Fuel and propellant composition for combustion tools
US-2016244684-A1 · Aug 25, 2016 · US
US9676089B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9676089-B2 |
| Application number | US-32133909-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 15, 2009 |
| Priority date | Jan 29, 2008 |
| Publication date | Jun 13, 2017 |
| Grant date | Jun 13, 2017 |
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A combustion-operated setting tool ( 10 ) for driving-in fastening elements includes a setting piston ( 14 ) displaceable in a guide cylinder ( 13 ), a combustion chamber ( 15 ), a fuel inlet ( 23 ) opening into the combustion chamber ( 15 ) for feeding fuel therein and an ignition element ( 26 ) for igniting the fuel in the combustion chamber ( 15 ). Both, the fuel inlet ( 23 ) and the ignition element ( 26 ), are located at the first end ( 31 ) of the combustion chamber ( 15 ) adjacent to the guide cylinder ( 13 ), and a motor-driven ventilator ( 16 ) supported on a rear wall ( 30 ) of the combustion chamber ( 15 ) at the second end ( 32 ) of the combustion chamber ( 15 ) remote from the guide cylinder ( 13 ).
Opening claim text (preview).
What is claimed is: 1. A combustion-operated setting tool ( 10 ) for driving in fastening elements, comprising: a guide cylinder ( 13 ); a setting piston ( 14 ) displaceable in the guide cylinder ( 13 ); a combustion chamber ( 15 ) bordering the guide cylinder, defining a combustion chamber axis (A) and having a first axial end ( 31 ) adjacent to the guide cylinder ( 13 ) and a second axial end ( 32 ) spaced from the guide cylinder ( 13 ); a fuel inlet ( 23 ) opening into the combustion chamber ( 15 ) substantially parallel to the axis of the combustion chamber for feeding fuel therein and located at the first end surface ( 31 ) of the combustion chamber ( 15 ); an ignition element ( 26 ) for igniting the fuel in the combustion chamber ( 15 ) and likewise located at the first end surface ( 31 ) of the combustion chamber ( 15 ); a ventilator ( 16 ) located in the combustion chamber ( 15 ) and supported on a rear wall ( 30 ) of the combustion chamber ( 15 ) at the second end ( 32 ) thereof; and a motor ( 17 ) for driving the ventilator ( 16 ). 2. A combustion-operated setting tool ( 10 ) according to claim 1 , wherein the fuel inlet ( 23 ) and the ignition element ( 26 ) lie on radii (R 1 , R 2 ) with respect to the combustion chamber axis (A) extending at an angle (α) to each other and that lies in a range from 5° to 180°. 3. A combustion-operated setting tool ( 10 ) according to claim 1 , wherein the ignition element ( 26 ) is located behind the fuel inlet ( 23 ) in a rotational direction ( 40 ) of the ventilator ( 16 ). 4. A combustion-operated setting tool ( 10 ) according to claim 1 , further comprising a fuel conduit ( 22 ) for connecting the fuel inlet ( 23 ) with a fuel reservoir. 5. A combustion-operated setting tool ( 10 ) according to claim 1 , wherein the fuel inlet ( 23 ) is located in a flow direction(s) of a flow generated by the ventilator ( 16 ). 6. A combustion-operated setting tool ( 10 ) according to claim 1 , wherein the ignition element ( 26 ) located in a flow direction(s) of a flow generated by the ventilator ( 16 ). 7. A combustion-operated setting tool ( 10 ) according to claim 1 wherein the ignition element ( 26 ) is located in a flow direction(s) of a flow generated by the ventilator ( 16 ). 8. A combustion-operated setting tool ( 10 ) for driving in fastening elements, comprising: a guide cylinder ( 13 ); a setting piston ( 14 ) displaceable in the guide cylinder ( 13 ); a combustion chamber ( 15 ) defining a combustion chamber axis (A) and having a front wall ( 29 ) adjacent to the setting piston ( 14 ) and a rear wall ( 30 ) spaced from the setting piston ( 14 ); a fuel inlet ( 23 ) opening into the combustion chamber ( 15 ) for feeding fuel therein and located in the front surface of the combustion chamber ( 15 ); an ignition element ( 26 ) for igniting the fuel in the combustion chamber ( 15 ) and secured in the front surface of the combustion chamber ( 15 ); a ventilator ( 16 ) supported on the rear wall ( 30 ) of the combustion chamber ( 15 ); and a motor ( 17 ) for driving the ventilator ( 16 ). 9. A combustion-operated setting tool ( 10 ) according to claim 8 , wherein the fuel inlet ( 23 ) and the ignition element ( 26 ) lie on radii (R 1 , R 2 ) with respect to the combustion chamber axis (A) extending at an angle (a) to each other and that lies in a range from 5° to 180°. 10. A combustion-operated setting tool ( 10 ) according to claim 8 , wherein the ignition element ( 26 ) is located behind the fuel inlet ( 23 ) in a rotational direction ( 40 ) of the ventilator ( 16 ). 11. A combustion-operated setting tool ( 10 ) according to claim 8 , further comprising a fuel conduit ( 22 ) for connecting the fuel inlet ( 23 ) with a fuel reservoir. 12. A combustion-operated setting tool ( 10 ) according to claim 8 , wherein the ventilator ( 16 ) is located in the combustion chamber ( 15 ). 13. A combustion-operated setting tool ( 10 ) according to claim 8 , wherein the fuel inlet ( 23 ) is located in a flow direction(s) of a flow generated by the ventilator ( 16 ). 14. A combustion-operated setting tool according to claim 8 , wherein the fuel inlet ( 23 ) opens into the combustion chamber ( 15 ) substantially axially.
operated by combustion pressure · CPC title
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