17958946. FLANGE AND ASSEMBLY FOR GAS TURBINE ENGINE CASE simplified abstract (Raytheon Technologies Corporation)

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FLANGE AND ASSEMBLY FOR GAS TURBINE ENGINE CASE

Organization Name

Raytheon Technologies Corporation

Inventor(s)

Jonas Banhos of West Hartford CT (US)

Thiago B. Vieira of Sarasota FL (US)

Anthony J. Prainito of Shelton CT (US)

James T. Roach of Vernon CT (US)

FLANGE AND ASSEMBLY FOR GAS TURBINE ENGINE CASE - A simplified explanation of the abstract

This abstract first appeared for US patent application 17958946 titled 'FLANGE AND ASSEMBLY FOR GAS TURBINE ENGINE CASE

Simplified Explanation

The patent application describes a flange stiffener support for a duct in a gas turbine engine, featuring a circumferential flange segment with flange fastener openings and an axial body segment with body fastener openings.

  • The flange stiffener support includes a circumferential flange segment with multiple flange fastener openings.
  • It also has an axial body segment extending from the inner side of the circumferential segment, with at least one body fastener opening.
  • The axial body segment runs along a portion of the circumferential distance of the flange segment.

Potential Applications

The technology could be applied in gas turbine engines, aerospace industry, and other machinery requiring duct support.

Problems Solved

The innovation provides structural support for ducts in gas turbine engines, enhancing stability and performance.

Benefits

The flange stiffener support improves the overall durability and reliability of gas turbine engines, reducing maintenance needs and increasing operational efficiency.

Potential Commercial Applications

Potential commercial applications include gas turbine engine manufacturers, aerospace companies, and industrial machinery producers.

Possible Prior Art

Prior art may include similar designs for flange stiffener supports in gas turbine engines or other machinery.

Unanswered Questions

How does the design of the flange stiffener support impact the overall weight of the gas turbine engine?

The article does not provide information on the weight implications of the new design.

Are there any specific materials recommended for manufacturing the flange stiffener support?

The article does not mention any preferred materials for constructing the support.


Original Abstract Submitted

A flange stiffener support for a duct in a gas turbine engine includes a circumferential flange segment that has a plurality of flange fastener openings. An axial body segment extends from a radially inner side of the circumferential segment and has at least one body fastener opening. The axial body segment extends at least partially along a circumferential distance of the circumferential flange segment.