineering

Multi-cover gas turbine engine component

 #3 | 2022-04-28
US20220127966A1
Mechanical engineering

Hybridized airfoil for a gas turbine engine

 #4 | 2022-03-10
US20220074310A1
Mechanical engineering

Airfoil with body and cover panel

 #5 | 2021-02-04
US20210032997A1
Mechanical engineering

Hybridized airfoil for a gas turbine engine

 #6 | 2020-12-17
US20200392854A1
Mechanical engineering

Airfoil with cover for gas turbine engine

 #7 | 2020-11-12
US20200355080A1
Mechanical engineering

Multi-cover gas turbine engine component

 #8 | 2020-09-24
US20200298352A1
Performing operations; transporting

Method of forming gas turbine engine components

 #9 | 2020-09-17
US20200291815A1
Mechanical engineering

Damped airfoil for a gas turbine engine

 #10 | 2020-07-23
US20200232329A1
Mechanical engineering

Airfoil with body and cover panel

 #11 | 2020-07-09
US20200215642A1
Performing operations; transporting

Hollow airfoil with catenary profiles

 #12 | 2020-06-18
US20200190985A1
Mechanical engineering

Fan blade for a gas turbine engine

 #13 | 2019-09-19
US20190284675A1
Chemistry; metallurgy

Method of producing a gas turbine engine component

 #14 | 2019-07-18
US20190218915A1
Mechanical engineering

Apparatus and method for selective bonding to form hollow components

 #15 | 2019-04-18
US20190112931A1
Mechanical engineering

Hollow fan blade constrained layer damper

 #16 | 2019-02-07
US20190040744A1
Mechanical engineering

Power beam welded cavity-back titanium hollow fan blade

 #17 | 2019-01-17
US20190017386A1
Mechanical engineering

Gas turbine engine hollow fan blade rib orientation

 #18 | 2018-12-06
US20180347582A1
Mechanical engineering

Hollow fan blade with structural ribs

 #19 | 2018-11-29
US20180340548A1
Mechanical engineering

Following blade impact load support

 #20 | 2018-11-29
US20180340425A1
Mechanical engineering

Airfoil damping assembly for gas turbine engine

 #21 | 2013-06-06
US20130142643A1
Mechanical engineering

Structural joint for connecting a first component to a segmented second component

 #22 | 2013-04-04
US20130081406A1
Mechanical engineering

Gas turbine engine rotor stack assembly

 #23 | 2013-02-21
US20130045089A1
Mechanical engineering

Gas turbine engine seal assembly having flow-through tube

 #24 | 2013-02-07
US20130034449A1
Mechanical engineering

Gas turbine engine rotor construction

 #25 | 2012-11-08
US20120282101A1
Mechanical engineering

Gas turbine engine rotor construction

 #26 | 2012-07-05
US20120171029A1
Mechanical engineering

Turbine engine rotating cavity anti-vortex cascade

 #27 | 2012-02-02
US20120027606A1
Mechanical engineering

Rotor assembly disk spacer for a gas turbine engine

 #28 | 2011-12-08
US20110299992A1
Mechanical engineering

Rotor assembly for gas turbine engine

 #29 | 2010-10-21
US20100266401A1
Mechanical engineering

Turbine engine rotating cavity anti-vortex cascade

 #30 | 2010-10-21
US20100266387A1
Mechanical engineering

Turbine engine rotating cavity anti-vortex cascade

 #31 | 2010-09-23
US20100239424A1
Mechanical engineering

Split disk assembly for a gas turbine engine

 #32 | 2007-01-25
US20070020101A1
Mechanical engineering

Fan rotor design for coincidence avoidance
InventorID:

77763 ⎘