The Boeing Company

Adrian Viisoreanu

Douglas Alan McCarville

Manny S Urcia

Joseph A Marshall

Otis Franklin Layton

Justin David Kearns

William John Koch, Iv

Justin C Christenson

Herbert Louis Hoffman

Shailesh Atreya

Alan Edgar Landmann

Hugh Poling

Gerald D Miller

Juhn-Shyue Lin

William John Bigbee-Hansen

Wesley K Moore

Gary R Chewning

Shin S Lee

Russell W Morris

Albert D Olsen

Ronald W Davidson

Jason Alexander Gordon

Balamurugan R Annamalai

Jason A Gordon

An antenna electronics attachment system is disclosed. The antenna electronics attachment system includes a structural honeycomb panel having an array of cells. The antenna electronics attachment system further includes a nutplate coupled to a mounting plate via a plurality of embedded fastening structures. The mounting plate is shaped to fit substantially precisely to a cell of the structural honeycomb panel. The antenna electronics attachment system also includes an electronic component coupled to the nutplate. And, the antenna electronics attachment system further includes mechanical-electronic coupling means operable for change-out while in-service of the electronic component.

Structurally integrated antenna aperture electronics attachment design

Vibration-damping blankets are attached to the back surfaces of fairing panels of a flight vehicle (e.g., an aircraft or spacecraft) to reduce vibration, fatigue, structure and airborne transmitted energy, and cabin noise. In one case, the flight vehicle fairing has an exterior comprising exterior surfaces of a multiplicity of removable panels. A method of retrofitting the flight vehicle with vibration-damping blankets comprises: removing a panel from the flight vehicle exterior; attaching a vibration-damping blanket to a back surface of the removed panel; and installing the panel with attached vibration-damping blanket on the flight vehicle with the exterior surface of the panel forming part of the flight vehicle exterior. In one embodiment, the vibration-damping blanket comprises polymeric (e.g., aromatic polyamide) fibers in a nonwoven structure.

Flight vehicle fairing having vibration-damping blankets

A method of manufacture of antenna electronics attachment is disclosed. A nutplate is coupled to a mounting plate via a plurality of embedded fastening structures such that mechanical-electronic coupling means allow in-service change-out of an electronic component coupled to the nutplate.

Structurally integrated antenna aperture electronics attachment design and methodology

A composite panel structure for an aircraft includes a plurality of annular, hat-shaped frames disposed coaxially along a long axis of the aircraft in a spaced, parallel relationship, an inner skin having an inner surface bonded to an outer surface of the hat frames, a plurality of elongated, hat-shaped stringers disposed in a longitudinal direction along an outer surface of the inner skin in a spaced, parallel relationship, a solid or rigid foam offset bonded to an outer surface of each of the stringers, and an outer skin having an inner surface bonded to an upper surface of each of the offsets. The inner skin carries the loads of the structure and the outer skin defines an aerodynamic surface of the aircraft and provides impact and lighting protection. The frames, inner skin and stringers are formed on a single forming tool and cured and bonded with each other simultaneously.

Composite aircraft structures with hat stiffeners

Hydrogen powered air vehicles that in some embodiments can fly with very long endurance (10 or more days) at altitudes over 60,000 ft carrying payloads of up to 2,000 pounds. Embodiments may include features such as large wingspan relative to fuselage and an all composite or partial composite structure for light weight and strength. The aircraft of the invention use one or more internal combustion engines adapted for hydrogen combustion, each engine driving propellers. The hydrogen fuel is stored on board in containers, located within the fuselage, as a cryogenic liquid, and is vaporized in a heat exchanger before delivery to the internal combustion engine.

Long endurance hydrogen powered vehicle

Growing community of inventors

Kent, WA, United States of America

Adrian Viisoreanu