Patents by Inventor Paul E. Harnisch

Paul E. Harnisch 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).

  • FAST-PIVOT MISSILE FLIGHT CONTROL SURFACE
    Publication number: 20080029642
    Abstract: Methods and apparatus are provided for a missile that includes a housing, a fin, and a first actuator. The housing has a slot formed therethrough. The fin is disposed within the housing proximate the slot. The first actuator is coupled to the fin and configured to selectively move the fin at least partially in and out of the housing through the slot.
    Type: Application
    Filed: February 25, 2005
    Publication date: February 7, 2008
    Inventors: Paul E. Harnisch, Robert E. Winkel
  • Fast-pivot missile flight control surface
    Patent number: 7325769
    Abstract: Methods and apparatus are provided for a missile that includes a housing, a fin, and a first actuator. The housing has a slot formed therethrough. The fin is disposed within the housing proximate the slot. The first actuator is coupled to the fin and configured to selectively move the fin at least partially in and out of the housing through the slot.
    Type: Grant
    Filed: February 25, 2005
    Date of Patent: February 5, 2008
    Assignee: Honeywell International, Inc.
    Inventors: Paul E. Harnisch, Robert E. Winkel