Hillsburgh, Canada

Nigel Caldwell Davenport

This inventor holds 25 USPTO granted patents and 3 published patent applications, plus 3 CIPO patents and 2 EPO patents, primarily in Gas Turbine Engineering. Top assignee: Pratt-Whitney Canada Corp. Active years: 2001-2024.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Nigel Caldwell Davenport. Retrieved from https://idiyas.com/inventor/nigel-caldwell-davenport

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

USPTO Granted Patents = 25 

% Patents Active = 96.0


 

Average Co-Inventor Count = 2.5

ph-index = 7

Forward Citations = 157(Granted Patents)


Location History:

  • Hillburgh, CA (2018)
  • Hillsburgh, CA (2001 - 2024)

Company Filing History:


Years Active: 2001-2024

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Areas of Expertise:
Gas Turbine Engine
Combustor Design
Heat Shield
Fuel Nozzle
Fluid Manifold
Rotary Internal Combustion
Laser-Ignition
Pilot Subchamber
Variable Premix-Lean Burn
Asymmetric Panels
Labyrinth Seal
Interlocking Panels
25 patents (USPTO):Explore Patents

Title: **Nigel Caldwell Davenport: Innovator in Gas Turbine Technology**

Introduction

Nigel Caldwell Davenport is a prominent inventor based in Hillburgh, California, renowned for his contributions to gas turbine technology. With an impressive portfolio of 25 patents, he has significantly advanced the efficiency and performance of combustors used in aircraft engines.

Latest Patents

Two of his latest patents reflect his innovative spirit and technical expertise. The first patent is a "Two-stage combustor for gas turbine engine," which features an inner and outer annular liner wall that together create a combustion chamber. This design includes a first dome wall with a series of fuel injection bores and a second dome wall with additional fuel injection points. The combustion process is divided into two stages, enhancing efficiency and performance in gas turbine operations.

Another notable patent is the "Heat shield labyrinth seal." This invention provides a novel sealing mechanism for a combustor heat shield against the interior surface of a combustor shell. The design incorporates first and second sealing surfaces featuring projections that create a non-linear leakage path, greatly improving the effectiveness of the sealing process.

Career Highlights

Nigel currently works at Pratt & Whitney Canada Corp., where he continues to push the boundaries of engineering in gas turbine technology. His innovative designs have not only contributed to the aerospace industry but have also positioned him as a leader in the field of propulsion systems.

Collaborations

Throughout his career, Nigel has collaborated with other talented engineers, including Eduardo David Hawie and Yen-Wen Wang. These partnerships have fostered a creative environment for innovation, enabling the development of groundbreaking technologies that significantly enhance engine performance.

Conclusion

In conclusion, Nigel Caldwell Davenport exemplifies the spirit of innovation in the aerospace sector. His 25 patents and the recent advancements he has made at Pratt & Whitney Canada Corp. demonstrate his dedication to improving gas turbine technology. Through collaboration and relentless pursuit of excellence, he continues to inspire future generations of inventors and engineers.

Profile summary based on public USPTO records.
Data Sources: USPTO Patent Grant XML, Patent Center, EPO & CIPO • Normalized by IDiyas Innovation Graph. Methodology & provenance architecturePlease report any incorrect information to [email protected]
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