TURBOJET ENGINE NOZZLE RING FOR AN AIRCRAFT

Organization Name

SAFRAN AIRCRAFT ENGINES

Inventor(s)

Alice Marie Clement of MOISSY-CRAMAYEL (FR)

Paul Grandin of MOISSY-CRAMAYEL (FR)

Clément Marchand of MOISSY-CRAMAYEL (FR)

Vijeay Patel of MOISSY-CRAMAYEL (FR)

Mireya Sanchez Gomez of MOISSY-CRAMAYEL (FR)

TURBOJET ENGINE NOZZLE RING FOR AN AIRCRAFT - A simplified explanation of the abstract

This abstract first appeared for US patent application 18278991 titled 'TURBOJET ENGINE NOZZLE RING FOR AN AIRCRAFT

The turbomachine subassembly described in the patent application includes at least one low-pressure nozzle ring with an integral root, a clamp to fasten the root to the turbomachine casing, and at least two pads positioned between the root and the clamp in a form-fitting manner.

The subassembly consists of a low-pressure nozzle ring with an integrated root.
A clamp is utilized to secure the root to the turbomachine casing.
Two pads are placed between the root and the clamp for proper assembly.
Each pad is fitted snugly with either the root or the clamp.
The design aims to enhance the efficiency and performance of the turbomachine.

Potential Applications: - Aerospace industry for aircraft engines - Power generation plants - Marine propulsion systems

Problems Solved: - Improved stability and alignment of the nozzle ring - Enhanced durability and longevity of the turbomachine components

Benefits: - Increased efficiency and performance - Reduced maintenance and repair costs - Extended lifespan of the turbomachine

Commercial Applications: Title: Innovative Turbomachine Subassembly for Enhanced Performance This technology can be applied in various industries such as aerospace, power generation, and marine propulsion, offering improved efficiency and durability.

Questions about Turbomachine Subassembly: 1. How does the design of the subassembly contribute to the overall performance of the turbomachine? 2. What are the potential cost-saving benefits of using this innovative subassembly technology?

Frequently Updated Research: Stay updated on the latest advancements in turbomachine subassembly technology to ensure optimal performance and efficiency in various applications.

Original Abstract Submitted

The turbomachine subassembly comprises:—at least one tow-pressure nozzle ring, the nozzle ring comprising a root () integral with the nozzle ring;—a clamp () configured so as to fasten the root to a casing of the turbomachine; and—at least two pads () interposed between the root and the clamp, each pad being assembled in a form-fitting manner with one of either the root or the clamp.