17958690. PLATFORM OUTSIDE DIAMETER CHANNEL FOR DUAL SUPPLY PRESSURE VANE APPLICATIONS simplified abstract (Raytheon Technologies Corporation)
Contents
- 1 PLATFORM OUTSIDE DIAMETER CHANNEL FOR DUAL SUPPLY PRESSURE VANE APPLICATIONS
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 PLATFORM OUTSIDE DIAMETER CHANNEL FOR DUAL SUPPLY PRESSURE VANE APPLICATIONS - 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 Unanswered Questions
- 1.11 Original Abstract Submitted
PLATFORM OUTSIDE DIAMETER CHANNEL FOR DUAL SUPPLY PRESSURE VANE APPLICATIONS
Organization Name
Raytheon Technologies Corporation
Inventor(s)
Rafael A. Perez Reisler of Arecibo PR (US)
Efrain Vega Rios of Manati PR (US)
Andres Diaz Alvarado of Humacao PR (US)
PLATFORM OUTSIDE DIAMETER CHANNEL FOR DUAL SUPPLY PRESSURE VANE APPLICATIONS - A simplified explanation of the abstract
This abstract first appeared for US patent application 17958690 titled 'PLATFORM OUTSIDE DIAMETER CHANNEL FOR DUAL SUPPLY PRESSURE VANE APPLICATIONS
Simplified Explanation
The outer platform leading edge cooling system described in the patent application includes a radially outer platform with a platform leading edge, a hollow cooling channel along the platform leading edge, an inlet port in the radially outer end region of the platform leading edge, and an outlet conduit connected to a trailing edge cavity.
- Radially outer platform with platform leading edge
- Hollow cooling channel along the platform leading edge
- Inlet port in the radially outer end region
- Outlet conduit connected to a trailing edge cavity
Potential Applications
The technology could be applied in gas turbine engines, aircraft engines, and other high-temperature applications where cooling of leading edges is crucial.
Problems Solved
This innovation addresses the issue of overheating and potential damage to the leading edges of platforms in high-temperature environments.
Benefits
- Improved cooling efficiency - Enhanced durability and longevity of components - Increased performance and reliability in high-temperature conditions
Potential Commercial Applications
"Leading Edge Cooling System for Gas Turbine Engines and Aircraft"
Possible Prior Art
Prior art may include similar cooling systems used in gas turbine engines or other high-temperature applications.
Unanswered Questions
How does the system handle different airflow conditions?
The patent abstract does not specify how the system adjusts to varying airflow conditions to ensure optimal cooling efficiency.
What materials are used in the construction of the cooling channel?
The abstract does not mention the specific materials used in the construction of the cooling channel, which could impact the system's effectiveness and longevity.
Original Abstract Submitted
An outer platform leading edge cooling system includes a radially outer platform having a platform leading edge; a hollow cooling channel is defined extending generally longitudinally along the platform leading edge of the radially outer platform; an inlet port located in a radially outer end region of the platform leading edge being fluidly coupled with the hollow cooling channel; and the hollow cooling channel comprising an outlet conduit extending from a cooling channel exit, the outlet conduit being connected in fluid flow communication with a trailing edge cavity.
