Inventor profile of:

Dmitriy B. Sidelkovskiy

City:

Ellington, Connecticut

Country:

United States

Published Applications:

19

Last publication date:

2024-02-01

Top Assignees for applications by Dmitriy B. Sidelkovskiy

The entities that hold a legal rights for patent applications filed by inventor Sidelkovskiy Dmitriy B.:

Recent patent applications by Sidelkovskiy Dmitriy B.

Dmitriy B. Sidelkovskiy from Ellington, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2024-02-01
US20240035392A1
Mechanical engineering

After-fan system with electrical motor for gas turbine engines

#2 | 2022-03-03
US20220063823A1
Performing operations; transporting

Nacelle

#3 | 2021-08-26
US20210262415A1
Mechanical engineering

High bypass ratio engine bypass duct nozzle with controlled nozzle area

#4 | 2021-08-26
US20210262359A1
Mechanical engineering

After-fan system with electrical motor for gas turbine engines

#5 | 2020-12-31
US20200408169A1
Mechanical engineering

Nacelle

#6 | 2020-10-15
US20200325852A1
Mechanical engineering

After-fan system for a gas turbine engine

#7 | 2020-08-11
US16110473
Mechanical engineering

Turbofan with motorized rotating inlet guide vane

#8 | 2020-08-06
US20200248628A1
Mechanical engineering

Gas turbine engine bypass drainage systems

#9 | 2020-03-05
US20200070962A1
Performing operations; transporting

Method for separated flow detection

#10 | 2020-02-27
US20200063657A1
Mechanical engineering

Turbofan with motorized rotating inlet guide vane

#11 | 2019-01-31
US20190031357A1
Performing operations; transporting

Nacelle

#12 | 2019-01-31
US20190031356A1
Performing operations; transporting

Nacelle

#13 | 2019-01-17
US20190017470A1
Mechanical engineering

Convergent divergent exit nozzle for a gas turbine engine

#14 | 2018-09-13
US20180258854A1
Mechanical engineering

Fan flutter suppression system

#15 | 2017-06-08
US20170159571A1
Mechanical engineering

Multi-shaft gas turbine engine

#16 | 2016-08-18
US20160237856A1
Mechanical engineering

Track fairing assembly for a turbine engine nacelle

#17 | 2016-07-07
US20160195038A1
Mechanical engineering

Convergent divergent exit nozzle for a gas turbine engine

#18 | 2014-09-11
US20140250860A1
Mechanical engineering

Multi-shaft gas turbine engine

#19 | 2013-12-05
US20130319002A1
Mechanical engineering

Nacelle bifurcation for gas turbine engine

InventorID:

551977 ⎘