Derby, United Kingdom

Marc Pons Perez


 

Average Co-Inventor Count = 2.3

ph-index = 2

Forward Citations = 27(Granted Patents)


Location History:

  • Barcelona, ES (2013)
  • Derby, GB (2014 - 2017)

Company Filing History:


Years Active: 2013-2017

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3 patents (USPTO):Explore Patents

Title: The Innovations of Marc Pons Perez

Introduction

Marc Pons Perez is a notable inventor based in Derby, GB. He has made significant contributions to the field of gas turbine technology, holding a total of 3 patents. His work focuses on enhancing the efficiency and performance of gas turbine engines.

Latest Patents

One of Marc's latest patents is for a gas turbine cowl. This invention comprises a rear cowl that defines an exhaust aperture and includes a motive system. The rear cowl features at least one panel that can be selectively moved between deployed and stowed configurations. This movement alters the area of the exhaust aperture, optimizing engine performance.

Another significant patent is for a gas turbine engine compressor variable stator vane arrangement. This arrangement includes a stage of variable stator vanes, with various sensors measuring the compressor's operational parameters. A processor determines a target operating line to ensure the gas turbine engine operates efficiently, minimizing idle thrust and fuel burn. The processor adjusts the angle of the variable stator vanes to maintain optimal performance.

Career Highlights

Marc Pons Perez is currently employed at Rolls-Royce Corporation, a leading company in aerospace and defense. His work at Rolls-Royce has allowed him to develop innovative solutions that enhance gas turbine engine technology.

Collaborations

Marc has collaborated with talented coworkers such as Julien N E Calvignac and Arthur Laurence Rowe. Their combined expertise contributes to the advancement of technology within their field.

Conclusion

Marc Pons Perez is a distinguished inventor whose work in gas turbine technology has led to several important patents. His contributions continue to influence the efficiency and performance of gas turbine engines.

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