The Boeing Company

Drew L Smallwood

Jonathan David Embler

Thomas R Pinney

Michael J Best

John Scott Kruse

A fairing assembly for an aerial vehicle having a tank that forms a body of the vehicle and a wing coupled to the tank is provided. The fining assembly includes a substructure configured to couple with a tank skin of the tank, a thermal protection system coupled to the substructure, and a seal assembly coupled to the substructure, the seal assembly being configured to overlap at least a portion of an edge of the wing.

Fairing assembly and method therefor

An example seal for use with a laminated window is described. The seal includes a first end formed from a first material and a second end formed from the first material, with the first material being compressible when a pressure force is applied to the first material. The seal also includes a connection portion positioned between the first end and the second end. At least some of the connection portion is formed from a second material having a greater indentation hardness than an indentation hardness of the first material. An example method for installing a seal is also described.

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Long Beach, CA, United States of America

Drew L Smallwood