Rtx Corporation

Applied University Research, Inc.

Virginia Tech Intellectual Properties Inc.

Gwibo Byun

Roger Lyndon Simpson

Kevin Todd Lowe

Albert P Krejmas

An aircraft includes a gas turbine engine and an optically-based measurement system. The gas turbine engine is configured to ingest a first mass flow and to exhaust a second mass flow. The optically-based measurement system is configured to determine the first and second mass flows in response to performing an imaging process on the gas turbine engine.

In-flight measured propulsion mass flow and thrust on aircraft

Several practical refinements, extensions, additions, and improvements to the manufactured three-dimensional continuous convex-concave fairing with attached vortex generators are provided. The piecewise continuously varying slope and curvature fairings provide manufacturing cost reductions, as well as cost reductions by reducing the frequency and complexity of monitoring practices for bridges and elimination of temporary fixes that require costly annual or periodic engineering studies and construction to mitigate scour on at-risk bridges. The probability of bridge failure and its associated liability to the public is totally avoided since the root cause of local scour is prevented.

Growing community of inventors

Blacksburg, VA, United States of America

Gwibo Byun