Donald A Mottaz

46939261, Sep 15, 1987

Nov 25, 1986

6/936461

Joseph C. Kowalski - Snohomish WA
Donald A. Mottaz - Issaquah WA
Berton A. Cole - Bellevue WA

The Boeing Company - Seattle WA

B32B 318
B32B 702
B32B 1508
B32B 3100

428204

Composite, lightweight, flexible, fire-resistant, decorative laminates (10, 10', 10") suitable for use as wall coverings on bulkhead panels in commercial aircraft include: (i) a laminar fire-resistant layer (15/14) including an aluminum foil sheet (15) bonded to a first inert polyvinyl fluoride sheet (14); (ii) an underlying flexible paper-like base lamination (11); (iii) means (12) for adhesively bonding the first polyvinyl fluoride sheet (14) to the panel-like base lamination (11); (iv) a resinous embossing film (16) overlying and in face-to-face bonded relation to the aluminum foil sheet (15); (v) sheet defining means (18, 18', 18") having an outer decorative surface and in overlying face-to-face bonded engagement with a resinous embossing film (16); and (vi), an outer transparent sheet (21) of clear polyvinyl fluoride overlying in bonded face-to-face relation with the decorative surface (19, 22) of the sheet defining means (18, 18', 18").

20170144779, May 25, 2017

Feb 7, 2017

15/426765

- Chicago IL, US
Daniel R. Smith - Redmond WA, US
Jayson J. Aquino - Bothell WA, US
Edward John Batt - Bothell WA, US
James N. Buttrick - Seattle WA, US
Antonio C. Micale - Seattle WA, US
Darrell D. Jones - Mill Creek WA, US
Clayton L. Munk - Maple Valley WA, US
Chris G. Couevas - Bothell WA, US
Azita N. Namdaran - Bellevue WA, US
Noman S. Noor - Bellevue WA, US
Donald A. Mottaz - Issaquah WA, US

B64F 5/10
B64F 5/50
B23P 21/00
B21J 15/14
B23P 23/06

A system and method are provided to automate the assembly of a wing panel, such as utilized by commercial aircraft. In the context of a system, a tacking cell is provided that is configured to tack one or more stringers to a skin plank. The system also includes a riveting cell configured to receive a tacked plank from the tacking cell and to rivet the one or more stringers to the skin plank. The system also includes a splicing cell configured to receive a plurality of riveted planks from the riveting cell and to attach one or more splice stringers to the plurality of riveted planks. Further, the system includes a side of body cell configured to receive a spliced panel from the splicing cell and to attach a side of body chord thereto to produce a wing panel.

20140090252, Apr 3, 2014

Mar 15, 2013

13/837750

THE BOEING COMPANY - , US
Daniel R. Smith - Redmond WA, US
Jayson J. Aquino - Bothell WA, US
Edward John Batt - Bothell WA, US
James N. Buttrick - Seattle WA, US
Antonio C. Micale - Seattle WA, US
Darrell D. Jones - Mill Creek WA, US
Clayton L. Munk - Maple Valley WA, US
Chris G. Couevas - Bothell WA, US
Mario Ramos - Tacoma WA, US
Azita N. Namdaran - Bellevue WA, US
Noman S. Noor - Bellevue WA, US
Donald A. Mottaz - Issaquah WA, US

THE BOEING COMPANY - Chicago IL

B23P 23/00

298972, 29 33 R

A system and method are provided to automate the assembly of a wing panel, such as utilized by commercial aircraft. In the context of a system, a tacking cell is provided that is configured to tack one or more stringers to a skin plank. The system also includes a riveting cell configured to receive a tacked plank from the tacking cell and to rivet the one or more stringers to the skin plank. The system also includes a splicing cell configured to receive a plurality of riveted planks from the riveting cell and to attach one or more splice stringers to the plurality of riveted planks. Further, the system includes a side of body cell configured to receive a spliced panel from the splicing cell and to attach a side of body chord thereto to produce a wing panel.