18081844. ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE simplified abstract (General Electric Company)
Contents
- 1 ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE - A simplified explanation of the abstract
- 1.4 Simplified Explanation
- 1.5 Potential Applications
- 1.6 Problems Solved
- 1.7 Benefits
- 1.8 Potential Commercial Applications
- 1.9 Possible Prior Art
- 1.10 Original Abstract Submitted
ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE
Organization Name
Inventor(s)
Michal Tomasz Kuropatwa of Warsaw (PL)
Adam Wojciech Deskiewicz of Warsaw (PL)
Robert Kaminski of Warsaw (PL)
Nicholas Joseph Kray of Mason OH (US)
ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE - A simplified explanation of the abstract
This abstract first appeared for US patent application 18081844 titled 'ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE
Simplified Explanation
The rotor assembly described in the patent application includes a spool with apertures arranged in a row, and a blade assembly with blades connected via a platform that extend through the apertures.
- The rotor assembly includes a spool with apertures arranged in a row.
- The blade assembly comprises at least two blades connected via a platform.
- Each blade extends through a respective aperture in the spool.
Potential Applications
The rotor assembly could be used in gas turbine engines for various applications such as power generation, aviation, and marine propulsion.
Problems Solved
This technology allows for efficient and reliable operation of gas turbine engines by securely connecting the blades to the spool, ensuring optimal performance.
Benefits
The rotor assembly provides improved stability, durability, and performance in gas turbine engines, leading to increased efficiency and reduced maintenance costs.
Potential Commercial Applications
The rotor assembly could be utilized in commercial aircraft engines, power plants, and marine vessels, offering enhanced performance and reliability.
Possible Prior Art
One possible prior art could be similar rotor assemblies used in gas turbine engines for various applications.
Unanswered Questions
How does the rotor assembly impact fuel efficiency in gas turbine engines?
The rotor assembly's impact on fuel efficiency in gas turbine engines is not explicitly addressed in the abstract. However, by providing improved stability and performance, it could potentially lead to increased fuel efficiency.
What materials are used in the construction of the rotor assembly?
The abstract does not mention the specific materials used in the construction of the rotor assembly. Further details on the materials and their properties would be beneficial for understanding the assembly's durability and performance.
Original Abstract Submitted
A rotor assembly is provided, along with gas turbine engines for its use. The rotor assembly may include a spool defining a plurality of apertures arranged in a first row and spaced circumferentially around the spool, wherein each aperture of the plurality of apertures extends through the spool from a radially inward-facing surface to a radially outward-facing surface; and a blade assembly comprising at least two blades connected to each other via a platform, wherein each blade extends through a respective aperture.
