Inventor profile of:

James D. Chase

City:

Reno, Nevada

Country:

United States

Published Applications:

15

Last publication date:

2022-03-10

Top Assignees for applications by James D. Chase

The entities that hold a legal rights for patent applications filed by inventor Chase James D.:

Recent patent applications by Chase James D.

James D. Chase from Reno, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2022-03-10
US20220073203A1
Performing operations; transporting

Supersonic aircraft jet engine installation

#2 | 2020-07-28
US15626012
Mechanical engineering

High flow plug nozzle apparatus and method of using the same

#3 | 2016-01-12
US13068773
Performing operations; transporting

Highly efficient supersonic laminar flow wing structure

#4 | 2015-03-31
US13068774
Performing operations; transporting

Highly efficient transonic laminar flow wing

#5 | 2012-02-23
US20120043430A1
Performing operations; transporting

Laminar flow wing optimized for transonic cruise aircraft

#6 | 2012-02-23
US20120043429A1
Performing operations; transporting

Laminar flow wing optimized for transonic cruise aircraft

#7 | 2011-04-28
US20110095137A1
Performing operations; transporting

Laminar flow wing optimized for supersonic cruise aircraft

#8 | 2011-03-24
US20110067393A1
Mechanical engineering

Aircraft emergency and backup secondary power apparatus

#9 | 2011-03-17
US20110062290A1
Performing operations; transporting

Supersonic aircraft jet engine installation

#10 | 2010-06-10
US20100139284A1
Mechanical engineering

Jet nozzle plug with varying, non-circular cross sections

#11 | 2009-08-20
US20090206206A1
Performing operations; transporting

Highly efficient supersonic laminar flow wing

#12 | 2009-01-15
US20090014597A1
Performing operations; transporting

Supersonic aircraft jet engine

#13 | 2006-02-21
US10693411
-

Laminar flow wing for transonic cruise

#14 | 2005-07-14
US20050151029A1
Performing operations; transporting

Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings

#15 | 2005-02-22
US10746744
-

Highly swept canard with low sweep wing supersonic aircraft configuration

InventorID:

3102887 ⎘