The Boeing Company

Shawn M Pare

Vasan S Sundaram

Andrew Francis Szerlag

Karen Lee Hills

Mostafa Rassaian

Kjersta Lynn Larson-Smith

Donald Paul Matheson

Joshua M Montgomery

Liam S C Pingree

David A Bowen

Steven Ellis Rhynard

Kjersta L Larson

Ryan A Street

Craig T Brockett

G Frank Sexton

Michael R Sirkis

Keith H Novak

Jung-Chuan Lee

Ashley G Badger

Julia W Miller

Chris H Balsillie

Jeffrey P Sandys

Robert W Mumm

Joe S Wong

Art Waidner

Liam SC Pingree

Terry N Christenson

A porthole, a porthole plug in a vehicle, and an aircraft with portholes are provided. The porthole includes an opaque plug with an aperture therethrough.

Plindow with opaque plug

A porthole, a porthole plug in a vehicle, and an aircraft with portholes are provided. The porthole includes an opaque plug with an aperture therethrough. A camera is arranged with a lens aligned with the aperture.

Plindow mounted camera system

A hard, transparent coating for a substrate and associated method for coating is disclosed. The coating includes alternating layers of a soft coating and a hard coating. The coating further includes a sensor. The electrical resistivity of the sensor may be measured to determine if the coating has been degraded. The coating may further include a hydrophobic outer layer.

Durable transparent intelligent coatings for polymeric transparencies

An exemplary embodiment provides coated polymeric substrates that have a polymeric substrate body with a coated surface. The surface coating includes more than one pair of coating layers. Each pair of coating layers includes a first applied coating layer and a second applied coating layer. In addition, an indicator, applied on top of or between coating layers, provides an indication of wear of the coating. The first and second applied coating layers have a thickness between about 3 to about 10 nanometers. The coating exhibits a Hall-Petch effect.

Barrier coatings for polymeric substrates

A method for applying an abrasion-resistant coating to a substrate including the steps of generating an atmospheric plasma, introducing a precursor to the atmospheric plasma, the precursor being selected to form the abrasion-resistant coating, and positioning the substrate relative to the atmospheric plasma such that the atmospheric plasma deposits the abrasion-resistant coating onto the substrate.

System and method for applying abrasion-resistant coatings

An exemplary embodiment provides coated polymeric substrates that have a polymeric substrate body with a coated surface. The surface coating includes more than one pair of coating layers. Each pair of coating layers includes a first applied coating layer and a second applied coating layer. In addition, an indicator, applied on top of or between coating layers, provides an indication of wear of the coating.

A window assembly and method for use with a mobile platform, and particularly with commercial or military aircraft. The window assembly includes a composite window panel that is secured to the fuselage skin of the aircraft. A tempered glass fairing is used in connection with a retainer clip and a plurality of sealing components to seal the fairing over the window panel in a manner that provides a sealed air gap between the inner surface of the fairing and the outer surface of the window panel. The fairing and the sealed air gap help to thermally isolate the window panel from the significant ambient temperature changes that are encountered during flight of the mobile platform. The fairing also provides a hazard barrier to protect the composite window panel from impact by foreign objects during flight. The sealed air gap also helps to control deflection of the fairing to thus ensure that the fairing maintains an aerodynamic profile generally in accordance with the contour of the outer surface of the fuselage.

Sealed structural passenger window assembly and method of forming same

A system and a method is provided for fitting an aircraft cabin with modular sidewall panels, window reveals, and foam insulation blocks in an integrated manner. The system comprises a sidewall panel which may have one or more openings therethrough to receive a window reveal held by snap-fit fastenings. The bezel of the window reveal may be held by snap-fit fasteners for easy removal to allow removal and cleaning of the inner dust cover disassembly of the sidewall panel. Foam insulation blocks may be molded to fit in the cavity between the outer wall of the aircraft and the sidewall panels, held in place by compressive pressure between the frames of the airframe. The outer extent of the window reveal is tapered inwardly to guide the window reveal to mating contact with an outer window assembly in the aircraft fuselage without further adjustment of the sidewall panel.

Integrated window belt system for aircraft cabins

Growing community of inventors

Woodinville, WA, United States of America

Shawn M Pare