The Boeing Company

Kenneth Patrick Kirchoff

Dennis Michael Lewis

Michael R Sirkis

Nathaniel Thomas Horton

Ryan Lee Carlson

Dennis Whetten

Joel J Peterson

Bruce J Donham

Jim Sears

Patrick M Njeim

Thomas K Morrow

Bradley James Mitchell

Sudhakar S Shetty

David T Kirkland

Ethan Carl Owyang

Scott Edward Marston

Frank L Whetten

David T Ii Kirkland

A method for accessing aircraft interference path loss in an aircraft. A plurality of radio frequency signals that are stepped through a plurality of frequencies in a frequency range is transmitted from a plurality of locations within an interior of the aircraft. Radio frequency signals present at a receive antenna are received in response to transmitting the plurality of radio frequency signals to form a plurality of measurements. An average of averages curve is generated from the plurality of measurements. A peak to average ratio is identified. Field uniformity is identified. A standard error for the average of averages curve is determined. An upper bound for the aircraft interference path loss in the aircraft is predicted using the average of averages curve, the peak to average ration, the field uniformity, and the standard error.

Assessing aircraft interference path loss employing discrete frequency stirring

In one embodiment a method to evaluate a shielding effectiveness of an enclosed structure, comprising collecting synthetic aperture data from an electromagnetic transmission originating from within the enclosed structure to generate a synthetic aperture dataset, performing angular spectrum processing on the synthetic aperture dataset to generate an angle of arrival dataset and determining a shielding effectiveness parameter from the angle of arrival dataset. Other embodiments may be described.

Shielding effectiveness determination

A method for determining a direct antenna coupling in a reverberant environment is disclosed. Radiowave energy is emitted in the reverberant environment from a transmitting antenna to a receiving antenna at a plurality of frequencies, and discrete frequency stirring data is collected at a plurality of frequencies. The discrete frequency stirring data is amplitude corrected and phase corrected using an expected amplitude shift and an expected phase shift at each of the frequencies to provide corrected discrete frequency stirring data. The direct antenna coupling is determined based on the corrected discrete frequency stirring data.

Method for determining an antenna pattern in a reverberant environment

An assembly for shielding an aircraft from electromagnetic energy may include a window mounting configured to be conductively coupled to an aperture in a fuselage of an aircraft. The window mounting may include a window pane having an electromagnetically-reflective coating for reflecting electromagnetic energy. The window pane may remain electrically isolated from the fuselage prior to the electromagnetic energy exceeding a frequency of approximately 1 GHz. The window mounting may further include a capacitive gasket capacitively coupling the window pane to the fuselage after the frequency of the electromagnetic energy reflected by the window pane exceeds approximately 1 GHz.

Radio frequency shielding system

A system for shielding an aircraft from electromagnetic energy includes a fuselage, aperture, window mounting, and window plug. The fuselage provides an electrically conductive envelope. The aperture is disposed in the fuselage. The window mounting spans the aperture. The window plug spans the aperture. The window mounting and the window plug are electrically coupled to the fuselage and provide an electrical path spanning the aperture.

Radio frequency shielding apparatus system and method

An integrated wireless network and associated method are provided for facilitating wireless communication onboard an aircraft. The integrated wireless network includes a wireless distribution system including a wired interface and a plurality of wireless radios. The wireless distribution system may also include a combiner and one or more antennas, such as leaky feeder antenna(s), extending through the cabin compartment of the aircraft. The combiner may provide the combined wireless signals to the antenna for transmission. And, the combiner may deconstruct wireless signals received by the antenna and provide the deconstructed wireless signals to a respective wireless radio. The integrated wireless network of this embodiment also includes one or more wireless data concentrators having a plurality of wireless radios in communication with the antenna. The plurality of wireless radios of the wireless distribution system and the wireless data concentrator may support wireless communications in accordance with a plurality of different protocols.

Integrated wireless network and associated method

Growing community of inventors

Redmond, WA, United States of America

Kenneth Patrick Kirchoff