18678321. 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 18678321 titled 'TURBOMACHINE AND METHOD OF ASSEMBLY
Simplified Explanation:
This patent application describes a gas turbine engine with a variable bleed assembly that includes a fan, a core turbine engine, and a variable bleed duct.
- The gas turbine engine has an annular casing and a fan with fan blades that rotate inside the casing.
- The core turbine engine is connected to the fan and consists of a compressor section, a combustion section, and a turbine section.
- The variable bleed assembly includes a duct that extends between a VB inlet and a VB outlet.
Key Features and Innovation:
- Gas turbine engine with variable bleed assembly
- Fan with fan blades and annular casing
- Core turbine engine with compressor, combustion, and turbine sections
- Variable bleed duct for controlling airflow
Potential Applications:
This technology can be used in aircraft engines, power generation systems, and industrial applications where efficient and controlled airflow is essential.
Problems Solved:
This technology addresses the need for improved airflow control, increased efficiency, and better performance in gas turbine engines.
Benefits:
- Enhanced airflow control
- Improved efficiency
- Better overall performance
Commercial Applications:
Potential commercial applications include aircraft propulsion systems, power plants, and industrial machinery where gas turbine engines are used.
Prior Art:
Readers interested in prior art related to this technology can explore patents and research papers on gas turbine engines, variable bleed systems, and airflow control mechanisms.
Frequently Updated Research:
Researchers are continually studying ways to enhance the performance and efficiency of gas turbine engines, including advancements in variable bleed technology.
Questions about Gas Turbine Engine with Variable Bleed Assembly:
1. How does the variable bleed assembly impact the overall efficiency of the gas turbine engine? 2. What are the potential challenges in implementing this technology in different applications?
1. A relevant generic question not answered by the article, with a detailed answer. - How does the variable bleed assembly contribute to reducing emissions in gas turbine engines? The variable bleed assembly helps optimize airflow, leading to more efficient combustion and potentially lower emissions.
2. Another relevant generic question, with a detailed answer. - What role does the fan play in the operation of the gas turbine engine? The fan helps draw in air, compress it, and deliver it to the combustion chamber, essential for the engine's overall performance and efficiency.
Original Abstract Submitted
A gas turbine engine includes an annular casing, a fan disposed inside the annular casing and mounted for rotation about an axial centerline, a core turbine engine drivingly coupled to the fan and comprising a compressor section, a combustion section, and a turbine section arranged in serial flow order, and a variable bleed assembly comprising a variable bleed duct extending between a VB inlet and a VB outlet. The fan includes fan blades that extend radially outwardly toward the annular casing. 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.
