DRIVE-IN DEVICE HAVING AN ADJUSTABLE COMBUSTION CHAMBER
20170341210 · 2017-11-30
Inventors
- Peter STAUSS-REINER (Feldkirch, AT)
- Norbert Heeb (Buchs, CH)
- Thomas Sperrfechter (Grüsch, CH)
- Markus Woerner (Hergensweiler, DE)
- Tilo DITTRICH (Feldkirch, AT)
Cpc classification
International classification
Abstract
The invention relates to a drive-in device, comprising a drive-in piston, guided in a cylinder, for driving a nail member into a workpiece, and a combustion chamber arranged above the drive-in piston, said combustion chamber being Tillable with a combustion gas, wherein the combustion chamber has a bottom that is adjustable along an axis, wherein the bottom has a groove that extends in the circumferential direction and has an inserted seal which bears in a radial direction against a rigid combustion-chamber wall, wherein a front surface, in the axial direction, of the seal protrudes in the direction of the axis from a terminating plane of the groove.
Claims
1. A drive-in tool, comprising a drive-in piston which is guided in a cylinder for driving a nail member into a workpiece, and a combustion chamber which is arranged over the drive-in piston and which can be filled with a combustion gas, wherein the combustion chamber has a cylindrical combustion chamber wall and a bottom that is adjustable with respect to the combustion chamber wall along an axis, wherein the bottom has a groove running in a circumferential direction and having a seal that rests against the combustion chamber wall in a radial direction, the groove, having a terminating plane and the seal having a front surface in an axial direction protruding in the direction of the axis in front of the terminating plane of the groove.
2. The drive-in tool according to claim 1, wherein the front surface of the seal protrudes over a terminating plane of the bottom in the direction of the axis.
3. The drive-in tool according to claim 1, wherein the front surface of the seal has a radially inner end having a sharp-edged termination.
4. The drive-in tool according to claim 1, including a recess for discharging water wiped off by the seal arranged on the combustion chamber bottom and/or in a region of the combustion chamber.
5. The drive-in tool according to claim 1, wherein the seal protrudes on both sides over the terminating plane of the groove.
6. The drive-in tool according to claim 1, wherein the seal comprises a sealing ring that is open in the circumferential direction.
7. The drive-in tool according to claim 6, wherein the sealing ring comprises a hard sealant.
8. The drive-in tool according to claim 6, wherein the seal comprises at least two sealing rings arranged successively in the axial direction.
9. The drive-in tool according to claim 6, further comprising an elastic support member arranged under the sealing ring.
10. The drive-in tool according to claim 1, wherein the drive-in tool comprises a housing and the combustion chamber wall is rigidly connected to the housing.
11. The drive-in tool according to claim 1, wherein the drive-in tool comprises a housing and the bottom is rigidly connected to the housing.
12. The drive-in tool according to claim 1, wherein the bottom is adjustable relative to the combustion chamber wall to such an extent as to form an inlet and/or outlet opening of the combustion chamber between the bottom and the combustion chamber wall.
13. The drive-in tool according to claim 3, wherein the sharp-edged termination comprises an edge having an angle between 30° and 120°.
14. The drive in tool according to claim 8, wherein the at least two sealing rings have been inserted into the groove.
15. The drive-in tool according to claim 2, wherein the front surface of the seal has a radially inner end having a sharp-edged termination.
16. The drive-in tool according to claim 2, including a recess for discharging water wiped off by the seal arranged on the combustion chamber bottom and/or in a region of the combustion chamber.
17. The drive-in tool according to claim 3, including a recess for discharging water wiped off by the seal arranged on the combustion chamber bottom and/or in a region of the combustion chamber.
18. The drive-in tool according to claim 2, wherein the seal protrudes on both sides over the terminating plane of the groove.
19. The drive-in tool according to claim 3, wherein the seal protrudes on both sides over the terminating plane of the groove.
20. The drive-in tool according to claim 4, wherein the seal protrudes on both sides over the terminating plane of the groove.
Description
[0016] A preferred embodiment of the present invention shall be described hereinbelow and set forth in greater detail with reference to the accompanying drawings.
[0017]
[0018]
[0019]
[0020] The drive-in tool from
[0021] A bottom 7 of the combustion chamber 1 can be moved along an axis coinciding with the drive-in direction, such that the volume of the combustion chamber is variable. The bottom 7 is sealed off for this purpose with a circumferential seal 8 from the cylindrical combustion chamber wall 2. The seal 8 is depicted only schematically in
[0022] In embodiments that are not shown, the bottom is rigidly connected to the housing, and the combustion chamber wall is configured as an axially movable sheath. In embodiments that also are not shown, the combustion chamber wall is adjustable relative to the bottom to such an extent as to form an inlet and/or outlet opening of the combustion chamber for air and/or fuel between the bottom and the combustion chamber wall.
[0023] The bottom 7 can be moved via an adjusting rod 9 in the direction of the axis, wherein the adjusting rod 9 penetrates through a leadthrough in a front second bottom of the combustion chamber. The pressing of the attachment sheath 5 first tensions a spring and acts on the adjusting rod 9, which in turn displaces the bottom 7. This first tensions a volume of the combustion chamber that is sufficient for an ignition. Upon this movement of the bottom along the combustion chamber wall, regularly condensed water is wiped off. To prevent stiffness of the mechanism, as little water as possible should penetrate into the region of the seal 8 and freeze. For this purpose, the bottom 7, the combustion chamber 1, and the seal 8 have special embodiments that shall be described hereinbelow.
[0024] The seal 8 is configured as a set of two sealing rings 10, 11 lying directly against one another in the axial direction. Both sealing rings 10, 11 are accommodated in the same groove 12 on an outer circumferential wall 7a of the bottom 7. The sealing rings 10, 11 are composed of a hard material, in this case steel. The sealing rings 10, 11 each have an open abutment 13, in order to be able to be inserted into the groove 12. The abutment also allows for a defined pressing of the sealing rings against the combustion chamber wall. For this purpose, an elastic support member 14 in the groove is arranged below the sealing rings. When the sealing rings 10, 11 have been inserted, the support member 14 is pressed in in the radial direction, and resiliently subjected to force. The abutments 13 of the sealing rings 10, 11 are oriented at an offset to one another in the circumferential direction. In the depiction according to
[0025] The sealing rings 10, 11 have in this case each an L-shaped cross-section and are arranged with mirror symmetry to a midplane of the groove. In particular, the sealing rings 10, 11 may be formed as identical components. One leg of each L-shaped cross-section engages with the groove 12. The other leg extends in the axial direction in the gap 15 between the circumferential wall 7a of the bottom 7 and the combustion chamber wall 2. A respective front surface 10a, 11a of the sealing rings 10, 11 that is to the front in the axial direction protrudes in each case in front of a terminating plane E1, E2 of the groove 12. In particular, the front surface 10a, 11a protrudes in the axial direction also in front of a respective terminating plane A1, A2 of the bottom 2. A respective radially inner end of the front surfaces 10a, 11a has a sharp-edged termination 10b, 11b in the form of an edge having an angle of 90°. The edge lies then in each case in front of the terminating plane A1, A2 of the bottom 2. A radius of curvature of the edge is preferably less than 0.5 mm, in particular, less than 0.2 mm.
[0026] In order to better discharge the water wiped off by the movement of the bottom, and prevent water from building up in addition to penetration into the gap 15, a recess 16 is provided on the bottom 7. The recess 16 is formed as an annular space that remains between the bottom 7 and a stop ring 17. When the combustion chamber is fully expanded, the bottom 7 is supported on the stop ring 17. Through openings 18, the wiped-off water can additionally flow past the stop ring 17 into other housing regions.