17987101. COATING COMPOSITION, COATED TURBINE COMPONENT, AND METHOD OF APPLYING THE COATING simplified abstract (General Electric Company)
Contents
- 1 COATING COMPOSITION, COATED TURBINE COMPONENT, AND METHOD OF APPLYING THE COATING
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 COATING COMPOSITION, COATED TURBINE COMPONENT, AND METHOD OF APPLYING THE COATING - 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 How does this coating composition compare to existing coatings in terms of performance and longevity?
- 1.11 What specific turbine components can benefit the most from this coating technology?
- 1.12 Original Abstract Submitted
COATING COMPOSITION, COATED TURBINE COMPONENT, AND METHOD OF APPLYING THE COATING
Organization Name
Inventor(s)
Eklavya Calla of Bangalore (IN)
Ritwik Biswas of Bangalore (IN)
COATING COMPOSITION, COATED TURBINE COMPONENT, AND METHOD OF APPLYING THE COATING - A simplified explanation of the abstract
This abstract first appeared for US patent application 17987101 titled 'COATING COMPOSITION, COATED TURBINE COMPONENT, AND METHOD OF APPLYING THE COATING
Simplified Explanation
The abstract describes a patent application for a coating composition containing aluminum, a carbide, and nickel-chromium (Ni-20Cr), which is sprayed onto turbine components.
- The composition includes a blend of a carbide and nickel-chromium (Ni-20Cr) with aluminum (Al) in specific weight ranges.
- The method involves blending the components to form the composition and then spraying it onto turbine components.
Potential Applications
The technology can be applied in the aerospace industry for coating turbine components to improve their performance and durability.
Problems Solved
1. Enhanced protection against corrosion and wear on turbine components. 2. Improved thermal resistance and overall performance of the coated parts.
Benefits
1. Increased lifespan of turbine components. 2. Reduced maintenance and replacement costs. 3. Enhanced efficiency and reliability of turbines.
Potential Commercial Applications
Optimizing Turbine Performance with Aluminum-Carbide-Nickel-Chromium Coating Technology
Possible Prior Art
There may be prior art related to similar coating compositions used in the aerospace or industrial sectors.
Unanswered Questions
How does this coating composition compare to existing coatings in terms of performance and longevity?
The article does not provide a direct comparison with existing coatings in the market.
What specific turbine components can benefit the most from this coating technology?
The article does not specify which turbine components would benefit the most from this coating technology.
Original Abstract Submitted
A composition includes aluminum (Al), and a blend of a carbide and nickel-chromium (Ni-20Cr). The method of applying a coating composition includes blending a carbide and nickel-chromium (Ni-20Cr) with aluminum (Al) to form a composition, the carbide and the nickel-chromium (Ni-20Cr) in a range between 90% and about 99.5% by weight of the composition, and wherein the aluminum (Al) is in a range between about 0.5% and less than about 10% by weight of the composition; and spraying the composition on the turbine component.
