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For the Inventor, By the Inventor

Derby, United Kingdom

Adam MacGregor Bagnall

USPTO Granted Patents = 14 

Average Co-Inventor Count = 1.4

ph-index = 8

Forward Citations = 170(Granted Patents)


Location History:

  • Derbyshire, GB (2012 - 2014)
  • Alderwasley, GB (2014)
  • Belper, GB (2015)
  • Derby, GB (1990 - 2019)

Company Filing History:

goldMedal14 out of 5,871 
 
Rolls-royce Corporation
 patents

Years Active: 1990-2019

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14 patents (USPTO):Explore Patents
1. 10240536 - Fluid system (2019-03-26),
2. 10190501 - Gas turbines engine support structures (2019-01-29),
3. 9752593 - Method of manufacturing a gas turbine engine having a fan track liner with an abradable layer (2017-09-05),
4. 9091174 - Method of reducing asymmetric fluid flow effects in a passage (2015-07-28),
5. 8821115 - Seal assembly (2014-09-02),
6. 8734088 - Variable stator vane (2014-05-27),
7. 8529204 - Gas turbine engine having a nose cone assembly rigidly attached in an axial direction but flexible in a radial direction (2013-09-10),
8. 8206079 - Temperature controlling apparatus (2012-06-26),
9. 7200999 - Arrangement for bleeding the boundary layer from an aircraft engine (2007-04-10),
10. 7014145 - Variable position intake for an aircraft mounted gas turbine engine (2006-03-21),
11. 6945494 - Variable position intake for an aircraft mounted gas turbine engine (2005-09-20),
12. 6722847 - Fan for a turbofan gas turbine engine (2004-04-20),
13. 6447255 - Gas turbine nose cone assembly (2002-09-10),
14. 4964844 - Gearbox arrangement for driving coaxial contra rotating multi-bladed (1990-10-23),

Title: Adam MacGregor Bagnall: Innovator in Gas Turbine Technology

Introduction

Adam MacGregor Bagnall, based in Derby, Great Britain, is a prominent inventor known for his contributions to gas turbine technology. With a total of 14 patents to his name, Bagnall has made significant advancements in the design and functionality of gas turbine engines.

Latest Patents

Some of Bagnall's latest patents include innovative designs that enhance the efficiency and performance of gas turbine engines. One noteworthy invention is a fluid system that incorporates a bifurcation fairing within a bypass duct of the gas turbine engine. This design features a delivery conduit that is specifically arranged for the effective delivery of bypass air to various components of the engine. Additionally, he holds a patent for gas turbine engine support structures, which includes a ducted fan gas turbine engine equipped with a propulsive fan and a series of support structures designed to efficiently transmit loads from the core engine to the fan case.

Career Highlights

Bagnall currently works at Rolls-Royce Corporation, an industry leader in aerospace and advanced engineering. His work focuses on enhancing gas turbine technologies that have wide applications in both civilian and military aviation sectors. The innovative solutions he has developed have significantly contributed to the efficiency and reliability of modern gas turbine engines.

Collaborations

Throughout his career, Adam Bagnall has collaborated with notable professionals such as Christopher Freeman and Clive Lockwood. These partnerships have played a critical role in driving forward innovative projects and solutions within the realm of gas turbine technology.

Conclusion

In conclusion, Adam MacGregor Bagnall stands out as a key figure in the field of gas turbine innovation. His expertise and numerous patents reflect a deep commitment to advancing technology within this sector. As he continues to collaborate with industry experts, Bagnall’s work will undoubtedly lead to further breakthroughs in gas turbine engine design and performance.

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