17961747. SYSTEMS AND METHODS FOR DEICING AIRCRAFT simplified abstract (The Boeing Company)

SYSTEMS AND METHODS FOR DEICING AIRCRAFT

Organization Name

The Boeing Company

Inventor(s)

Mark Everette Albrecht of Lake Stevens WA (US)

Richard John Loftis of Daniel Island SC (US)

Marcus Anthony Belcher of Sammamish WA (US)

Edwin John Smith of Everett WA (US)

Kristofer Logan Peterson of Lynnwood WA (US)

Collin William Childs of Newcastle WA (US)

Benjamin David Walker of West Linn OR (US)

Jonathan William Udell of Renton WA (US)

Doria Pei of Seattle WA (US)

Robert N. Jaeger of Seattle WA (US)

Sara Jane Lynn of Spokane Valley WA (US)

Mirza Mustafayev of Everett WA (US)

Ignas Sabet-kazilas of Snoqualmie WA (US)

Varun Suri of Huntsville AL (US)

SYSTEMS AND METHODS FOR DEICING AIRCRAFT - A simplified explanation of the abstract

This abstract first appeared for US patent application 17961747 titled 'SYSTEMS AND METHODS FOR DEICING AIRCRAFT

Simplified Explanation

The abstract describes an aircraft with thermal emitters integrated into external structures to deice them using generated heat.

• The aircraft includes external structures with integrated thermal emitters.
• The thermal emitters generate heat to deice the external structures.
• The thermal emitters can receive electrical power from various sources like the aircraft's auxiliary power unit, power distribution system, engines, or an external power cart.

Potential Applications

This technology could be applied in the aviation industry for deicing aircraft external structures, ensuring safe operation in cold weather conditions.

Problems Solved

This innovation solves the problem of ice buildup on aircraft external structures, which can compromise aerodynamics and safety during flight.

Benefits

The use of integrated thermal emitters provides a more efficient and reliable deicing solution for aircraft, improving overall performance and safety.

Potential Commercial Applications

A potential commercial application for this technology could be in the manufacturing and installation of deicing systems for various aircraft models.

Possible Prior Art

Prior art may include existing deicing systems for aircraft that rely on different methods such as chemical treatments or pneumatic systems.

How does this technology compare to traditional deicing methods in terms of efficiency and cost-effectiveness?

This article does not provide a direct comparison between this technology and traditional deicing methods. Further research or testing may be needed to determine the efficiency and cost-effectiveness of this innovation.

Are there any regulatory approvals required for implementing this technology on commercial aircraft?

The article does not address the regulatory aspect of implementing this technology on commercial aircraft. It is essential to consider any necessary approvals or certifications before widespread adoption in the aviation industry.

Original Abstract Submitted

An aircraft includes external structures, and one or more thermal emitters integrated with one or more of the external structures. The one or more thermal emitters are configured to generate heat to deice the one or more external structures. The one or more thermal emitters are configured to receive electrical power from one or more of an auxiliary power unit of the aircraft, a power distribution system of the aircraft, one or more engines of the aircraft, or an external power cart that is separate and distinct from the aircraft.