Patents Assigned to Plasecki Aircraft Corporation
  • Feedback mechanism and circuit design for flight control boost actuators
    Publication number: 20210300526
    Abstract: Safer, redundant electromechanical flight control boost actuators for aircraft, having simple feedback mechanism independent of fly-by-wire systems are described herein. Said redundancy is achieved by two independent electric motors' systems and dual feedback mechanism.
    Type: Application
    Filed: May 4, 2020
    Publication date: September 30, 2021
    Applicant: Plasecki Aircraft Corporation
    Inventor: Luigi U. Ricci Moretti
  • Modular and morphable air vehicle
    Patent number: 10494092
    Abstract: A personal air vehicle may feature an air module that may be attached to a ground module. The air module may be equipped with exit vanes or vectored engine exhaust to provide redundant control effectors to the cyclic or collective pitch of at least one rotary wing under the control of a control system.
    Type: Grant
    Filed: April 14, 2018
    Date of Patent: December 3, 2019
    Assignee: Plasecki Aircraft Corporation
    Inventors: John W. Piasecki, Frederick W. Piasecki, Brian Geiger, Douglas Johnson, David Pitcairn