Eric A Dickey, 6213968 Pine St, Trona, CA 93562

2021032, Oct 21, 2021

Apr 15, 2020

16/849096

- Chicago IL, US
Eric D. Dickey - Long Beach CA, US

B64C 9/00
B64C 3/18
B64C 3/26
B64C 13/30
B64C 13/02

Aircraft wing droop leading edge apparatus and methods are described. An example aircraft includes a wing having a front spar and an outer skin covering the front spar. The outer skin includes a forward portion located forward of the front spar. The forward portion of the outer skin includes a leading edge movable between a neutral position and a drooped position deflected downward relative to the neutral position. The forward portion of the outer skin has a continuous outer mold line when the leading edge is in the drooped position.

2021000, Jan 14, 2021

Jul 10, 2019

16/507999

- Chicago IL, US
Eric David Dickey - Long Beach CA, US

B64C 23/06
B64C 13/12
B64C 13/04
B64C 19/02

High-lift systems and related methods are described. An example apparatus includes a fixed wing and a Krueger flap movably coupled to the fixed wing between a stowed position and a deployed position. The Krueger flap includes a first flap portion movably coupled to the fixed wing and a second flap portion movable coupled to the first flap portion. The first flap portion moves relative to the second flap portion between a retracted position and an extended position. The first flap is to move to the retracted position in response to the Krueger flap moving to the stowed position. The first flap is to move to the extended position to define an aerodynamic surface in response to the Krueger flap moving to the deployed position.

2019029, Sep 26, 2019

Mar 22, 2018

15/928429

- Chicago IL, US
Lie-Mine Gea - Irvine CA, US
Anthony J. Sclafani - Alta Loma CA, US
Eric D. Dickey - Long Beach CA, US
Michael D. Beyar - Long Beach CA, US
Christopher K. Droney - Long Beach CA, US

B64C 3/50
B64C 9/34
B64C 1/26
B64C 23/04

Described herein is an aircraft. The aircraft comprises a body. The aircraft also comprises a wing coupled to and extending from the body. The wing comprises a wing inboard end portion, a wing outboard end portion, opposite the wing inboard end portion, and an intermediate portion between the wing inboard end portion and the wing outboard end portion. The aircraft further comprises a strut. The strut comprises a strut inboard end portion coupled to and extending from the body and a strut outboard end portion coupled to and extending from the intermediate portion of the wing. The aircraft additionally comprises at least one aerodynamic control surface movably coupled to the strut.

2019000, Jan 3, 2019

Aug 21, 2018

16/107562

- Chicago IL, US
Daniel Michael Tompkins - Cypress CA, US
Robert Hauschild Liebeck - Irvine CA, US
Kevin Robert Elmer - Foothills Ranch CA, US
Eric David Dickey - Long Beach CA, US

The Boeing Company - Chicago IL

B64C 9/24
B64C 3/28

A leading edge high-lift device, that may be deployable from a wing of an aircraft, may include a leading edge and a trailing edge. A lower surface and an upper surface may both extend between the leading edge and the trailing edge. A trailing edge region may be defined by the trailing edge and an adjacent region thereto. A shaping device may be disposed at the trailing edge region and may be movable between a non-activated position and an activated position.

2017015, Jun 1, 2017

Dec 1, 2015

14/956006

- Chicago IL, US
Daniel Michael Tompkins - Cypress CA, US
Robert Hauschild Liebeck - Irvine CA, US
Kevin Robert Elmer - Foothills Ranch CA, US
Eric David Dickey - Long Beach CA, US

The Boeing Company - Chicago IL

B64C 9/24
B64C 3/28

A leading edge high-lift device, that may be deployable from a wing of an aircraft, may include a leading edge and a trailing edge. A lower surface and an upper surface may both extend between the leading edge and the trailing edge. A trailing edge region may be defined by the trailing edge and an adjacent region thereto. A shaping device may be disposed at the trailing edge region and may be movable between a non-activated position and an activated position.