Prosecution Insights
Last updated: April 19, 2026
Application No. 18/858,084

AIRFOIL AND FLUID-DYNAMIC SURFACE COMPRISING SUCH AIRFOIL

Non-Final OA §102§112
Filed
Oct 18, 2024
Examiner
ZAMORA ALVAREZ, ERIC J
Art Unit
3745
Tech Center
3700 — Mechanical Engineering & Manufacturing
Assignee
R E M Patents S R L
OA Round
1 (Non-Final)
88%
Grant Probability
Favorable
1-2
OA Rounds
2y 5m
To Grant
99%
With Interview

Examiner Intelligence

Grants 88% — above average
88%
Career Allow Rate
458 granted / 519 resolved
+18.2% vs TC avg
Strong +22% interview lift
Without
With
+21.9%
Interview Lift
resolved cases with interview
Typical timeline
2y 5m
Avg Prosecution
14 currently pending
Career history
533
Total Applications
across all art units

Statute-Specific Performance

§103
33.8%
-6.2% vs TC avg
§102
27.6%
-12.4% vs TC avg
§112
31.7%
-8.3% vs TC avg
Black line = Tech Center average estimate • Based on career data from 519 resolved cases

Office Action

§102 §112
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 . Election/Restrictions Applicant’s election without traverse of Group I in the reply filed on 10/27/2025 is acknowledged. Claims 14-24 are examined. Claims 25-26 are withdrawn. Specification Applicant is reminded of the proper language and format for an abstract of the disclosure. The abstract should be in narrative form and generally limited to a single paragraph on a separate sheet within the range of 50 to 150 words in length. The abstract should describe the disclosure sufficiently to assist readers in deciding whether there is a need for consulting the full patent text for details. The language should be clear and concise and should not repeat information given in the title. It should avoid using phrases which can be implied, such as, “The disclosure concerns,” “The disclosure defined by this invention,” “The disclosure describes,” etc. In addition, the form and legal phraseology often used in patent claims, such as “means” and “said,” should be avoided. The abstract of the disclosure is objected to because: Line 8, change: “further [[concernsa]] concerns a fluid-dynamic…” Correction is required. See MPEP § 608.01(b). Claim Objections Claims 14, 22, and 24 are objected to because of the following informalities: Claim 14, line 4, change: “from the leading edge [[backwards]] toward the trailing edge,” Claim 14, line 6, change: “from the trailing edge [[forwards]] toward the leading edge,” Claim 22, line 2, change: “the central portions, in [[the]] a direction perpendicular…” Claim 24, line 2, change: “surface is [[the]] a blade of a rotor.” Appropriate correction is required. Claim Rejections - 35 USC § 112 The following is a quotation of 35 U.S.C. 112(b): (b) CONCLUSION.—The specification shall conclude with one or more claims particularly pointing out and distinctly claiming the subject matter which the inventor or a joint inventor regards as the invention. The following is a quotation of 35 U.S.C. 112 (pre-AIA ), second paragraph: The specification shall conclude with one or more claims particularly pointing out and distinctly claiming the subject matter which the applicant regards as his invention. Claims 14-24 are rejected under 35 U.S.C. 112(b) or 35 U.S.C. 112 (pre-AIA ), second paragraph, as being indefinite for failing to particularly point out and distinctly claim the subject matter which the inventor or a joint inventor, or for pre-AIA the applicant regards as the invention. Claim 14 recites the limitation "the leading edge" and “the trailing edge” in line 3. There is insufficient antecedent basis for this limitation in the claim. It is unclear whether the leading edge and the trailing edge are the same or different with respect to a “front leading edge” and a “rear trailing edge”, respectively, recited in line 1. Claim 20 is indefinite because in line 1, the claim recites of “A fluid-dynamic surface” and further recites in line 2, “at least two airfoils”. It is unclear how the fluid dynamic surface (i.e., 54 from Applicant’s Fig. 13) can comprise at least two airfoils because the fluid dynamic surface is a surface of a blade (56). It is therein unclear how the claim can be directed to a “fluid dynamic surface” and further claim “two airfoils according to claim 14” because structurally, the fluid dynamic surface cannot comprise of two airfoils since the fluid dynamic surface is a surface of a single airfoil/blade. In other words, two airfoils are not on the fluid dynamic surface (54), according to Applicant’s disclosure. Due to the lack of clarity and ambiguity of the claim, the metes and bounds cannot be determined, which renders the claim indefinite. Further, due to the lack of clarity of the claim, a prior art rejection cannot be applied to claim 20 and the dependent claims thereof (claims 21-24) since it is unclear how a fluid-dynamic surface of a blade airfoil can comprise two additional airfoils. Claim 22 recites the limitation "the extension of the central portion" in line 2. There is insufficient antecedent basis for this limitation in the claim. It is unclear of the feature “the extension” since “the extension” has not been previously introduced with respect to claims 1 or 20. Dependent claims are also rejected due to their dependency of a rejected independent claim. Claim Rejections - 35 USC § 102 In the event the determination of the status of the application as subject to AIA 35 U.S.C. 102 and 103 (or as subject to pre-AIA 35 U.S.C. 102 and 103) is incorrect, any correction of the statutory basis for the rejection will not be considered a new ground of rejection if the prior art relied upon, and the rationale supporting the rejection, would be the same under either status. 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. Claims 14-19 are rejected under 35 U.S.C. 102(a)(1) as being anticipated by Munoz Saiz (EP 1043223). Regarding claim 14, Munoz Saiz discloses an airfoil (Fig. 1) comprising: a front leading edge (i.e., front leading edge of airfoil shown in Fig. 1), a rear trailing edge (i.e., rear trailing edge shown in Fig. 1), a mean line (i.e., imaginary mean line equidistance from suction and pressure sides of airfoil in Fig. 1) and a thickness (i.e., thickness between top and bottom surfaces of airfoil in Fig. 1), - a front portion in which the thickness increases (as shown in Fig. 1, the front portion of the airfoil increases in thickness), along the mean line from the leading edge backwards, up to a maximum thickness (i.e., in the direction of an imaginary mean line toward the trailing edge up to section 2, which has the maximum thickness); and - a rear portion in which the thickness increases along the mean line from the trailing edge forwards, up to the maximum thickness (i.e., in the direction from the trailing edge of the airfoil toward the leading edge of the airfoil, the thickness increases to a maximum thickness up to section 2); a central portion (2), placed between the front portion and the rear portion (as shown in Fig. 1), in which the thickness is constant and equal to the maximum thickness (as shown in Fig. 1, the thickness is constant and maximum in section 2); and at least one front section (4) and rear section (5), assembled (assembled as shown in Fig. 1), wherein: - the front portion is defined by the front section (i.e., the front portion containing the leading edge is defined by the front section 4); and - the rear portion is defined by the rear section (i.e., the rear portion containing the trailing edge is defined by the rear section 5). Regarding claim 15, the limitation “wherein the front section (4) and the rear section (5) are obtained by extrusion/pultrusion.” renders the claim as a product-by-process claim. As shown above, the apparatus or structure claimed is identical to that described in the reference and is therefore anticipated by the reference because patentability of a product does not depend on its method of production. See MPEP 2113. Regarding claim 16, Munoz Saiz discloses wherein the central portion (2) is defined by the front section (i.e., the central portion is continuous with the front section 4, and is therein defined by the front section) and/or by the rear section (i.e., the central portion is continuous with the rear section 5, and is therein defined by the rear section). Regarding claim 17, Munoz Saiz discloses a central section (i.e., the central section is formed by the central portion 2, wherein the central section spans between the front section 4 and the rear section 5, as shown in Fig. 1). Regarding claim 18, the limitation “wherein the central section (2) is obtained by extrusion/pultrusion.” renders the claim as a product-by-process claim. As shown above, the apparatus or structure claimed is identical to that described in the reference and is therefore anticipated by the reference because patentability of a product does not depend on its method of production. See MPEP 2113. Regarding claim 19, Munoz Saiz discloses a back (i.e., back surface referenced by “bk” in Fig. 1’ below) and a belly (i.e., belly surface referenced by “be” in Fig. 1’), and wherein the back and/or the belly and/or the mean line are continuous and uniform (i.e., each surface of the back “bk” and the belly “be” is continuous and uniform, as shown in Fig. 1’, wherein each surface is planar and uniform without changes in direction; the belly and back are also continuous with other portions of the airfoil). PNG media_image1.png 262 793 media_image1.png Greyscale Fig. 1’ Conclusion Any inquiry concerning this communication or earlier communications from the examiner should be directed to ERIC J ZAMORA ALVAREZ whose telephone number is (571)272-7928. The examiner can normally be reached Monday-Friday 7:30 am- 5:00 pm EST alternating Fridays off. Examiner interviews are available via telephone, in-person, and video conferencing using a USPTO supplied web-based collaboration tool. To schedule an interview, applicant is encouraged to use the USPTO Automated Interview Request (AIR) at http://www.uspto.gov/interviewpractice. If attempts to reach the examiner by telephone are unsuccessful, the examiner’s supervisor, COURTNEY HEINLE can be reached at (571)270-3508. The fax phone number for the organization where this application or proceeding is assigned is 571-273-8300. Information regarding the status of published or unpublished applications may be obtained from Patent Center. Unpublished application information in Patent Center is available to registered users. To file and manage patent submissions in Patent Center, visit: https://patentcenter.uspto.gov. Visit https://www.uspto.gov/patents/apply/patent-center for more information about Patent Center and https://www.uspto.gov/patents/docx for information about filing in DOCX format. For additional questions, contact the Electronic Business Center (EBC) at 866-217-9197 (toll-free). If you would like assistance from a USPTO Customer Service Representative, call 800-786-9199 (IN USA OR CANADA) or 571-272-1000. /ERIC J ZAMORA ALVAREZ/Primary Examiner, Art Unit 3745 12/01/2025
Read full office action

Prosecution Timeline

Oct 18, 2024
Application Filed
Oct 18, 2024
Response after Non-Final Action
Nov 18, 2024
Response after Non-Final Action
Dec 01, 2025
Non-Final Rejection — §102, §112 (current)

Precedent Cases

Applications granted by this same examiner with similar technology

Patent 12601357
AIR MOVING DEVICES, AERODYNAMIC ROTOR, AND METHODS
2y 5m to grant Granted Apr 14, 2026
Patent 12595782
WIND TURBINE BLADE AND METHOD FOR MANUFACTURING A WIND TURBINE BLADE
2y 5m to grant Granted Apr 07, 2026
Patent 12590590
AIRCRAFT ENGINE IMPELLER WITH EXDUCER SHROUD FORWARD SWEEP
2y 5m to grant Granted Mar 31, 2026
Patent 12588784
Mixing Utensil
2y 5m to grant Granted Mar 31, 2026
Patent 12587065
ENERGY CONVERSION DEVICE, ASSOCIATED SYSTEMS AND METHODS
2y 5m to grant Granted Mar 24, 2026
Study what changed to get past this examiner. Based on 5 most recent grants.

AI Strategy Recommendation

Get an AI-powered prosecution strategy using examiner precedents, rejection analysis, and claim mapping.
Powered by AI — typically takes 5-10 seconds

Prosecution Projections

1-2
Expected OA Rounds
88%
Grant Probability
99%
With Interview (+21.9%)
2y 5m
Median Time to Grant
Low
PTA Risk
Based on 519 resolved cases by this examiner. Grant probability derived from career allow rate.

Sign in with your work email

Enter your email to receive a magic link. No password needed.

Personal email addresses (Gmail, Yahoo, etc.) are not accepted.

Free tier: 3 strategy analyses per month