Setting tool containing a laval nozzle
AssigneeHilti Aktiengesellschaft
InventorRalph Scotoni
Life of this patent
Estimating the term…
Loading patent…
AssigneeHilti Aktiengesellschaft
InventorRalph Scotoni
Estimating the term…
In a setting tool using explosive caseless propellant charges for driving fastening elements into a hard target material, a combustion chamber for the charges is located rearwardly of the rear end of the bore in the setting tool through which a drive piston is displaceable for inserting the fastening elements. The combustion chamber is in communication with the rear end of the bore through at least one Laval nozzle. A mixing chamber can be located between the combustion chamber and the rear end of the bore with constant cross section flow channels located between the combustion chamber and the mixing chamber and with the Laval nozzle extending between the mixing chamber and the rear end of the bore. The rear end of the drive piston can be selectively positioned relative to the rear end of the bore so that a working chamber of variable dimension in the axial direction of the bore is provided between the rear end of the piston and the rear end of the bore.
A setting tool employing an explosive caseless propellant charge for driving fastening elements into a hard target material, comprises a member forming an axially elongated bore having a rear end and a front end, said member forming a combustion chamber arranged to receive a caseless propellant charge and said combustion chamber located adjacent the rear end of said bore and on the opposite side of said rear end from the front end thereof, said member forming at least one gas flow channel communicating between said combustion chamber and the rear end of said bore, a drive piston movably displaceable through said bore from the rear end toward the front end thereof under the action of an exploded propellant charge and said drive piston being movably displaceable toward the rear end of the bore after the insertion of a fastening element, wherein the improvement comprises that said gas flow channel is a Laval nozzle, and an axially extending firing pin located within said member rearwardly of said combustion chamber for igniting a propellant charge therein.
Dependencies are inferred from the claim text.