Keith Christopher Goldfinch

This inventor holds 9 USPTO granted patents and 1 published patent application and 9 EPO patents. Top assignee: Rolls-Royce Corporation. Active years: 2007-2019.

USPTO Granted Patents = 9 (Patent Applications = 1)

% Patents Active = 22.2

EPO Patents = 9 (Patent Applications = 4)

Average Co-Inventor Count = 2.0

ph-index = 4

Forward Citations = 39(Granted Patents)

Location History:

Bristol, GB (2007 - 2014)
Singapore, SG (2019)

Company Filing History:

9 out of 6,025

Rolls-Royce Corporation

patents

Years Active: 2007-2019

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9 patents (USPTO):Sort by Forward CitationsExplore Patents

1. 10364687 - Fan containing fan blades with a U-shaped slot having a decreased length planar section (2019-07-30),

2. 8857054 - Method of forming an aerofoil with a damping filler (2014-10-14),

3. 8579181 - Method of forming an internal structure in a hollow component (2013-11-12),

4. 8529720 - Aerofoil sub-assembly, an aerofoil and a method of making an aerofoil (2013-09-10),

5. 8381398 - Component with a damping filler and method (2013-02-26),

6. 8225506 - Method of manufacturing a rotor for a gas turbine engine that includes identifying the frequency response of the rotor and adjusting the frequency response by providing a pressure gradient within the rotor (2012-07-24),

7. 8186057 - Bladed rotor balancing (2012-05-29),

8. 8182233 - Component with a damping filler (2012-05-22),

9. 7306434 - Reduction of co-efficient of friction to reduce stress ratio in bearings and gas turbine parts (2007-12-11),

Title: Innovations of Keith Christopher Goldfinch

Introduction

Keith Christopher Goldfinch is a notable inventor based in Bristol, GB. He has made significant contributions to the field of gas turbine engines, holding a total of 9 patents. His work focuses on enhancing the efficiency and functionality of fan systems within these engines.

Latest Patents

Goldfinch's latest patents include a fan design that features fan blades with a U-shaped slot having a decreased length planar section. This innovative fan is specifically designed for gas turbine engines and includes a hub with an annular array of fan blades that extend radially outward. Each fan blade is equipped with a blade root that fits into hub grooves, ensuring a secure and efficient operation. Additionally, he has developed a method for forming an aerofoil with a damping filler, which involves creating an internal cavity between two panels and incorporating a pattern of ribs to enhance the structural integrity of the aerofoil.

Career Highlights

Goldfinch is currently employed at Rolls-Royce Corporation, where he continues to push the boundaries of engineering and design in the aerospace sector. His innovative approaches have garnered attention and respect within the industry.

Collaborations

Some of his notable coworkers include Oliver Michael Strother and Julian MacKechnie-Jarvis, who have collaborated with him on various projects, contributing to the advancement of technology in gas turbine engines.

Conclusion

Keith Christopher Goldfinch's contributions to the field of gas turbine engines through his patents and innovative designs highlight his expertise and commitment to engineering excellence. His work continues to influence the industry and pave the way for future advancements.