Patents by Inventor Thomas Leidenberger

Thomas Leidenberger 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: 10746503
    Abstract: A launcher device for launching ammunition or weapons provided with primers, contains a plurality of launch tubes combined so as to form a launcher battery. Each of the launch tubes is loaded with ammunition or a weapon, and each of the launch tubes is closed off by a cover. A device is provided for detecting damage to the covers closing off the launch tubes.
    Type: Grant
    Filed: May 17, 2019
    Date of Patent: August 18, 2020
    Assignee: Diehl Defence GmbH & Co. KG
    Inventors: Markus Bittner, Thomas Leidenberger
  • Publication number: 20190353453
    Abstract: A launcher device for launching ammunition or weapons provided with primers, contains a plurality of launch tubes combined so as to form a launcher battery. Each of the launch tubes is loaded with ammunition or a weapon, and each of the launch tubes is closed off by a cover. A device is provided for detecting damage to the covers closing off the launch tubes.
    Type: Application
    Filed: May 17, 2019
    Publication date: November 21, 2019
    Inventors: MARKUS BITTNER, THOMAS LEIDENBERGER
  • Patent number: 6769643
    Abstract: A projectile (12) to be fired from a rifled barrel (66) is described. At its tail (10) it has control surface vanes (14) which can be pivoted out from a sub-calibre launch position into an over-calibre functional position. To protect the inwardly folded vanes (14) and to protect further ballistic and sensor structures at the tail end of the projectile (12), a securing pot (18) is temporarily fixed to the tail (10) of the projectile (12), the securing pot having a pot peripheral portion (22) and a pot bottom (24). There is a pressure chamber (32) between the tail end face (26) of the projectile (12) and the pot bottom (24) of the securing pot (18). The pot bottom (24) has at least one propellent gas inlet (34) which opens into the pressure chamber (32). When the projectile (12) is fired from the barrel propellent gas flows through the propellent gas inlet (34) into the pressure chamber (32) so that a correspondingly high propellent gas pressure is produced in the pressure chamber (32).
    Type: Grant
    Filed: December 10, 2002
    Date of Patent: August 3, 2004
    Assignee: Diehl Munitionssysteme GmbH & Co. KG
    Inventors: Klaus Bär, Jürgen Bohl, Thomas Leidenberger
  • Publication number: 20040004156
    Abstract: A projectile (12) to be fired from a rifled barrel (66) is described. At its tail (10) it has control surface vanes (14) which can be pivoted out from a sub-calibre launch position into an over-calibre functional position. To protect the inwardly folded vanes (14) and to protect further ballistic and sensor structures at the tail end of the projectile (12), a securing pot (18) is temporarily fixed to the tail (10) of the projectile (12), the securing pot having a pot peripheral portion (22) and a pot bottom (24). There is a pressure chamber (32) between the tail end face (26) of the projectile (12) and the pot bottom (24) of the securing pot (18). The pot bottom (24) has at least one propellent gas inlet (34) which opens into the pressure chamber (32). When the projectile (12) is fired from the barrel propellent gas flows through the propellent gas inlet (34) into the pressure chamber (32) so that a correspondingly high propellent gas pressure is produced in the pressure chamber (32).
    Type: Application
    Filed: December 10, 2002
    Publication date: January 8, 2004
    Applicant: Diehl Munitionssysteme GmbH & Co. KG
    Inventors: Klaus Bar, Jurgen Bohl, Thomas Leidenberger
  • Patent number: 5211357
    Abstract: An airborne body possessing stabilizing fins or control surfaces, wherein each stabilizing fin is displaceable about an associated bearing axle between a retracted inoperative position and a position of flight in which it is unfolded from the airborne body. An arrangement is associated with each stabilizing fin or control surface, which arrangement is provided for the damping or cushioning of the extending movement of the respective stabilizing fin from the inoperative position into the flying position and for the latching of the stabilizing fin in the flying position, while inhibiting and rebounding of the fin.
    Type: Grant
    Filed: June 11, 1992
    Date of Patent: May 18, 1993
    Assignee: Diehl GmbH & Co.
    Inventor: Thomas Leidenberger
  • Patent number: 5114095
    Abstract: An arrangement for the unlatching and extension of the stabilizing fins or control surfaces of a projectile, including a power element which is effective in the longitudinal direction of the projectile for pressing a follower against camming or runoff edges located proximate hinged connections at the fin footings, after a latching for the stabilizing fin in the region of their end surfaces has been released. The power element causes a latching crown or ring to be raised away from the end surfaces of the stabilizing fins opposite the force of a spring through the longitudinal movement of a connecting or pusher rod prior to the pusher rod engaging behind the follower and then pressing against the runoff or camming edges.
    Type: Grant
    Filed: June 19, 1991
    Date of Patent: May 19, 1992
    Assignee: Diehl GmbH & Co.
    Inventors: Werner Schroppel, Thomas Leidenberger