Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
174 words
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.
Claim 2
Dependent Claim
174 words
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.
Claim 3
Dependent Claim
35 words
A setting tool, as set forth in claim 1, wherein at least two said Laval nozzles are provided each arranged for flowing explosive gas from said combustion chamber to the rear end of said bore.
Claim 4
Dependent Claim
27 words
A setting tool, as set forth in claim 2, wherein the at least two said Laval nozzles are offset radially outwardly from the axis of said bore.
Claim 5
Dependent Claim
40 words
A setting tool, as set forth in claim 1, wherein said member forms a mixing chamber located between said combustion chamber and the rear end of said bore with flow channels communicating between said combustion chamber and said mixing chamber.
Claim 6
Dependent Claim
27 words
A setting tool, as set forth in claim 4, wherein said flow channels between said combustion chamber and said mixing chamber are of constant transverse cross section.
Claim 7
Dependent Claim
25 words
A setting tool, as set forth in claim 4, wherein said Laval nozzle extends between said mixing chamber and the rear end of said bore.
Claim 8
Dependent Claim
24 words
A setting tool, as set forth in claim 1, wherein said member comprises a replaceable insert and said Laval nozzle formed in said insert.
Claim 9
Dependent Claim
43 words
A setting tool, as set forth in claim 1, wherein means are positioned in said member for limiting the rearward position of said drive piston relative to the rear end of said bore so that an axially extending working chamber is formed therebetween.
Claim 10
Dependent Claim
72 words
A setting tool, as set forth in claim 8, wherein said means comprises a rod movably adjustable in the axial direction of said bore and extending into said bore for limiting the rearward position of said drive piston relative to the rearward end of said bore so that the axial dimension of said working chamber can be varied in accordance with the axial extent to which said rod extends into said bore.
Claim 11
Dependent Claim
82 words
A setting tool, as set forth in claim 1, wherein said combustion chamber being coaxial with the said bore, and said firing pin disposed in axial alignment with said combustion chamber and said member providing a bearing surface on the opposite side of said combustion chamber from said firing pin disposed transversely of the axis of said combustion chamber for forming a countersupport surface for the propellant charge within said combustion chamber when said firing pin is displaced against the propellant charge.
Claim 12
Dependent Claim
50 words
A setting tool, as set forth in claim 1, wherein said member comprises a barrel forming said bore and a breech member removably positionable in the end of said barrel adjacent the rearward end of said bore and said breech mechanism in combination with said barrel forming said combustion chamber.