Inventor profile of:

Stephen J. Fox

City:

Everett, Washington

Country:

United States

Published Applications:

13

Last publication date:

2016-10-13

Top Assignees for applications by Stephen J. Fox

The entities that hold a legal rights for patent applications filed by inventor Fox Stephen J.:

Recent patent applications by Fox Stephen J.

Stephen J. Fox from Everett, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2016-10-13
US20160297513A1
Performing operations; transporting

High-positioned 2-position variable camber Krueger

#2 | 2015-11-26
US20150336657A1
Performing operations; transporting

Rotary drive assembly for wing tip

#3 | 2014-10-23
US20140312175A1
Performing operations; transporting

High-positioned 2-position variable camber Krueger

#4 | 2013-12-26
US20130341467A1
Performing operations; transporting

Swing tip assembly rotation joint

#5 | 2013-08-15
US20130206917A1
Performing operations; transporting

High-positioned 3-position variable camber krueger

#6 | 2013-04-25
US20130099060A1
Performing operations; transporting

Hinged raked wing tip

#7 | 2013-03-28
US20130075537A1
Performing operations; transporting

Aircraft flap mechanism having compact large fowler motion providing multiple cruise positions

#8 | 2013-01-10
US20130009016A1
Performing operations; transporting

Retractable vortex generator for reducing stall speed

#9 | 2012-01-19
US20120012696A1
Performing operations; transporting

Aircraft flap actuator assembly

#10 | 2009-03-19
US20090072093A1
Performing operations; transporting

Link mechanisms for gapped rigid krueger flaps, and associated systems and methods

#11 | 2007-08-21
US10188988
-

Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface

#12 | 2007-05-10
US20070102587A1
Performing operations; transporting

Wing leading edge slat system

#13 | 2005-02-03
US20050022866A1
Mechanical engineering

Apparatus and methods for varying inlet lip geometry of a jet engine inlet

InventorID:

21795 ⎘