18575954. FOIL, ROTOR BLADE, ASSEMBLY FOR A TURBOMACHINE ROTOR AND ROTOR simplified abstract (SAFRAN AIRCRAFT ENGINES)
Contents
FOIL, ROTOR BLADE, ASSEMBLY FOR A TURBOMACHINE ROTOR AND ROTOR
Organization Name
Inventor(s)
Nicolas Daniel Delaporte of MOISSY-CRAMAYEL (FR)
Pierre Marie Mulheim of MOISSY-CRAMAYEL (FR)
Arnaud Martine of MOISSY-CRAMAYEL (FR)
Antoine Giguet of MOISSY-CRAMAYEL (FR)
Vincent Goyon of MOISSY-CRAMAYEL (FR)
FOIL, ROTOR BLADE, ASSEMBLY FOR A TURBOMACHINE ROTOR AND ROTOR - A simplified explanation of the abstract
This abstract first appeared for US patent application 18575954 titled 'FOIL, ROTOR BLADE, ASSEMBLY FOR A TURBOMACHINE ROTOR AND ROTOR
The abstract describes a foil and a root of a blade of a turbomachine rotor, where the foil is longitudinally retained relative to the root of the blade to ensure stability.
- The foil and root assembly includes a base and two side limbs connected by the base.
- The first limb has a recess with folds in two different directions to engage with a notch in the root of the blade.
- This design ensures the foil is securely retained in a longitudinal direction relative to the blade's root.
Potential Applications: - Aerospace industry for turbomachinery applications - Power generation for gas turbines - Marine propulsion systems
Problems Solved: - Ensures stability and alignment of the foil with the blade's root - Prevents unwanted movement or dislodging of the foil during operation
Benefits: - Improved efficiency and performance of turbomachinery - Enhanced safety and reliability in operation - Simplified assembly and maintenance processes
Commercial Applications: Title: "Advanced Foil and Root Assembly for Turbomachinery" This technology can be used in various turbomachinery applications across industries such as aerospace, power generation, and marine propulsion. It offers improved performance, reliability, and maintenance efficiency, making it a valuable innovation for companies operating in these sectors.
Questions about the technology: 1. How does the foil and root assembly contribute to the overall efficiency of turbomachinery systems? 2. What are the key factors that ensure the longitudinal retention of the foil relative to the blade's root?
Frequently Updated Research: Stay updated on the latest advancements in turbomachinery design and manufacturing techniques to enhance the performance and reliability of these systems. Regularly review industry publications and research studies to incorporate new findings into the development of foil and root assemblies for turbomachinery applications.
Original Abstract Submitted
A foil and a root of a blade of a turbomachine rotor and includes a base, two side limbs that are connected to each other by the base, at least the first limb includes at least one recess including at least two folds in two different directions, the recess being capable of engaging with a notch provided in the root of the blade to ensure the foil is longitudinally retained relative to the root of the blade at least in a longitudinal direction.
