View source for 20240044258. VANE MULTIPLET WITH CONJOINED SINGLET VANES simplified abstract (Raytheon Technologies Corporation)

=VANE MULTIPLET WITH CONJOINED SINGLET VANES=


==Organization Name==

[[:Category:Raytheon Technologies Corporation|Raytheon Technologies Corporation]]


[[Category:Raytheon Technologies Corporation]]

==Inventor(s)==

[[:Category:David J. Wasserman of Hamden CT (US)|David J. Wasserman of Hamden CT (US)]][[Category:David J. Wasserman of Hamden CT (US)]]

[[:Category:Raymond Surace of Newington CT (US)|Raymond Surace of Newington CT (US)]][[Category:Raymond Surace of Newington CT (US)]]

==VANE MULTIPLET WITH CONJOINED SINGLET VANES - A simplified explanation of the abstract==


This abstract first appeared for US patent application 20240044258 titled 'VANE MULTIPLET WITH CONJOINED SINGLET VANES

==Simplified Explanation==

The abstract describes a patent application for a vane multiplet that consists of two ceramic matrix composite (CMC) singlet vanes arranged next to each other. Each singlet vane has an airfoil section and a platform at one end. The platform has forward and trailing edges, as well as circumferential side edges. The singlet vanes are joined together by a CMC overwrap, which includes fused fiber plies on the platforms.

* The patent application is for a vane multiplet made of ceramic matrix composite (CMC) singlet vanes.
* Each singlet vane has an airfoil section and a platform at one end.
* The platform has forward and trailing edges, as well as circumferential side edges.
* The singlet vanes are joined together by a CMC overwrap, which includes fused fiber plies on the platforms.

Potential Applications:
* Gas turbine engines
* Aerospace industry
* Power generation systems

Problems Solved by this Technology:
* Increased efficiency and performance of gas turbine engines
* Enhanced durability and lifespan of vane components
* Reduction in weight and fuel consumption

Benefits of this Technology:
* Improved engine performance and efficiency
* Increased durability and lifespan of vane components
* Reduced weight and fuel consumption


==Original Abstract Submitted==

a vane multiplet includes first and second ceramic matrix composite (cmc) singlet vanes that are arranged circumferentially adjacent each other. each of the cmc singlet vanes includes an airfoil section and a platform at one end of the airfoil section. the platform defines forward and trailing platform edges and first and second circumferential side edges. a cmc overwrap conjoins the cmc singlet vanes. the cmc overwrap includes fiber plies that are fused to the platforms of the cmc singlet vanes.



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