Actuating Piston and Adjustment Installation
20210102559 ยท 2021-04-08
Inventors
Cpc classification
F15B15/1428
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B1/146
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B1/324
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03C1/0686
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B49/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B1/295
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
An actuating piston for a hydrostatic adjustment installation includes at least one sealing and guiding unit which is insertable into a circumferential recess of an actuating piston. The circumferential recess is composed of two regions, and has the effect of improving the guiding and sealing of the actuating piston. The actuating piston is arranged in an adjustment installation.
Claims
1. An actuating piston for a hydrostatic adjustment installation comprising: an external shell face defining a circumferential recess; and a sealing and guiding unit encompassing the external shell face in a region of the circumferential recess, the sealing and guiding unit configured to guide the actuating piston in an actuating cylinder of the hydrostatic adjustment installation so as to be stable in terms of tilting and displaceable in an axial manner, and to seal a gap between the external shell face of the actuating piston and an internal shell face of the actuating cylinder, wherein the circumferential recess has a first region having a guide region for the sealing and guiding unit that is configured to absorb transverse forces, and a second region having protrusions, and wherein the first region has a larger axial extent than the second region.
2. The actuating piston according to claim 1, wherein an axial extent of the guide region is larger by a multiple than an axial extent of the protrusions.
3. The actuating piston according to claim 1, wherein the sealing and guiding unit is configured so as to be integral.
4. The actuating piston according to claim 1, wherein the protrusions in the second region, when viewed in a direction of an axial force resulting from an actuating pressure, have a decreasing diameter.
5. The actuating piston according to claim 1, wherein the protrusions push at least partially into a circumference of the sealing and guiding unit so as to engage behind the sealing and guiding unit, and/or the protrusions plunge into recesses of the sealing and guiding unit.
6. The actuating piston according to claim 1, wherein the protrusions have end face portions that absorb axial forces acting on the sealing and guiding unit, the protrusions configured to seal a gap between the external shell face of the actuating piston and the internal shell face of the actuating cylinder.
7. The actuating piston according to claim 5, wherein the protrusions push into the sealing and guiding unit during the deformation under a transverse force and/or according to wear takes place by at least 40% of an initial thickness of the sealing and guiding unit in a region of a largest protrusion of the protrusions.
8. The actuating piston according to claim 1, wherein the sealing and guiding unit, upon being applied to the actuating piston, has a sealing diameter which is at most 0.5% larger than an internal diameter of the actuating cylinder.
9. The actuating piston according to claim 1, wherein a diameter in end portions of the circumferential recess is smaller than a diameter of a contact area of the guide region.
10. The actuating piston according to claim 9, wherein the sealing and guiding unit, by way of the end portions of the circumferential recess produces a gap, which is reduced because of internal stresses of the sealing and guiding unit, the sealing and guiding unit plunging at least partially into the gap such that a chamfer is provided on the sealing and guiding unit.
11. An adjustment installation comprising: an actuating cylinder; and an actuating piston comprising: an external shell face defining a circumferential recess; and a sealing and guiding unit encompassing the external shell face in a region of the circumferential recess, the sealing and guiding unit configured to guide the actuating piston in the actuating cylinder so as to be stable in terms of tilting and displaceable in an axial manner, and to seal a gap between the external shell face of the actuating piston and an internal shell face of the actuating cylinder, wherein the circumferential recess has a first region having a guide region for the sealing and guiding unit that is configured to absorb transverse forces, and a second region having protrusions, and wherein the first region has a larger axial extent than the second region.
12. The actuating piston according to claim 1, wherein the actuating piston is configured for adjusting a displacement volume of a hydrostatic positive-displacement machine having a variable displaced volume.
13. The actuating piston according to claim 7, wherein the protrusions push into the sealing and guiding unit during the deformation under the transverse force and/or according to wear by at most 55% of the initial thickness of the sealing and guiding unit in the region of the largest protrusion.
14. The actuating piston according to claim 13, wherein the protrusions push into the sealing and guiding unit during the deformation under the transverse force and/or according to wear by at least 42% and at most 50% of the initial thickness of the sealing and guiding unit in the region of the largest protrusion.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0028] The disclosure will be explained in more detail hereunder by means of an exemplary embodiment of an adjustment installation having an actuating piston.
[0029] In the figures:
[0030]
[0031]
[0032]
DETAILED DESCRIPTION
[0033]
[0034] The actuating piston 1 is guided so as to be displaceable along a longitudinal axis 19 in a main portion 3 of an actuating cylinder 1a configured with two functions, said actuating cylinder 1a being configured so as to be integral to a housing of the positive-displacement machine to be adjusted, or configured so as to be attachable to said housing. An end-side closure of the actuating cylinder 1a is formed by a cover 10.
[0035] A spring pack 5 is disposed in a spring chamber of the actuating piston 1 on a side of the actuating piston 1 (shown on the right in
[0036] The pressurized chamber 11 penetrated by the pin 7 is partially delimited by the cover 10 and, as mentioned above, in terms of the pressurizing medium is fluidically connected to the spring chamber of the actuating piston 1 in which the spring pack 5 is received, said pressurized chamber 11 herein being sealed in relation to a zone that is not impinged with pressure. The sealing and guiding unit 6 (on the right in
[0037] A support disk 13 and a support disk 15 are disposed so as to be displaceable on the pin 7 in the pressurized chamber 11, said support disk 13 and support disk 15 delimiting the spring pack 5. When the pressurized chamber 11 is impinged with an actuating pressure, the actuating piston 1 is moved by an axial force F.sub.A (to the left according to the illustration in
[0038] When the second pressurized chamber 21 is impinged with an actuating pressure, the actuating piston 1 by an axial force is moved to the right, counter to the F.sub.A illustrated in
[0039] An adjustment pin 9 of the positive-displacement machine to be adjusted, as described in the prior art according to DE 10 2017 211 750 A1 mentioned at the outset, engages with a sliding block which on one side engages in a circumferential groove of the actuating piston 1. The adjustment pin 9 is displaced by the actuating piston 1 on account of an impingement with actuating pressure, this causing an adjustment of a displacement volume of a connected hydrostatic positive-displacement machine not shown here.
[0040] The spring force of the spring pack 5 acts counter to the axial force acting during an adjustment, for example the axial force F.sub.A, and in the absence of an actuating pressure returns the actuating piston 1 to the central position thereof (illustrated in
[0041] Transverse forces F.sub.Q arise on the actuating piston 1 on account of the one-sided eccentric position of the adjustment pin 9. The two sealing and guiding units 6 contribute toward the actuating piston 1 in the region of the main portion 3 and in the region of the cover 10 being guided in a stable manner in terms of tilting.
[0042] The two sealing and guiding units 6 which are in each case embodied as sealing collars have a minor wall thickness and are received in the shape of collars or sleeves in the circumferential recesses 8 of the external shell faces 4 of the actuating piston 1, said circumferential recesses 8 being adapted to said sealing and guiding units 6. A detailed description of the sealing and guiding units 6, the position, function and positioning of the latter, takes place by means of
[0043]
[0044] As discussed above, the two sealing and guiding units 6 by expanding and compressing an annular disk are in each case configured in the manner of collars having a minor wall thickness, and are in each case disposed about/in the circumferential recess 8 of the actuating piston 1 (only the circumferential recess adjacent to the pressurized chamber 11 is provided with the reference sign 8 in
[0045] The sealing and guiding unit 6 can have circumferential recesses which correspond to the protrusions 18a, 18b, 18c and which could receive the protrusions 18a, 18b, 18c in portions. The circumferential faces of the two sealing and guiding units 6 (sealing collars) are preferably planar (smooth), configured without recesses, wherein the protrusions 18a, 18b, 18c push into the circumferential wall such that radial plunging of the protrusions 18a, 18b, 18c into the sealing and guiding unit 6 results. A hybrid version having circumferential recesses in the sealing and guiding unit 6 is likewise conceivable, said circumferential recesses in terms of the radial extent thereof being smaller than the protrusions 18a, 18b, 18c such that plunging and pushing is combined. Independently of the type of the afore-described embodiment, the protrusions 18a, 18b, 18c are in engagement so as to engage axially behind the sealing and guiding unit 6.
[0046] The protrusions 18a, 18b, 18c, when viewed in the direction of an axial force F.sub.A resulting from the actuating pressure in the pressurized chamber 11, are of dissimilar sizes, wherein the first protrusion 18c which is disposed so as to be most remote from the first region 14 is larger than the second protrusion 18b which is larger than the smallest protrusion 18a which is disposed so as to be closest to the first region 14. The protrusions 18a, 18b, 18c are thus stepped, or disposed so as to decrease in size in the direction of the axial force F.sub.A, respectively (see
[0047] A detailed illustration of the circumferential recess 8 is shown in
[0048] The guide region 20 has a radial extent d, hereunder also referred to as the height d, which is substantially less than the axial extent a, hereunder also referred to as the length a. A space 40 which is delimited by an end face 36 of the circumferential recess 8, on the one hand, and is delimited by the guide region 20 and circumferentially by the base 34, on the other hand, is configured in the region of the end portion 26. A corresponding space 41 is configured in a further end portion 28, said space 41 being delimited by an end face 38, on the one hand, and delimited by the protrusion 18c and circumferentially by the base 34, on the other hand. The protrusions 18a, 18b, 18c as well as the guide region 20 extend from the base 34 in the radial direction.
[0049] The radial extent D.sub.a of the smallest protrusion 18a is larger than the radial extent d of the contact area formed by the guide region 20 and larger than the axial extent b of the protrusions 18a, 18b, 18c. The radial extent D.sub.c is larger than the radial extent D.sub.b and the latter is larger than the radial extent D.sub.a. The end face portions 22 which are configured on the protrusions 18a, 18b, 18c engage axially behind portions of the sealing and guiding unit 6 not illustrated here. These end face portions 22 absorb the axial force F.sub.A acting on the sealing and guiding unit 6 and by way of the protrusions 18a, 18b, 18c direct said axial force F.sub.A into the circumferential recess 8 and thus into the actuating piston 1.
[0050] The spaces 40, 41 in conjunction with the assigned sealing and guiding unit 6 configure radial gaps. Spaces are also configured between the guide region 20 and the protrusions 18a, 18b, 18c, as well as between the protrusions 18a, 18b, 18c. According to
[0051] Disclosed is an actuating piston for a hydrostatic adjustment installation having at least one sealing and guiding unit which is inserted into a circumferential recess of an actuating piston, said circumferential recess being composed of two regions, and has the effect of improving the guiding and sealing of the actuating piston. Furthermore disclosed is an adjustment installation which is configured having an actuating piston of this type.
LIST OF REFERENCE SIGNS
[0052] 1a Actuating cylinder
[0053] 1 Actuating piston
[0054] 2 Hydrostatic adjustment installation
[0055] 3 Main portion of the actuating cylinder
[0056] 4 External shell face
[0057] 5 Spring pack
[0058] 6 Sealing and guiding unit
[0059] 7 Pin
[0060] 8 Circumferential recess
[0061] 9 Adjustment pin
[0062] 10 Cover of the actuating cylinder
[0063] 11 Pressurized chamber
[0064] 12 Gap
[0065] 13 Support disk
[0066] 14 First region
[0067] 15 Support disk
[0068] 16 Second region
[0069] 17 Ventilation bore
[0070] 18 Protrusion
[0071] 19 Longitudinal axis
[0072] 20 Guide region
[0073] 21 Further pressurized chamber
[0074] 22 End face portion
[0075] 24 Internal shell face
[0076] 26 End portion
[0077] 28 End portion
[0078] 30 Chamfer
[0079] 32 Chamfer
[0080] 34 Base
[0081] 36 End face
[0082] 38 End face
[0083] 40 Chamber
[0084] 41 Chamber
[0085] F.sub.A Axial force
[0086] F.sub.Q Transverse force
[0087] a Length/axial extent of the guide region 20
[0088] b Length/axial extent of the protrusion
[0089] d Height/radial extent of the guide region 20
[0090] D Height/radial extent of the protrusion