Patents by Inventor Luis Frederico Puerta

Luis Frederico Puerta has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Airfoil for a compressor blade
    Patent number: 9291059
    Abstract: The present disclosure provides an improved first stage airfoil for a compressor blade having a unique chord length (CD), stagger angle (?) and camber angle (??). The stagger angle (?) and camber angle (??) provide improved aerodynamics while the chord length (CD) provides for reduced airfoil weight.
    Type: Grant
    Filed: December 23, 2009
    Date of Patent: March 22, 2016
    Assignee: ALSTOM TECHNOLOGY LTD.
    Inventors: Marco Micheli, Gabriel Dunkel, Luis Frederico Puerta, Wolfgang Kappis
  • Airfoil for a compressor blade
    Patent number: 8523531
    Abstract: An improved second stage airfoil for a compressor blade having a unique chord length (CD), a stagger angle (?), and camber angle (??). The stagger angle (?) and camber angle (??) provide improved aerodynamics while the chord length (CD) provides for reduced airfoil weight.
    Type: Grant
    Filed: December 23, 2009
    Date of Patent: September 3, 2013
    Assignee: ALSTOM Technology Ltd
    Inventors: Marco Micheli, Luis Frederico Puerta, Wolfgang Kappis
  • AIRFOIL FOR A COMPRESSOR BLADE
    Publication number: 20110150660
    Abstract: The present disclosure provides an improved first stage airfoil for a compressor blade having a unique chord length (CD), stagger angle (?) and camber angle (??). The stagger angle (?) and camber angle (??) provide improved aerodynamics while the chord length (CD) provides for reduced airfoil weight.
    Type: Application
    Filed: December 23, 2009
    Publication date: June 23, 2011
    Applicant: ALSTOM Technology Ltd
    Inventors: Marco Micheli, Gabriel Dunkel, Luis Frederico Puerta, Wolfgang Kappis
  • AIRFOIL FOR A COMPRESSOR BLADE
    Publication number: 20110150659
    Abstract: The present disclosure provides an improved second stage airfoil for a compressor blade having a unique chord length (CD), a stagger angle (?), and camber angle (??). The stagger angle (?) and camber angle (??) provide improved aerodynamics while the chord length (CD) provides for reduced airfoil weight.
    Type: Application
    Filed: December 23, 2009
    Publication date: June 23, 2011
    Applicant: ALSTOM Technology Ltd
    Inventors: Marco Micheli, Luis Frederico Puerta, Wolfgang Kappis