DETAILED ACTION
Notice of Pre-AIA or AIA Status
The present application, filed on or after March 16, 2013, is being examined under the first inventor to file provisions of the AIA .
Response to Amendment
Applicants’ response filed 2/6/2026 amended claims 1, 8-9, 18 and 20, cancelled claim 19, and added new claim 21. Applicants’ amendments in light of their arguments are persuasive in overcoming the 35 USC 102/103 rejections over Gonia, and the 35 USC 103 rejection over Gonia in view of Suzuki from the office action mailed 11/7/2025; therefore, these rejections are withdrawn. New grounds of rejection necessitated by applicants’ amendments are set forth below.
Claim Rejections - 35 USC § 102/103
The following is a quotation of the appropriate paragraphs of 35 U.S.C. 102 that form the basis for the rejections under this section made in this Office action:
A person shall be entitled to a patent unless –
(a)(1) the claimed invention was patented, described in a printed publication, or in public use, on sale, or otherwise available to the public before the effective filing date of the claimed invention.
The following is a quotation of 35 U.S.C. 103 which forms the basis for all obviousness rejections set forth in this Office action:
A patent for a claimed invention may not be obtained, notwithstanding that the claimed invention is not identically disclosed as set forth in section 102, if the differences between the claimed invention and the prior art are such that the claimed invention as a whole would have been obvious before the effective filing date of the claimed invention to a person having ordinary skill in the art to which the claimed invention pertains. Patentability shall not be negated by the manner in which the invention was made.
The factual inquiries for establishing a background for determining obviousness under 35 U.S.C. 103 are summarized as follows:
1. Determining the scope and contents of the prior art.
2. Ascertaining the differences between the prior art and the claims at issue.
3. Resolving the level of ordinary skill in the pertinent art.
4. Considering objective evidence present in the application indicating obviousness or nonobviousness.
Claims 1-4, 7, 10-17 and 20-21 are rejected under 35 U.S.C. 102(a)(1) as anticipated by or, in the alternative, under 35 U.S.C. 103 as obvious over Sridhar et al., US Patent Application Publication No. 2018/0372151 (hereinafter referred to as Sridhar).
Regarding claims 1-4, 7 and 10-17, Sridhar discloses a system and method wherein the system includes an assembly with a base, and a coating disposed on the base. The assembly includes a shaft and a journal bearing coupled to the shaft, wherein at least one of the shaft and the journal bearing includes the base. The assembly may include a valve coupled to a valve seat, wherein at least one of the valve and the valve seat includes the base, and the base includes a plurality of dimples, the coating disposed on at least some dimples. The method is for disposing a coating on a base of the assembly using a friction surface process (as recited in claims 10 and 12-17) (see Abstract).
The function of the coating is to provide lubrication between valves and valve seats, and hence reduce friction. The base includes a plurality of dimples on the surface. As the pin tool is traversed along the base, iron-based alloy, or other material of the pin tool is deposited to form a coating of the pin tool material on the surface of the base (an amorphous metal as recited in claim 1 and reads on claims 2-3). The pin tool material is coated on some dimples. The coating may further comprise a solid lubricant, such as, molybdenum disulfide which can be mixed and therefore dispersed in the coating with the amorphous metal component (solid lubricant as recited in claim 1 and reads on claims 4 and 7 – reads on claim 7 as paragraph 0102 explicitly discloses that a desired mixture of solid lubricants can be used and concentration is a result effective variable and as such can be optimized without undue experimentation) (Para. [0066] and [0080]-[0102]) wherein the coating does not include any fluid lubricants (as recited in claim 11) (Para. [0097]).
Regarding claims 20-21, see discussion above.
Claim Rejections - 35 USC § 103
Claims 5-6 and 8-9 are rejected under 35 U.S.C. 103 as being unpatentable over Sridhar in view of Suzuki et al., US Patent Application Publication No. 2023/0167849 (hereinafter referred to as Suzuki).
Regarding claims 5-6, Sridhar discloses all the limitations discussed above but does not explicitly disclose the surface roughness recited in claims 5-6.
Suzuki discloses a turbo fluid machine includes a rotating member having a bearing-contact surface; an operating part configured to rotate together with the rotating member to compress and discharge a fluid; a housing accommodating the rotating member and the operating part; and a foil bearing having a bearing surface that faces the bearing-contact surface and supporting the rotating member such that the rotating member is rotatable relative to the housing. At least one of the bearing-contact surfaces or the bearing surface has thereon a coating layer. The coating layer comprises polyamide-imide serving as a binder resin and molybdenum disulfide serving as a solid lubricant and has a surface roughness ranging from 0.05 to 0.3 (as recited in claims 5-6 and 10-19) (see Abstract and see Figure 8). It would have been obvious to one of ordinary skill in the art at the time of the invention to combine the teachings of Sridhar with Suzuki as it is combining art elements according to known methods to yield predictable results.
Regarding claims 8-9, Sridhar/Suzuki do not explicitly disclose the relationship recited in the claims. It is the position of the examiner that as the combination of references disclose all the limitations of claims 1 and 6 that the combination of references would inherently read on claims 8-9. This is especially the case when taking into account paragraph 0057 of Suzuki. Polyamide-imide as the binder resin has high hardness and high wear resistance. Polyamide-imide further has high toughness and high viscosity. A transfer particle (abrasion powders) of polyamide-imide is transferred largely from the surface of the coating layer by initial wear due to sliding of the coating layer on a counterpart. This largely roughens the surface of the coating layer, thereby increasing the surface roughness of the coating layer after the initial wear. This raises the upper limit of the thickness of the fluid film in the foil bearing. That is, this increases the thickness of the fluid film in the transition from contact support of the rotating member by the foil bearing to non-contact support of the rotating member by the foil bearing, i.e., the thickness of the fluid film at the floating rotational speed at which the rotating member floats off the foil bearing, thereby decreasing the floating capability of the foil bearing. The decrease in the floating capability of the foil bearing increases the possibility of wear of the coating layer due to sliding of the coating layer on the counterpart, thereby decreasing the durability of the coating layer.
Claim Rejections - 35 USC § 103
Claim 18 is rejected under 35 U.S.C. 103 as being unpatentable over Sridhar in view of Marcos Izquierdo, US Patent Application Publication No. 2022/0390004 (hereinafter referred to as Marcos Izquierdo).
Regarding claim 18, Sridhar discloses all the limitations discussed above but does not explicitly disclose the limitations recited in claim 18.
Marcos Izquierdo discloses a fan mounted upstream of a low-pressure compressor. The fan is driven by a fan shaft which is driven by the LP shaft by means of a mechanical reducer. The fan comprises a plurality of fan vanes that extend radially outward from a fan disc. The fan vanes are radially delimited by a fan casing. The latter carries a nacelle attached to the aircraft. The reducer is formed with a gear train and is known by the acronym RGB for “Reduction Gear Box”. The reducer is generally of the planetary or epicyclic type. The reducer comprises, a sun gear, planet gears, a planet carrier, and a ring gear. The sun gear, the ring gear and the planet carrier are planetary because their axes of revolution coincide with the longitudinal axis X of the turbomachine. The planet gears each have a different axis of revolution and are equally distributed on the same operating diameter around the axis of the planetaries. These axes are parallel to the longitudinal axis X. The reducer is here with a planetary gear train. The input of the reducer is coupled to the LP shaft while the output of the reducer is coupled to the fan shaft. In particular, the ring gear is rotatable and the planet carrier is non-rotatable wherein the surface includes a coating (as recited in claim 18) (see Abstract and Para. [0036]-[0038]). It would have been obvious to one of ordinary skill in the art at the time of the invention to use the coating of Sridhar in the mechanical part of Marcos Izquierdo in order to enhance the friction reducing properties of the mechanical part.
Response to Arguments
Applicants’ arguments filed 2/6/2026 regarding claims 1-18 and 20-21 have been fully considered and are moot as the rejections from the previous office action have been withdrawn as discussed above.
It is the position of the examiner that the references discussed above adequately read on the claims as instantly recited.
Conclusion
Applicant's amendment necessitated the new ground(s) of rejection presented in this Office action. Accordingly, THIS ACTION IS MADE FINAL. See MPEP § 706.07(a). Applicant is reminded of the extension of time policy as set forth in 37 CFR 1.136(a).
A shortened statutory period for reply to this final action is set to expire THREE MONTHS from the mailing date of this action. In the event a first reply is filed within TWO MONTHS of the mailing date of this final action and the advisory action is not mailed until after the end of the THREE-MONTH shortened statutory period, then the shortened statutory period will expire on the date the advisory action is mailed, and any nonprovisional extension fee (37 CFR 1.17(a)) pursuant to 37 CFR 1.136(a) will be calculated from the mailing date of the advisory action. In no event, however, will the statutory period for reply expire later than SIX MONTHS from the mailing date of this final action.
Any inquiry concerning this communication or earlier communications from the examiner should be directed to VISHAL V VASISTH whose telephone number is (571)270-3716. The examiner can normally be reached M-F 9:00-4:30 and 7:00-10:00p.
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If attempts to reach the examiner by telephone are unsuccessful, the examiner’s supervisor, Prem Singh can be reached at 5712726381. The fax phone number for the organization where this application or proceeding is assigned is 571-273-8300.
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/VISHAL V VASISTH/Primary Examiner, Art Unit 1771
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