Prosecution Insights
Last updated: May 29, 2026
Application No. 19/170,780

TURBINE ENGINE GEARBOX ASSEMBLY

Final Rejection §102§103
Filed
Apr 04, 2025
Priority
Apr 04, 2024 — IT 102024000007375
Examiner
KNIGHT, DEREK DOUGLAS
Art Unit
3655
Tech Center
3600 — Transportation & Electronic Commerce
Assignee
GE Aviation Czech S R O
OA Round
2 (Final)
85%
Grant Probability
Favorable
3-4
OA Rounds
1y 2m
Est. Remaining
88%
With Interview

Examiner Intelligence

Grants 85% — above average
85%
Career Allowance Rate
643 granted / 757 resolved
+32.9% vs TC avg
Minimal +3% lift
Without
With
+3.2%
Interview Lift
resolved cases with interview
Typical timeline
2y 4m
Avg Prosecution
11 currently pending
Career history
779
Total Applications
across all art units

Statute-Specific Performance

§101
0.8%
-39.2% vs TC avg
§103
51.6%
+11.6% vs TC avg
§102
26.0%
-14.0% vs TC avg
§112
19.4%
-20.6% vs TC avg
Black line = Tech Center average estimate • Based on career data from 757 resolved cases

Office Action

§102 §103
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 . 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 (i.e., changing from AIA to pre-AIA ) 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. Claim(s) 1, 7, and 15-16 is/are rejected under 35 U.S.C. 102(a)(1) as being anticipated by GRAVINA (US 10,8890,247). Regarding claim 1, GRAVINA discloses a turbine engine comprising: a turbo-engine coupled to an input shaft (120); a fan (38) coupled to an output shaft (45); and a gearbox assembly (46), wherein a torque is transferrable from the input shaft to the output shaft through the gearbox assembly, the gearbox assembly comprising: a split sun gear (106) rotationally coupled to the input shaft, the split sun gear comprising a forward sun gear (114) and an aft sun gear (112) separate from the forward sun gear, wherein the forward sun gear and the aft sun gear are each rotationally coupled to the input shaft; a plurality of planet gears (122, 124) located radially outward of, and intermeshing with, the split sun gear; and a single piece ring gear (126) located radially outward of, and intermeshing with, the plurality of planet gears ; and a connection device for rotationally coupling the split sun gear (106) to the input shaft (120), the connection device comprising a forward support member ((A), see Figure 1 below), an aft support member (B) , and an input shaft coupling member (C), wherein the forward support member, the aft support member, and the input shaft coupling member are coupled together (via the bolt and nut) at the input shaft coupling member. PNG media_image1.png 414 681 media_image1.png Greyscale Figure 1: Simplified and annotated Fig. 2 of GRAVINA Regarding claim 7, the combination of GRAVINA_247-GRAVINA_260 discloses the forward support member (A) extends between the input shaft (120) and the forward sun gear (114), the aft support member (B) extends between the input shaft (120) and the aft sun gear (112), and the input shaft coupling member (C) rotationally couples the forward sun gear and the aft sun gear to the input shaft. Regarding claim 15, the combination of GRAVINA discloses each of the forward support member (A), the aft support member (B), and the input shaft coupling member (C) comprises a first portion and a second portion. Regarding claim 16, the combination of GRAVINA discloses a fastening device (bolts and nut) extending through the first portion of each of the forward support member, the aft support member, and the input shaft coupling member to secure the forward sun gear and the aft sun gear in an axial direction with respect to the input shaft Claim Rejections - 35 USC § 103 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 (i.e., changing from AIA to pre-AIA ) 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 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. Claim(s) 2 is/are rejected under 35 U.S.C. 103 as being unpatentable over GRAVINA (US 10,8890,247) as applied to claims 1 and 3 above, and further in view of MOULY et al. (US 11,674,592). Regarding claim 2, GRAVINA does not disclose the split sun gear as a double helical gear. MOULY teaches a sun gear (11) that has helical teeth (col. 3, lines 4-7). It would have been obvious to one of ordinary skill in the art, before the effective filing date of the invention to have the teeth of the sun gear of GRAVINA be helical, as taught by MOULY, as MOULY teaches the teeth of the reducer can be straight, helical, or herringbone (col. 3, lines 4-7). Claim(s) 5 and 8 is/are rejected under 35 U.S.C. 103 as being unpatentable over GRAVINA (US 10,8890,247) as applied to claims 1 and 3 above, and further in view of GRAVINA et al. (US 10,823,260). Regarding claim 5, GRAVINA_247 discloses the aft support member (B) is rotationally coupled to the input shaft coupling member (C) but does not disclose it being a curvic connection. GRAVINA_260 teaches a connection device comprising a forward support member (51c), an aft support member (74c), and an input shaft coupling member (32c) via a curvic connection (see col. 9, lines 42-47; and Figs. 9-10 of GRAVINA_260). It would have been obvious to one of ordinary skill in the art, before the effective filing date of the invention to modify the connection device of GRAVINA_247 to have the details of GRAVINA_260 as they both are used to connect an input shaft to a split sun gear of a gear box assembly of a turbine engine. The design detailed in GRAVINA_260 allows for the transmission device to be manufactured and assembled simply, so as to reduce the errors in construction and assembly. (GRAVINA_260, col.1, lines 63-67). Regarding claim 8, the combination of GRAVINA-GRAVINA_260 discloses the forward support member is rotationally coupled to the aft support member with a curvic connection. Allowable Subject Matter Claims 6, 9-14, and 17-22 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. Response to Arguments Applicant’s arguments with respect to claim(s) 1 and 4 have been considered but are moot because the new ground of rejection required by the claim amendments. 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 DEREK D. KNIGHT whose telephone number is (571)272-7951. The examiner can normally be reached Telework: From 5:30am-1:30pm 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, Ernesto Suarez can be reached at 571-270-5565. 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. /DEREK D KNIGHT/ Primary Examiner, Art Unit 3655
Read full office action

Prosecution Timeline

Apr 04, 2025
Application Filed
Oct 08, 2025
Non-Final Rejection mailed — §102, §103
Jan 08, 2026
Response Filed
Apr 10, 2026
Final Rejection mailed — §102, §103 (current)

Precedent Cases

Applications granted by this same examiner with similar technology

Patent 12636951
IN-WHEEL DRIVING DEVICE
3y 8m to grant Granted May 26, 2026
Patent 12638073
PLANETARY GEARBOX DEVICE COMPRISING OIL FEED NOZZLES AND OIL FEED CHANNELS ARRANGED ECCENTRICALLY INSIDE PLANET GEARS, CORRESPONDING INDUSTRIAL GEARBOX, CORRESPONDING USE, AND CORRESPONDING METHOD
1y 7m to grant Granted May 26, 2026
Patent 12638075
TRANSFER OF LUBRICANT INTO THE INTERIOR OF A HOLLOW SHAFT
1y 6m to grant Granted May 26, 2026
Patent 12623535
TORQUE VECTORING DEVICE FOR A VEHICLE
3y 0m to grant Granted May 12, 2026
Patent 12607253
POWER TRANSMISSION DEVICE FOR VEHICLE
1y 4m to grant Granted Apr 21, 2026
Study what changed to get past this examiner. Based on 5 most recent grants.

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Prosecution Projections

3-4
Expected OA Rounds
85%
Grant Probability
88%
With Interview (+3.2%)
2y 4m (~1y 2m remaining)
Median Time to Grant
Moderate
PTA Risk
Based on 757 resolved cases by this examiner. Grant probability derived from career allowance rate.

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