The boeing company (20240254943). MULTIPLE TURN REVERSER WITH SIDE TURNING VANES simplified abstract

MULTIPLE TURN REVERSER WITH SIDE TURNING VANES

Organization Name

the boeing company

Inventor(s)

Chen Chuck of Mercer Island WA (US)

Brian S. Kornegay of Snohomish WA (US)

MULTIPLE TURN REVERSER WITH SIDE TURNING VANES - A simplified explanation of the abstract

This abstract first appeared for US patent application 20240254943 titled 'MULTIPLE TURN REVERSER WITH SIDE TURNING VANES

Simplified Explanation:

The patent application describes a thrust reverser for an engine that can direct gas in two different directions to create reverse thrust.

• The first reverser portion directs gas in a first direction to generate reverse thrust.
• The second reverser portion directs gas in a different direction from the first portion.
• The second reverser portion can be located either upstream or downstream from the first reverser portion.

Key Features and Innovation:

• Dual-direction gas flow for reverse thrust.
• Flexibility in positioning of the second reverser portion.
• Enhanced control over reverse thrust generation.

Potential Applications:

The technology can be applied in aircraft engines, industrial machinery, and marine propulsion systems.

Problems Solved:

• Improving maneuverability and braking capabilities.
• Enhancing safety during landing and takeoff procedures.

Benefits:

• Increased efficiency in thrust reversal.
• Enhanced control and performance in various applications.

Commercial Applications:

Title: Innovative Thrust Reverser Technology for Enhanced Performance in Aircraft Engines

This technology can revolutionize the aviation industry by improving safety and efficiency in aircraft operations. It can also have significant implications in the industrial and marine sectors where precise control over thrust is crucial.

Questions about Thrust Reverser Technology:

1. How does the positioning of the second reverser portion impact the efficiency of reverse thrust generation? 2. What are the potential cost savings associated with implementing this dual-direction thrust reverser technology?

Original Abstract Submitted

a thrust reverser in an engine includes a first reverser portion configured to direct a gas in a first direction to create reverse thrust. the thrust reverser also includes a second reverser portion configured to direct the gas in a second direction that is different than the first direction. the second reverser portion is upstream or downstream from the first reverser portion.