Prosecution Insights
Last updated: October 27, 2026
Application No. 19/493,400

COUPLING DEVICE FOR TWO PARTS OF AN AIRCRAFT TURBOMACHINE

Non-Final OA §102
Filed
Dec 15, 2025
Priority
Jun 27, 2023 — FR FR2306726 +1 more
Examiner
BROCKMAN, ELDON T
Art Unit
3745
Tech Center
3700 — Mechanical Engineering & Manufacturing
Assignee
Safran S.A.
OA Round
1 (Non-Final)
85%
Grant Probability
Favorable
1-2
OA Rounds
1y 7m
Est. Remaining
91%
With Interview

Examiner Intelligence

Grants 85% — above average
85%
Career Allowance Rate
609 granted / 716 resolved
+15.1% vs TC avg
Moderate +6% lift
Without
With
+5.7%
Interview Lift
resolved cases with interview
Typical timeline
2y 6m
Avg Prosecution
18 currently pending
Career history
742
Total Applications
across all art units

Statute-Specific Performance

§101
1.0%
-39.0% vs TC avg
§103
39.1%
-0.9% vs TC avg
§102
33.8%
-6.2% vs TC avg
§112
22.3%
-17.7% vs TC avg
Black line = Tech Center average estimate • Based on career data from 716 resolved cases

Office Action

§102
DETAILED ACTION The present application, filed on or after March 16, 2013, is being examined under the first inventor to file provisions of the AIA . This action is in response to the claims filed 12/15/2025. Claims 1-11 are presented for examination. Preliminary amendment is acknowledged. Priority Receipt is acknowledged of certified copies of papers required by 37 CFR 1.55. Information Disclosure Statement The information disclosure statement (IDS) submitted on 12/15/2025 is in compliance with the provisions of 37 CFR 1.97. Accordingly, the information disclosure statement is being considered by the examiner. Claim Rejections - 35 USC § 102 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. (a)(2) the claimed invention was described in a patent issued under section 151, or in an application for patent published or deemed published under section 122(b), in which the patent or application, as the case may be, names another inventor and was effectively filed before the effective filing date of the claimed invention. Claim(s) 1, 7-8, and 10-11 is/are rejected under 35 U.S.C. 102(a)(1) as being anticipated by Di Paola et al. in US Patent 11414993 (hereinafter “Di Paola”). Regarding claim 1, Di Paola discloses (column 5, line 3 - column 10, line 16; figures 1-8) a coupling device (50) for coupling between a first part (26) of a turbine rotor (22) and a second part (36) of a turbine rotor (22) extending along a longitudinal axis (11), said first rotor part (26) being provided with a first thread (60), said coupling device (50) comprising a nut (80) which is provided with a nut thread that is intended to engage with said first thread (60), said nut (80) being intended to lock said second rotor part (36) onto said first rotor part (26) along said longitudinal axis, said coupling device (50) further comprises a brake (90) which comprises a first rotational coupling member (95) which is intended to engage with a first complementary rotational coupling member (86) provided on said nut (80) in a first rotational coupling position, said brake (90) being free to move in longitudinal translation relative to said nut (90) in said first rotational coupling position, and which comprises a second rotational coupling member (97) which is intended to engage with a second complementary rotational coupling member (73, 74) provided on said second rotor part (36) in a second rotational coupling position during the first rotational coupling position, said coupling device (80) further comprising a longitudinal locking element (100) which is intended to engage with said brake (90) and with said nut (80) in order to longitudinally lock said brake onto said nut in said second rotational coupling position. Regarding claim 7, Di Paola discloses the coupling device according to claim 1, wherein said longitudinal locking (100) element is a split O-ring which is housed in a recess (87) of said nut (see Fig. 3B and 8). Regarding claim 8, Di Paola discloses the coupling device according to claim 1, wherein said first rotor part is a rotor shaft (26) and said second part is a sleeve which is capable of sliding on said first part (see Fig. 2). Regarding claim 10, Di Paola discloses an aircraft engine (column 4 line 8). Regarding claim 11, assembly of the coupling device of Di Paola as applied above against claim 1 necessarily contains all of the method steps required of claim 11. The rejection will not be repeated verbatim so as to not unnecessarily belabor the record. Allowable Subject Matter Claims 2-6 and 9 are objected to as being dependent upon a rejected base claim, but would be allowable if rewritten in independent form including all of the limitations of the base claim and any intervening claims. The following is a statement of reasons for the indication of allowable subject matter. Regarding claim 2, Di Paola, applied above and considered the closest art of record, is silent to the coupling device according to claim 1, wherein said first rotational coupling member is a set of N teeth distributed evenly around the circumference of said brake and said first complementary rotational coupling member is a set of N notches distributed evenly around the circumference of said nut, such that in said first rotational coupling position each of said teeth is housed in one of said notches. Instead, the equivalent notches of Di Paola are distributed around the first complementary rotational coupling member, not the nut. Claims 3-4 depend on claim 2. Regarding claims 5-6 and 9, the art of record is silent to the particular positional interactions of components required of any of these claims. Conclusion The prior art made of record and not relied upon is considered pertinent to applicant's disclosure. US8491267 discloses a retaining ring arrangement for a gas turbine engine with complementary engaging teeth and recesses. US2013/0156589 discloses a rotor retaining system with a split ring coupling shaft components. Any inquiry concerning this communication or earlier communications from the examiner should be directed to ELDON T BROCKMAN whose telephone number is (571)270-3263. The examiner can normally be reached Mon-Fri 9am-5pm EST. 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, Court 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. /ELDON T BROCKMAN/Primary Examiner, Art Unit 3799
Read full office action

Prosecution Timeline

Dec 15, 2025
Application Filed
Oct 01, 2026
Non-Final Rejection mailed — §102 (current)

Precedent Cases

Applications granted by this same examiner with similar technology

Patent 12760657
Nozzle For Partitioned Volute
1y 7m to grant Granted Oct 13, 2026
Patent 12752891
LIFE-SAVING ROBOT
2y 0m to grant Granted Oct 06, 2026
Patent 12741356
THERMAL IMAGING SURFACE PROCESSING AUXILIARY SYSTEM AND METHOD
2y 9m to grant Granted Sep 22, 2026
Patent 12742391
METHOD OF RESTORING ALLOY DEPLETION IN AN AIRFOIL AROUND COOLING HOLES
1y 8m to grant Granted Sep 22, 2026
Patent 12742457
IMPELLER
1y 4m to grant Granted Sep 22, 2026
Study what changed to get past this examiner. Based on 5 most recent grants.

Strategy Recommendation AI-generated — please review before filing

Get a prosecution strategy drawn from examiner precedents, rejection analysis, and claim mapping.
Typically takes 5-10 seconds — AI-generated, attorney review required before filing

Prosecution Projections

1-2
Expected OA Rounds
85%
Grant Probability
91%
With Interview (+5.7%)
2y 6m (~1y 7m remaining)
Median Time to Grant
Low
PTA Risk
Based on 716 resolved cases by this examiner. Grant probability derived from career allowance 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