18678303. TURBOMACHINE AND METHOD OF ASSEMBLY simplified abstract (General Electric Company)
Contents
TURBOMACHINE AND METHOD OF ASSEMBLY
Organization Name
Inventor(s)
Jixian Yao of Niskayuna NY (US)
Trevor Howard Wood of Clifton Park NY (US)
Kishore Ramakrishnan of Rexford NY (US)
William Joseph Solomon of Montgomery OH (US)
Giridhar Jothiprasad of Clifton Park NY (US)
Aaron J. King of West Harrison OH (US)
TURBOMACHINE AND METHOD OF ASSEMBLY - A simplified explanation of the abstract
This abstract first appeared for US patent application 18678303 titled 'TURBOMACHINE AND METHOD OF ASSEMBLY
The patent application describes a turbomachine with an annular casing, a fan inside the casing, and an airfoil with unique features.
- The fan blades extend radially outward towards the annular casing.
- The airfoil has a waveform along its leading edge, defined by multiple chord sections.
- The fan's performance is determined by factors such as average chord fan width and quantity of fan blades.
Potential Applications: - Aerospace industry for aircraft engines - Power generation for gas turbines - Marine propulsion systems
Problems Solved: - Improved aerodynamic efficiency - Enhanced performance and fuel efficiency - Reduced noise and vibration levels
Benefits: - Increased power output - Lower operating costs - Extended equipment lifespan
Commercial Applications: Title: Innovative Turbomachine Technology for Enhanced Performance This technology can be utilized in various industries such as aerospace, power generation, and marine propulsion systems, offering improved efficiency and performance.
Prior Art: Researchers can explore prior patents related to turbomachinery design, airfoil technology, and fan blade configurations to understand the evolution of this innovation.
Frequently Updated Research: Ongoing research focuses on optimizing fan blade designs, enhancing aerodynamic performance, and reducing environmental impact through innovative turbomachine technologies.
Questions about Turbomachine Technology: 1. How does this technology compare to traditional turbomachinery designs? This technology offers improved aerodynamic efficiency and performance compared to traditional designs, leading to enhanced overall system efficiency.
2. What are the key factors influencing the performance of the fan in this turbomachine? The performance of the fan is influenced by factors such as average chord fan width and the quantity of fan blades, which impact aerodynamic efficiency and power output.
Original Abstract Submitted
A turbomachine includes an annular casing, a fan disposed inside the annular casing and mounted for rotation about an axial centerline, and an airfoil. The fan includes fan blades that extend radially outwardly toward the annular casing. The airfoil includes a first side and a second side coupled together at a leading edge and a trailing edge, a plurality of first chord sections defining at least one first chord length, and a plurality of second chord sections defining at least one second chord length. The plurality of first chord sections and second chord sections define a waveform along a leading edge of the airfoil. The fan has an average chord fan width according to a first performance factor. The fan has a quantity of fan blades according to a second performance factor.
