20240035383. AIRFOIL JOINING APPARATUS AND METHODS simplified abstract (General Electric Company)

AIRFOIL JOINING APPARATUS AND METHODS

Organization Name

General Electric Company

Inventor(s)

Suhas Prabhakar Vaze of Loveland OH (US)

Timothy Trapp of Cincinnati OH (US)

Scott Sager Campbell of Columbus OH (US)

Gregory Christopher Firestone of Pickerington OH (US)

Jonathan David Mast of Lebanon OH (US)

Timothy Vernon Stotler of Columbus OH (US)

AIRFOIL JOINING APPARATUS AND METHODS - A simplified explanation of the abstract

This abstract first appeared for US patent application 20240035383 titled 'AIRFOIL JOINING APPARATUS AND METHODS

Simplified Explanation

The abstract describes an airfoil component that can be attached to a cropped airfoil. The cropped airfoil has an attachment section and two sides that extend between edges to define a chord length. The airfoil component has a body with two sides and an attachment section for attaching it to the cropped airfoil. The attachment section is larger than the cropped airfoil attachment section, resulting in a longer chord length for the airfoil component.

• The patent application describes an airfoil component designed to attach to a cropped airfoil.
• The cropped airfoil has an attachment section and two sides that define a chord length.
• The airfoil component has a body with an attachment section for attaching it to the cropped airfoil.
• The attachment section of the airfoil component is larger than the attachment section of the cropped airfoil, resulting in a longer chord length.
• The invention provides systems and methods for attaching the airfoil component to the cropped airfoil.

Potential Applications:

• This technology can be used in the aerospace industry for improving the performance of aircraft wings.
• It can be applied in the design and manufacturing of high-performance airfoils for aircraft and drones.
• The airfoil component can be used to enhance lift and reduce drag, improving the overall efficiency of the airfoil.

Problems Solved:

• The airfoil component solves the problem of limited chord length in cropped airfoils.
• It allows for the attachment of a larger component with a longer chord length, improving the aerodynamic characteristics of the airfoil.
• This technology addresses the need for increased lift and reduced drag in aircraft design.

Benefits:

• The airfoil component increases the lift generated by the airfoil, leading to improved aircraft performance.
• It reduces drag, resulting in increased fuel efficiency and reduced operating costs.
• The technology offers flexibility in airfoil design, allowing for customized solutions for different aircraft applications.

Original Abstract Submitted

an airfoil component for attaching to a cropped airfoil is provided. the cropped airfoil comprises a cropped airfoil attachment section and a cropped first side opposite a cropped second side, which each extend axially between a cropped first edge and a cropped second edge to define a cropped chord length. the airfoil component comprises a body having a component first side opposite a component second side. the body defines an attachment section for attaching the airfoil component to the cropped airfoil at the cropped airfoil attachment section. the attachment section extends axially between a component first edge and a component second edge to define a component chord length, and the attachment section is oversized with respect to the cropped airfoil attachment section such that the component chord length is longer than the cropped chord length. systems and methods also are provided.