Automatic Greaser Retainer
20230228287 · 2023-07-20
Inventors
Cpc classification
F16B5/128
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A retaining system provides stability to an automatic greater when attached to a wheel hub. The system includes a hub assembly having a hub base and body, an automatic greater affixed to the hub body, and a retainer having a metal body. The metal body includes pair of wing grips connected by a bridge section. Prongs extend from each wing grip and terminate at first and second ends. Retainer tips extend from each end toward opposing prongs. When in an engaged configuration, the metal body of the retainer may simultaneously engage an interior surface of the automatic greater and an outer surface of the hub body so that the automatic greater is secure and removably affixable from the hub body. To secure the retainer to the hub body, the pair of tips are positioned within a pair of orifices located on the outer surface of hub body.
Claims
1. An apparatus for retaining an automatic greaser, comprising: a metal body, the metal body including: a first wing grip spaced from a second wing grip via a bridge section; a first prong extending from the first wing grip to a first end; a second prong extending from the second wing grip to a second end; and a pair of tips, each of the pair of tips extending from a respective one of the first end and the second end of the first and second prongs toward the other of the first and second prongs; and wherein the metal body is aligned along a retaining plane when in an engaged configuration.
2. The apparatus of claim 1, wherein the apparatus is a retaining clip.
3. The apparatus of claim 1, wherein the apparatus is configured to engage a wheel hub body.
4. The apparatus of claim 1, wherein each of the first wing grip and the second wing grip comprises a lower retaining section substantially parallel to the pair of tips.
5. The apparatus of claim 1, wherein each of the first prong and the second prong are tensioned inward toward a tension axis when in a disengaged configuration.
6. The apparatus of claim 1, wherein each of the first tip and the second tip are substantially parallel with the bridge section when in an engaged configuration.
7. The apparatus of claim 1, wherein the bridge section is configured to abut at least one of a cavity of an automatic greater and a greater cover.
8. An automatic greater retaining system, comprising: a hub assembly having a hub base and a hub body, the hub body including at least one friction reducing element positioned within the hub body; an automatic greater affixed to the hub body; a retainer having a metal body, the metal body including; a first wing grip spaced from a second wing grip via a bridge section; a first prong extending from the first wing grip to a first end; a second prong extending from the second wing grip to a second end; and a pair of tips, each of the pair of tips extending from a respective one of the first end and the second end of the first and second prongs toward the other of the first and second prongs and engaging an outer surface of the hub body with the pair of tips; and wherein the metal body is aligned along a retaining plane when in an engaged configuration.
9. The system of claim 7, wherein the hub body is a wheel hub body.
10. The system of claim 7, wherein each of the pair of tips engages a respective one of a pair of orifices symmetrically spaced from one another on the outer surface of the hub body.
11. The system of claim 7, wherein the retainer abuts the automatic greater and the wheel hub along the retaining plane.
12. The system of claim 7, wherein the bridge section is configured to abut at least one of a cavity of an automatic greater and a greater cover.
13. The system of claim 7, wherein the retainer simultaneously engages an interior surface of the automatic greater and an outer surface of the hub body when in an engaged configuration.
14. The system of claim 7, wherein each of the first and second wing grips are configured to apply at least one compressive force to an interior surface of the automatic greater when the retainer is in an engaged configuration.
15. A method for manufacturing an automatic greater retaining system, comprising: providing a metal strand; forming the metal strand into a retainer configured to retain an automatic greaser, the retainer comprising: a first wing grip spaced from a second wing grip via a bridge section; a first prong extending from the first wing grip; a second prong extending from the second wing grip; and a pair of tips, each of the pair of tips extending from a respective one of the first end and the second end of the first and second prongs toward the other of the first and second prongs; engaging an automatic greater with the first wing grip and the second wing grip; and engaging an outer surface of a hub body with the pair of tips so that the retainer is aligned along a retaining plane when in an engaged configuration.
16. The method of claim 15, wherein the hub body is a wheel hub body.
17. The method of claim 15, further comprising forming each of the first wing grip and the second wing grip substantially parallel to the pair of tips.
18. The method of claim 15, further comprising engaging, via each of the pair of tips, a respective one of a pair of orifices symmetrically spaced from one another on the outer surface of the hub body.
19. The method of claim 15, further comprising positioning the retainer to abut the automatic greater and the hub body along the retaining plane.
20. The method of claim 15, further comprising forming each of the first and second wing grips in a shape configured to apply at least one compressive force to an interior surface of the automatic greater when the retainer is in an engaged configuration.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0009] The disclosed subject matter, objectives, and advantages thereof, will best be understood by reference to the following detailed description of an illustrative embodiment when read in conjunction with the accompanying drawings, wherein:
[0010]
[0011]
[0012]
[0013]
DETAILED DESCRIPTION
[0014] Reference now should be made to the drawings, in which the same reference numbers are used throughout the different figures to designate the same components.
[0015] It will be understood that, although the terms first, second, third, etc. may be used herein to describe various elements, these elements should not be limited by these terms. These terms are only used to distinguish one element from another element. Thus, a first element discussed below could be termed a second element without departing from the teachings of the present disclosure.
[0016] The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting. As used herein, the singular forms “a”, “an”, and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising” or “includes” and/or “including” when used in this specification, specify the presence of stated features, regions, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, regions, integers, steps, operations, elements, components, and/or groups thereof
[0017]
[0018] First and second prongs 12,13 are attached to the outer jaws 23,24 of respective first and second wing grips 14,15. First prong 12 may extend from the first wing grip 14 to a first end 18 while a second prong 13 may extend from the second wing grip 15 to a second end 19. Tips 10,11 positioned at each prong end 18,19 may extend toward the other of the first and second prongs 12,13. A compressive force applied by the prongs 12,13 assist in securely positioning the first and second ends 18,19 into respective orifices 25 (only one orifice depicted in
[0019] In embodiments, each of the first prong 12 and the second prong 13 are tensioned inward toward the tension axis when clip 5 is in a disengaged configuration (as shown in
[0020] In embodiments, metal body 17 may comprise tension wire. Use of tension wire may allow a user of clip 5 to use his/her hands to pull apart first and second prongs 12,13 away from a tension axis and place clip 5 on to automatic greater 31 and hub assembly 33 as well as pull apart first and second prongs 12,13 away from the tension axis and remove clip 5 from automatic greater 31 and hub assembly 33.
[0021] As shown in
[0022]
[0023] Lower retaining sections 29,30 of the first and second wing grips 14,15 may keep the inner jaws 21,22 and outer jaws 23,24 in the proper position so that tension forces are applied to lips 32 of the sidewall of automatic greater 31 and clip 5 is further secured to automatic greater 31. First and second prongs 12,13 extending from the wing grips 14,15 may be biased inward so that the tips 10,11 affixed to the prong ends 18,19 are able to removably engage the hub body. The metal body 17, when engaged, may be aligned along the retaining plane extending along the length of system 34. In embodiments, each of the lower retaining sections 29,30 may be substantially parallel to respective ones of the pair of tips 10,11. In further embodiments, each of the first tip 10 and the second tip 11 may be substantially parallel with bridge section 16 when clip 5 is in an engaged configuration.
[0024] In order to provide additional support for automatic greater 31, the pair of tips 10,11 may each engage one of a pair of orifices 25 (other orifice not depicted) that are symmetrically spaced from one another on the outer surface 37 of hub body 36. Additionally, clip 5 may be positioned to abut the automatic greater 31 and hub body 36 along the retaining plane when clip is in an engaged position.
[0025] It is noted that the shape of clip 5 may allow a user to easily insert and remove the clip 5 from an automatic greater and wheel bearing. The shape of clip 5 may be designed in a way that allows the user to grip the clip 5 at the first and second wing grips 14,15, allowing for comfortable and easy insertion and removal of clip 5. Furthermore, as shown in
[0026]
[0027] Retainer 5, such as the clip 5 described previously, includes a metal body 17 and is configured to engage both the automatic greater 31 and the hub body 36. First and second wing grips 14,15 of the metal body 17 may then engage 450 an automatic greater 31 (as described previously). An outer surface 37 of a hub body 36 may also be engaged 460 by retainer tips 10,11 so that retainer 5 is aligned along the retaining plane when in an engaged configuration. In order to provide additional support for automatic greater 31, the pair of tips 10,11 may each engage 470 one of a pair of orifices 25 (other orifice not depicted) that are symmetrically spaced from one another on the outer surface 37 of hub body 36. Furthermore, retainer 5 may be positioned 480 to abut the automatic greater 31 and hub body 36 along the retaining plane.
[0028] In embodiments, a drill may be used to form round orifices 25 (other orifice not depicted) in hub body 36.
ELEMENTS LIST
[0029] retaining clip 5
[0030] left tip 10
[0031] right tip 11
[0032] first prong 12
[0033] second prong 13
[0034] first wing grip 14
[0035] second wing grip 15
[0036] bridge section 16
[0037] metal body 17
[0038] first prong end 18
[0039] second prong end 19
[0040] inner jaws 21,22
[0041] outer jaws 23,24
[0042] orifices 25 (only one orifice depicted in
[0043] greater cover/bra (not depicted)
[0044] automatic greater cavity 28
[0045] lower retaining sections 29,30
[0046] automatic greater 31
[0047] lips 32
[0048] (wheel) hub assembly 33
[0049] automatic greater retaining system 34
[0050] hub base 35
[0051] hub body 36
[0052] outer surface 37
[0053] In embodiments, metal body 17 may comprise a coating that may abut at least a portion of the outer surface of metal body 17.
[0054] It is noted that the space between first prong 12 and second prong 13 may allow a user to insert his/her fingers into the space, moving first and second prongs 12,13 into an open, disengaged configuration (pulling first and second prongs 12,13 away from the tension axis as well as pulling left and right tips 10,11 out of orifices 25 [and other orifice not depicted]) for the insertion and removal of clip 5 from automatic greater 31 and hub assembly 33.
[0055] It is noted that retaining clip 5 may be utilized in an automatic greater retaining system 34 that is not associated with wheel hub assemblies.
[0056] For the purposes of this disclosure, the terms “clip”, “retaining clip”, “retainer”, “automatic greater clip”, “automatic greater retaining clip”, and “apparatus” may be synonymous.
[0057] For the purposes of this disclosure, the terms “hub assembly” and “wheel hub assembly” may be synonymous.
[0058] For the purposes of this disclosure, the term “engaged configuration” may refer to clip 5 engaging both the automatic greater 31 and the hub assembly 33 (as shown in
[0059] A plurality of additional features and feature refinements are applicable to specific embodiments. These additional features and feature refinements may be used individually or in any combination. It is noted that each of the following features discussed may be, but are not necessary to be, used with any other feature or combination of features of any of the embodiments presented herein.
[0060] Unless otherwise defined, all technical and scientific terms used herein have the same meanings as are commonly understood by one of ordinary skill in the art to which this disclosure belongs. Although methods similar or equivalent to those described herein can be used in the practice or testing of the present disclosure, suitable methods are described herein.
[0061] All publications, patent applications, patents, and other references mentioned herein are incorporated by reference in their entirety. In case of conflict, the patent specification, including definitions, will prevail. In addition, the materials, methods, and examples are illustrative only and not intended to be limiting.
[0062] It will be appreciated by persons skilled in the art that the present disclosure is not limited to what has been particularly shown and described hereinabove. Rather, the scope of the present disclosure is defined by the appended claims and includes both combinations and sub-combinations of the various features described hereinabove as well as variations and modifications thereof, which would occur to persons skilled in the art upon reading the foregoing description.