Auto-adaptive braze dispensing systems and methods
Systems and methods for moving a substrate to a vision system using a robot; using the vision system to determine where a braze material is to be applied to the substrate; moving the substrate to a braze dispenser using the robot; applying a braze material to the substrate using the braze dispenser based on the determination from the vision system; and using the vison system to determine whether to apply additional braze to the substrate, including for the substrate of a component for gas turbine engine, such as configured for use in an aircraft.
1. An automated method of applying a braze material to a substrate, comprising:
moving the substrate to a vision system using a robot controlled by a controller, the controller configured to communicate with and control the vision system, a braze dispenser, the robot, and a control interface; subsequently
identifying, by the vision system, an identifier for the substrate; subsequently
identifying, by the vision system, an expected configuration based on the identifier; subsequently
identifying, by the vision system, a crack or a hole in the substrate based on the expected configuration of the substrate; subsequently
determining, by the vision system, a first location where the braze material is to be applied to the substrate based on identifying the crack or the hole;
moving the substrate to the braze dispenser using the robot;
applying the braze material to the substrate using the braze dispenser based on the first location from the vision system; and
determining, by the vision system, whether to apply additional braze material to the substrate at a second location.
2. The automated method of claim 1 , wherein the braze dispenser applies the braze material to the substrate at approximately 0.011-0.11 pounds (5-50 grams) per minute.
3. The automated method of claim 1 , wherein the braze dispenser applies the braze material to the substrate at approximately 0.008-0.016 inches (0.2-0.4 millimeters) per pass.
4. The automated method of claim 1 , wherein a thickness of the applied braze material is approximately 0.01-0.06 inches (0.254-1.524 millimeters).
5. The automated method of claim 1 , wherein the braze dispenser applies the braze material to the substrate at a distance of approximately 0.049-0.059 inches (1.25-1.5 millimeters) away from the substrate.
6. The automated method of claim 1 , wherein the substrate is a component of a gas turbine engine.
7. The automated method of claim 6 , wherein the gas turbine engine is configured for use in an aircraft.
8. An automated method of applying a braze material to a component of a gas turbine engine of an aircraft, comprising:
moving the component to a vision system using a robot controlled by a controller, the controller configured to communicate with and control the vision system, a braze dispenser, the robot, and a control interface; subsequently
identifying, by the vision system, an identifier for the component subsequently
identifying, by the vision system, an expected configuration based on the identifier; subsequently
identifying, by the vision system, a crack or a hole in the component based on the expected configuration of the component; subsequently
determining, by the vision system, a first location where the braze material is to be applied to the component based on identifying the crack or the hole;
moving the component to the braze dispenser using the robot;
applying the braze material to the component using the braze dispenser based on the first location from the vision system; and
determining, by the vision system, whether to apply additional braze material to the component at a second location.
9. The automated method of claim 8 , wherein the braze dispenser applies the braze material to the component at approximately 0.011-0.11 pounds (5-50 grams) per minute.
10. The automated method of claim 8 , wherein the braze dispenser applies the braze material to the component at approximately 0.008-0.016 inches (0.2-0.4 millimeters) per pass.
11. The automated method of claim 8 , wherein a thickness of the applied braze material is approximately 0.01-0.06 inches (0.254-1.524 millimeters).
12. The automated method of claim 8 , wherein the braze dispenser applies the braze material to the component at a distance of approximately 0.049-0.059 inches (1.25-1.5 millimeters) away from the component.