Patents by Inventor Francis Deazley

Francis Deazley 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).

  • Patent number: 8070104
    Abstract: A releasable deployment line for a parachute system is provided. The releasable deployment line may include a first segment of material including an aircraft end configured to be operably connected to an aircraft, and a release end configured to be operably connected to a first section of a multi-ring release system. The replaceable deployment line may further include a second segment of material including a container end configured to be operably connected to a parachute container, and a ring end configured to be operably connected to a second section of the multi-ring release system and a third segment of material. The third segment of material may include a parachute end configured to be operably connected to a parachute within the parachute container, and a pin end configured to be operably connected to a retaining pin associated with the first section of the multi-ring release system.
    Type: Grant
    Filed: March 4, 2011
    Date of Patent: December 6, 2011
    Assignee: Strong Enterprises
    Inventor: Francis Deazley
  • Publication number: 20110155857
    Abstract: A releasable deployment line for a parachute system is provided. The releasable deployment line may include a first segment of material including an aircraft end configured to be operably connected to an aircraft, and a release end configured to be operably connected to a first section of a multi-ring release system. The replaceable deployment line may further include a second segment of material including a container end configured to be operably connected to a parachute container, and a ring end configured to be operably connected to a second section of the multi-ring release system and a third segment of material. The third segment of material may include a parachute end configured to be operably connected to a parachute within the parachute container, and a pin end configured to be operably connected to a retaining pin associated with the first section of the multi-ring release system.
    Type: Application
    Filed: March 4, 2011
    Publication date: June 30, 2011
    Inventor: Francis DEAZLEY
  • Patent number: 7922123
    Abstract: A releasable deployment line for a parachute system is provided. The releasable deployment line may include a first segment of material including an aircraft end configured to be operably connected to an aircraft, and a release end configured to be operably connected to a first section of a multi-ring release system. The replaceable deployment line may further include a second segment of material including a container end configured to be operably connected to a parachute container, and a ring end configured to be operably connected to a second section of the multi-ring release system and a third segment of material. The third segment of material may include a parachute end configured to be operably connected to a parachute within the parachute container, and a pin end configured to be operably connected to a retaining pin associated with the first section of the multi-ring release system.
    Type: Grant
    Filed: July 31, 2007
    Date of Patent: April 12, 2011
    Assignee: Strong Enterprises
    Inventor: Francis Deazley
  • Publication number: 20090294594
    Abstract: A releasable deployment line for a parachute system is provided. The releasable deployment line may include a first segment of material including an aircraft end configured to be operably connected to an aircraft, and a release end configured to be operably connected to a first section of a multi-ring release system. The replaceable deployment line may further include a second segment of material including a container end configured to be operably connected to a parachute container, and a ring end configured to be operably connected to a second section of the multi-ring release system and a third segment of material. The third segment of material may include a parachute end configured to be operably connected to a parachute within the parachute container, and a pin end configured to be operably connected to a retaining pin associated with the first section of the multi-ring release system.
    Type: Application
    Filed: July 31, 2007
    Publication date: December 3, 2009
    Inventor: Francis Deazley