Jason Scott Warner

US Patent:

20220242591, Aug 4, 2022

Filed:

Apr 19, 2022

Appl. No.:

17/724278

Inventors:

- Chicago IL, US
Don Russell - Arlington WA, US
Matthew B. Moore - Edmonds WA, US
Jason Warner - Granite Falls WA, US
David Jon Herman - Monroe WA, US
Patrick B. Stone - Monroe WA, US

International Classification:

B64F 5/10
B64F 5/50

Abstract:

Methods and systems for assembling containerized aircraft as complete aircraft. The methods comprise removing aircraft components from shipping container(s), unloading the aircraft components from shipping fixture(s), removing tooling comprising aircraft component positioning structure(s) from the shipping container(s), loading aircraft component(s) onto aircraft component positioning structure(s), positioning the aircraft components in aircraft component installation positions, positioning the aircraft component(s) using the aircraft component positioning structure(s), and attaching the aircraft components to assemble the complete aircraft. The systems comprise aircraft components configured to be loaded into shipping container(s) in a shipping arrangement, unloaded from the shipping arrangement and attached to at least one other aircraft component to assemble the complete aircraft; shipping fixture(s) configured to support the aircraft components in the shipping arrangement, and tooling configured to facilitate assembly of the aircraft components and comprising aircraft component positioning structure(s) configured to position aircraft component(s) in aircraft component installation position(s).

US Patent:

20210206514, Jul 8, 2021

Filed:

Jan 6, 2020

Appl. No.:

16/735315

Inventors:

- Chicago IL, US
Don Russell - Arlington WA, US
Matthew B. Moore - Edmonds WA, US
Jason Warner - Granite Falls WA, US
David Jon Herman - Monroe WA, US
Patrick B. Stone - Monroe WA, US

International Classification:

B64F 5/10
B64F 5/50

Abstract:

Methods and systems for assembling containerized aircraft as complete aircraft. The methods comprise removing aircraft components from shipping container(s), unloading the aircraft components from shipping fixture(s), removing tooling comprising aircraft component positioning structure(s) from the shipping container(s), loading aircraft component(s) onto aircraft component positioning structure(s), positioning the aircraft components in aircraft component installation positions, positioning the aircraft component(s) using the aircraft component positioning structure(s), and attaching the aircraft components to assemble the complete aircraft. The systems comprise aircraft components configured to be loaded into shipping container(s) in a shipping arrangement, unloaded from the shipping arrangement and attached to at least one other aircraft component to assemble the complete aircraft; shipping fixture(s) configured to support the aircraft components in the shipping arrangement, and tooling configured to facilitate assembly of the aircraft components and comprising aircraft component positioning structure(s) configured to position aircraft component(s) in aircraft component installation position(s).

US Patent:

20190247884, Aug 15, 2019

Filed:

Apr 22, 2019

Appl. No.:

16/390928

Inventors:

- Chicago IL, US
Bennett M. Moriarty - Bothell WA, US
Luis A. Perla - Sammamish WA, US
Jeffrey S. Rebmann - Kirkland WA, US
Trevor S. McCrea - Everett WA, US
Jason S. Warner - Granite Falls WA, US
Seana B. Kobak - Sammamish WA, US
Ryan M. Trumbo - Renton WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

B05D 7/22
B05B 13/04
B05B 13/02
B64F 5/10
B41J 2/01

Abstract:

Surface treatment of a tubular surface defining an axis extending from a first surface end to a second surface end includes partially surrounding the tubular surface, at a first position, with a first set of treating units, with the treating units arranged in a first arcuate array. Furthermore, each treating unit is configured to include a plurality of first applicator heads. In some examples, a position of each of the plurality of first applicator heads is determined relative to the tubular surface. The first set of treating units is moved from the first position towards a second position. In one non-limiting example, each of the plurality of first applicator heads is independently controlled to selectively apply a first treatment as the first set of treating units moves from the first position towards the second position.

US Patent:

20180126416, May 10, 2018

Filed:

Nov 9, 2016

Appl. No.:

15/347375

Inventors:

- Chicago IL, US
Bennett M. Moriarty - Bothell WA, US
Luis A. Perla - Sammamish WA, US
Jeffrey S. Rebmann - Kirkland WA, US
Trevor S. McCrea - Everett WA, US
Jason S. Warner - Granite Falls WA, US
Seana B. Kobak - Sammamish WA, US
Ryan M. Trumbo - Renton WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

B05D 7/22
B41J 2/01
B64F 5/00

Abstract:

A method of treating a tubular surface which defines an axis extending from a first surface end to a second surface end includes partially surrounding the tubular surface, at a first position, with a first set of treating units, with the treating units arranged in a first arcuate array. Furthermore, each treating unit is configured to include a plurality of first applicator heads. Additionally, an embodiment of the method includes determining a position of each of the plurality of first applicator heads relative to the tubular surface and moving the first set of treating units from the first position towards a second position. In one non-limiting example, the method further includes independently controlling each of the plurality of first applicator heads to selectively apply a first treatment as the first set of treating units moves from the first position towards the second position.