CYLINDER DRUM OF A HYDROSTATIC AXIAL PISTON MACHINE HAVING A WEAR-RESISTANT LAYER
20170343107 · 2017-11-30
Inventors
Cpc classification
F05C2251/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05C2203/0813
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B1/143
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B53/166
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16J10/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C23C8/34
CHEMISTRY; METALLURGY
F04B53/162
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16J10/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B1/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B1/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A method is provided for forming wear-resistant layer on the surface of cylinder bores a cylinder drum of a hydrostatic axial piston machine within which a respective piston is moved in a manner subject to intensive wear. The cylinder bores are gas nitrocarburized in two stages to minimize the wear and include a thin uniform connecting layer that has a thickness of 4 to 16 μm and a comparatively thick underlying diffusion layer.
Claims
1. A method of forming a wear-resistant layer on the surface of a cylinder bore within a cylinder drum of a hydrostatic axial piston machine, the method comprising gas nitrocarburizing the surface of the cylinder bore in two stages: the first stage forming an oxide layer and a diffusion layer at the surface separated by a ductile connecting layer that is comparatively thin relative to the diffusion layer, the first stage comprising gas nitrocarburizing at a comparatively low treatment temperature and a comparatively long treatment duration; and the second stage comprising further gas nitrocarburizing while increasing the carbon content of the connecting layer by the addition of carbon donors at a comparatively high treatment temperature relative to the first stage.
2. The method according to claim 1, wherein the connecting layer is formed with a thickness of 4 to 16 μm.
3. The method according to claim 2, wherein the connecting layer is formed with a thickness of 5 to 12 μm.
4. The method according to claim 1, wherein the diffusion layer is formed with a thickness of at least 50 μm.
5. The method according to claim 1, wherein the comparatively low temperature of the first stage is 500 to 510° C.
6. The method according to claim 5, wherein the comparatively high treatment temperature of the second stage is greater than 500° C.
7. The method according to claim 1, further comprising adding during the gas nitrocarburizing stages more nitrogen than in an undersaturated furnace atmosphere.
8. The method according to claim 7, wherein the step of adding nitrogen includes adding during the gas nitrocarburizing stages less nitrogen than in a supersaturated furnace atmosphere.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0020] An exemplary embodiment according to the disclosure of a cylinder drum is shown in the drawings. The disclosure will now be explained in more detail with reference to the figures in the drawings, in which:
[0021]
[0022]
DETAILED DESCRIPTION
[0023]
[0024]
[0025] With reference to
[0026] According to the disclosure, the cylinder drum 1 shown in
[0027] The disclosure discloses a cylinder drum of a hydrostatic axial piston machine, wherein a plurality of cylinder bores, in each of which a piston is moved in a manner subject to intensive wear, are introduced into the cylinder drum. The cylinder bores of the cylinder drum are nitrocarburized in a salt bath or in gas to minimize the wear, a thin uniform connecting layer having a thickness of 4 to 16 μm and a comparatively thick underlying diffusion layer being provided.
LIST OF REFERENCE SIGNS
[0028] 1 Cylinder drum
[0029] 2 Longitudinal axis
[0030] 4 End face
[0031] 6 End face
[0032] 8 Cylinder bore
[0033] 10 Through bore
[0034] DS Diffusion layer
[0035] OS Oxide layer
[0036] VS Connecting layer