Tokyo, Japan

Osamu Ueda

USPTO Granted Patents = 4 

 

Average Co-Inventor Count = 2.2

ph-index = 2

Forward Citations = 14(Granted Patents)


Location History:

  • Hyogo, JP (2014)
  • Tokyo, JP (2000 - 2015)

Company Filing History:


Years Active: 2000-2015

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4 patents (USPTO):Explore Patents

Title: The Innovative Contributions of Osamu Ueda

Introduction

Osamu Ueda is a notable inventor based in Tokyo, Japan. He has made significant contributions to the field of turbine technology, holding a total of 4 patents. His work focuses on enhancing the efficiency and functionality of turbine blades and gas turbines.

Latest Patents

Ueda's latest patents include innovative designs for turbine rotor blades and gas turbines. One of his patents describes a turbine rotor blade featuring a concave relief portion along the circumferential direction of the rotor. This design includes a cooling channel opening in the trailing-edge end surface, which is thicker in the radial direction at the cooling channel opening compared to the trailing-edge end of the hub. Another patent outlines turbine blades and a gas turbine that effectively dampen vibrations caused by excitation forces. This design incorporates a shroud portion at the end of the airfoil, a holder casing that can slide and detach, and an elastic portion that biases the shroud away from the holder casing.

Career Highlights

Throughout his career, Ueda has worked with prominent companies such as Mitsubishi Heavy Industries Limited and Clarion Co. His experience in these organizations has allowed him to develop and refine his innovative ideas in turbine technology.

Collaborations

Ueda has collaborated with notable coworkers, including Hiroyuki Hamana and Naoyuki Seki. Their combined expertise has contributed to the advancement of turbine technology and the successful development of Ueda's patents.

Conclusion

Osamu Ueda's contributions to turbine technology through his innovative patents demonstrate his significant impact on the field. His work continues to influence advancements in turbine design and functionality.

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