Company Filing History:
Years Active: 1999-2001
Title: Bruce A. Stauffer: Innovator in Turbomachinery Design
Introduction
Bruce A. Stauffer is a notable inventor based in Scotland, CT (US). He has made significant contributions to the field of turbomachinery, particularly in the design of turbine blades for gas turbine engines. With a total of 2 patents to his name, Stauffer's work has advanced the efficiency and manufacturability of turbine components.
Latest Patents
Stauffer's latest patents include innovative designs that enhance the functionality of turbine blades. One of his patents, titled "Turbomachinery blade or vane with a survivable machining datum," describes a turbine blade that incorporates a machining datum and support tool interface. This design features a frustoconical depression in the blade's outer shroud, which is aligned with the airfoil stacking line. The depression serves as a support feature during manufacturing and remains useful for post-manufacturing inspection and repair.
Another patent, "Turbomachinery blade or vane with a permanent machining datum," presents a turbine blade that includes a machining datum extending radially from a pocket in the outer shroud. This datum is designed to be peripherally continuous, ensuring its availability for inspection and repair operations, regardless of the blade's manufacturing state.
Career Highlights
Bruce A. Stauffer is currently employed at United Technologies Corporation, where he continues to innovate in the field of turbomachinery. His work has been instrumental in developing advanced turbine technologies that improve performance and reliability.
Collaborations
Stauffer collaborates with fellow inventor Gilbert B. Wilcox, contributing to the advancement of turbine blade technology through shared expertise and innovative ideas.
Conclusion
Bruce A. Stauffer's contributions to turbomachinery design have made a significant impact on the industry. His patents reflect a commitment to enhancing the manufacturability and functionality of turbine blades, ensuring their effectiveness in gas turbine engines.