Prosecution Insights
Last updated: May 29, 2026
Application No. 18/657,507

ELECTRIC MACHINE FLUID COOLING SYSTEM WITH AIR VENT

Non-Final OA §103
Filed
May 07, 2024
Priority
May 11, 2023 — provisional 63/501,596
Examiner
SECK, AHMED F
Art Unit
2834
Tech Center
2800 — Semiconductors & Electrical Systems
Assignee
Dana Automotive Systems Group LLC
OA Round
1 (Non-Final)
69%
Grant Probability
Favorable
1-2
OA Rounds
11m
Est. Remaining
87%
With Interview

Examiner Intelligence

Grants 69% — above average
69%
Career Allowance Rate
71 granted / 103 resolved
+0.9% vs TC avg
Strong +18% interview lift
Without
With
+18.5%
Interview Lift
resolved cases with interview
Typical timeline
2y 11m
Avg Prosecution
19 currently pending
Career history
134
Total Applications
across all art units

Statute-Specific Performance

§103
94.3%
+54.3% vs TC avg
§102
4.3%
-35.7% vs TC avg
§112
0.7%
-39.3% vs TC avg
Black line = Tech Center average estimate • Based on career data from 103 resolved cases

Office Action

§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 . Priority Receipt is acknowledged of certified copies of papers required by 37 CFR 1.55. Double Patenting The nonstatutory double patenting rejection is based on a judicially created doctrine grounded in public policy (a policy reflected in the statute) so as to prevent the unjustified or improper timewise extension of the “right to exclude” granted by a patent and to prevent possible harassment by multiple assignees. A nonstatutory double patenting rejection is appropriate where the conflicting claims are not identical, but at least one examined application claim is not patentably distinct from the reference claim(s) because the examined application claim is either anticipated by, or would have been obvious over, the reference claim(s). See, e.g., In re Berg, 140 F.3d 1428, 46 USPQ2d 1226 (Fed. Cir. 1998); In re Goodman, 11 F.3d 1046, 29 USPQ2d 2010 (Fed. Cir. 1993); In re Longi, 759 F.2d 887, 225 USPQ 645 (Fed. Cir. 1985); In re Van Ornum, 686 F.2d 937, 214 USPQ 761 (CCPA 1982); In re Vogel, 422 F.2d 438, 164 USPQ 619 (CCPA 1970); In re Thorington, 418 F.2d 528, 163 USPQ 644 (CCPA 1969). A timely filed terminal disclaimer in compliance with 37 CFR 1.321(c) or 1.321(d) may be used to overcome an actual or provisional rejection based on nonstatutory double patenting provided the reference application or patent either is shown to be commonly owned with the examined application, or claims an invention made as a result of activities undertaken within the scope of a joint research agreement. See MPEP § 717.02 for applications subject to examination under the first inventor to file provisions of the AIA as explained in MPEP § 2159. See MPEP § 2146 et seq. for applications not subject to examination under the first inventor to file provisions of the AIA . A terminal disclaimer must be signed in compliance with 37 CFR 1.321(b). The filing of a terminal disclaimer by itself is not a complete reply to a nonstatutory double patenting (NSDP) rejection. A complete reply requires that the terminal disclaimer be accompanied by a reply requesting reconsideration of the prior Office action. Even where the NSDP rejection is provisional the reply must be complete. See MPEP § 804, subsection I.B.1. For a reply to a non-final Office action, see 37 CFR 1.111(a). For a reply to final Office action, see 37 CFR 1.113(c). A request for reconsideration while not provided for in 37 CFR 1.113(c) may be filed after final for consideration. See MPEP §§ 706.07(e) and 714.13. The USPTO Internet website contains terminal disclaimer forms which may be used. Please visit www.uspto.gov/patent/patents-forms. The actual filing date of the application in which the form is filed determines what form (e.g., PTO/SB/25, PTO/SB/26, PTO/AIA /25, or PTO/AIA /26) should be used. A web-based eTerminal Disclaimer may be filled out completely online using web-screens. An eTerminal Disclaimer that meets all requirements is auto-processed and approved immediately upon submission. For more information about eTerminal Disclaimers, refer to www.uspto.gov/patents/apply/applying-online/eter minal-disclaimer. Claims 1-8, and 9 are rejected on the ground of nonstatutory double patenting as being unpatentable over the claims of U.S. Application No. 18439780. Although the claims at issue are not identical, they are not patentably distinct from each other because the claims share the following limitations: Instant Application: 18657507 Conflicting application: 18908434 Claim 1: An electric machine { fluid cooling system, comprising: an air vent in fluidic communication with a radial coolant passage; a rotor shaft coolant passage that extends through a rotor shaft; and an inlet coolant passage that is positioned in a rotor shaft; wherein the radial coolant passage is in fluidic communication with: the rotor shaft coolant passage; and the inlet coolant passage. } 1 Claim 9: The electric machine fluid cooling system of claim 1, { wherein the radial coolant passages are inlet radial coolant passages and the electric machine fluid cooling system further comprises outlet radial coolant passages that are fluidly connected to the inlet radial coolant passages via axial coolant passages and wherein the inlet radial coolant passages and the outlet radial coolant passages are symmetric. } 2 Claim 10: The electric machine fluid cooling system of claim 1, { wherein a central axis of the air vent is parallel to a rotational axis of a rotor.} 3 Claim 1: A shaft { fluid cooling system, comprising: one or more air vents in fluidic communication with one or more radial cooling passages;}wherein the one or more radial cooling passages are in fluidic communication with: one or more rotor shaft cooling passages that extend axially through a rotor shaft; and an inlet cooling passage that extends through the rotor shaft. } 1 Claim 5: The shaft fluid cooling system of claim 1, { wherein the one or more radial cooling passages comprise one or more inlet side radial cooling passages and one or more outlet side radial cooling passages, wherein the one or more inlet side radial cooling passages and the one or more outlet side radial cooling passages are symmetric. } 2 Claim 13: The method of claim 12, { wherein: a central axis of the air vent is parallel to a rotational axis of a rotor; } 3 and {a central axis of the inlet coolant passage is coaxial to the rotational axis of the rotor. } 6 Claim 16: An electric machine { fluid cooling system, comprising: a plurality of air vents in direct fluidic communication with a plurality of radial coolant passages; wherein the plurality of radial coolant passages are each in direct fluidic communication with one of a plurality of rotor shaft coolant passages; wherein each of the plurality of radial coolant passages are in direct fluidic communication with an inlet coolant passage;} 4 and wherein each of the plurality of radial coolant passages are in direct fluidic communication with an outlet coolant passage. Claim 17: The electric machine { fluid cooling system of claim 16, wherein the plurality of radial coolant passages are equally spaced with regard to a radial plane. } 5 Claim 18: The electric machine fluid cooling system of claim 16, { wherein: a central axis of the plurality of air vents are parallel to a rotational axis of a rotor;} 3 {a central axis of the inlet coolant passage is coaxial to the rotational axis of the rotor;} 6 and a central axis of the outlet coolant passage is coaxial to the rotational axis of the rotor. Claim 10: An electric machine { fluid cooling system, comprising: one or more air vents in direct fluidic communication with a plurality of radial cooling passages, wherein the plurality of radial cooling passages are each in direct fluidic communication with one of a plurality of rotor shaft cooling passages and wherein each of the plurality of radial cooling passages are in direct fluidic communication with an inlet cooling passage.} 4 Claim 11: The electric machine { fluid cooling system of claim 10, wherein the plurality of radial cooling passages are equally spaced with regard to a radial plane. } 5 Claim 15: The method of claim 13, wherein the one or more radial cooling passages are Claim Rejections - 35 USC § 103 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) 1, 2, 9-13, and 16-18 are rejected under 35 U.S.C. 103 as being unpatentable over Weidman (US 6772504 B2) in view of Huber (US 4026315 A). Claim 1 As for claim 1, Weidman teaches: An electric machine fluid cooling system, comprising: a radial coolant passage (passage extending from pump 148 into 112 and 138); a rotor shaft (108) coolant passage (108b) that extends through a rotor shaft (108); and an inlet coolant passage (112) that is positioned in a rotor shaft (108); wherein the radial coolant passage (passage extending from pump 148 into 112 and 138) is in fluidic communication with: the rotor shaft (108) coolant passage (108b); and the inlet coolant passage (112). PNG media_image1.png 792 526 media_image1.png Greyscale \ Weidman is silent to: an air vent in fluidic communication with a radial coolant passage; Huber conversely teaches an air ventilation system for a rotating cooling system including inlet openings (11’/12’/13’) positioned near the axis of rotation where air accumulates, a bypass/vent path (11/12/13) that transports air or gas bubbles, an outlet structure (11”/12”/13”) that vents the air into another flow passage (e.g. a discharge duct 4), and specifically describes radial ducts (9) adjacent to axial ducts (1) in a rotating coolant system. Huber also teaches that air or gas bubbles naturally accumulate at low-pressure (para. 7) near the rotational axis, and teaches providing a vent path (bypass) in fluidic communication with coolant passages removes such air to prevent overheating and flow blockage (para. 33). PNG media_image2.png 792 452 media_image2.png Greyscale PNG media_image3.png 380 472 media_image3.png Greyscale It would have been obvious to a person of ordinary skill in the art (PHOSITA) during the time of the claimed invention to modify the cooling system of Weidman to include an air vent in fluidic communication with the radial coolant passage as taught by Huber. A PHOSITA would recognize that the cooling system of Weidman, which includes rotating coolant passages (including radial passages), would be subject to the same problem of trapped air or gas bubbles causing localized overheating and flow blockage as taught by Huber. Incorporating an air vent to be in fluidic communication with a radial coolant passage would be advantageous since doing so ensures effective removal of air throughout the system to improve cooling efficiency, prevent overheating, and enhance reliability of the rotating electric machine. Claim 2/1 The electric machine fluid cooling system of claim 1, wherein the air vent (11/12/13 of Huber modified into Weidman’s rotor shaft 108) is in fluidic communication with a cavity (108b) that is positioned radially inward from a rotor shaft bearing (104). Claim 9/1 The electric machine fluid cooling system of claim 1, wherein the radial coolant passages (passage extending from pump 148 into 112 and 138) are inlet radial coolant passages and the electric machine fluid cooling system further comprises outlet radial coolant passages (138b and passage from 111 to heat exchanger 150) that are fluidly connected to the inlet radial coolant passages (138 and passage from pump 148 to 112) via axial coolant passages (124, 126) and wherein the inlet radial coolant passages (138 and passage from pump 148 to 112) and the outlet radial coolant passages (138b and passage from 111 to heat exchanger 150) are symmetric (at least 138a and 138b). Claim 10/1 The electric machine fluid cooling system of claim 1, wherein a central axis (symmetrical axis parallel to rotation) of the air vent (11/12/13; Huber) is parallel to a rotational axis of a rotor (110; Huber). Claim 11/1 The electric machine fluid cooling system of claim 1, wherein a central axis (19; Huber) of the air vent (11/12/13; Huber) is angled (90 degrees) in relation to a rotational axis of a rotor (110; Huber). Claim 12 As for claim 12, Weidman teaches: A method for operation of an electric machine fluid cooling system (100), comprising: an inlet coolant passage (112); wherein the electric machine fluid cooling system includes: a rotor shaft (108) coolant passage (108b) that extends through a rotor shaft (108); and an inlet coolant passage (112) that is positioned in a rotor shaft (108); wherein the radial coolant passage (passage extending from pump 148 into 112 and 138) is in fluidic communication with: the rotor shaft (108) coolant passage (108b); and that extends through a rotor shaft (108); and the inlet coolant passage (112). PNG media_image1.png 792 526 media_image1.png Greyscale Weidman is silent to: an air vent in fluidic communication with a radial coolant passage; Huber conversely teaches an air ventilation system for a rotating cooling system including inlet openings (11’/12’/13’) positioned near the axis of rotation where air accumulates, a bypass/vent path (11/12/13) that transports air or gas bubbles, an outlet structure (11”/12”/13”) that vents the air into another flow passage (e.g. a discharge duct 4), and specifically describes radial ducts (9) adjacent to axial ducts (1) in a rotating coolant system. Huber also teaches that air or gas bubbles naturally accumulate at low-pressure (para. 7) near the rotational axis, and teaches providing a vent path (bypass) in fluidic communication with coolant passages removes such air to prevent overheating and flow blockage (para. 33). PNG media_image2.png 792 452 media_image2.png Greyscale PNG media_image3.png 380 472 media_image3.png Greyscale It would have been obvious to a person of ordinary skill in the art (PHOSITA) during the time of the claimed invention to modify the cooling system of Weidman to include an air vent in fluidic communication with the radial coolant passage as taught by Huber. A PHOSITA would recognize that the cooling system of Weidman, which includes rotating coolant passages (including radial passages), would be subject to the same problem of trapped air or gas bubbles causing localized overheating and flow blockage as taught by Huber. Incorporating an air vent to be in fluidic communication with a radial coolant passage would be advantageous since doing so ensures effective removal of air throughout the system to improve cooling efficiency, prevent overheating, and enhance reliability of the rotating electric machine. Claim 13/12 The method of claim 12, wherein: a central axis (symmetrical axis parallel to rotation) of the air vent (11/12/13; Huber) is parallel to a rotational axis of a rotor (110; Huber); and a central axis (19; Huber) of the inlet coolant passage is coaxial to the rotational axis of the rotor (110; Huber). Claim 16 As for claim 16, Weidman teaches: An electric machine fluid cooling system (100), comprising: a plurality of radial coolant passages (passage extending from pump 148 into 112 and 138) wherein the plurality of radial coolant passages (passage extending from pump 148 into 112 and 138) are each in direct fluidic communication with one of a plurality of rotor shaft (108) coolant passages (108b); wherein each of the plurality of radial coolant passages (passage extending from pump 148 into 112 and 138) are in direct fluidic communication with an inlet coolant passage (112); and wherein each of the plurality of radial coolant passages (passage extending from pump 148 into 112 and 138) are in direct fluidic communication with an outlet coolant passage (passage extending from 111 to heat exchanger and 111). PNG media_image1.png 792 526 media_image1.png Greyscale Weidman is silent however to teaching: a plurality of air vents in direct fluidic communication with a plurality of radial coolant passages; Huber conversely teaches an air ventilation system for a rotating cooling system including inlet openings (12’/13’) positioned near the axis of rotation where air accumulates, a bypass/vent path (12/13) that transports air or gas bubbles, an outlet structure (12”/13”) that vents the air into another flow passage (e.g. a discharge duct 4), and specifically describes radial ducts (9) adjacent to axial ducts (1) in a rotating coolant system. Huber also teaches that air or gas bubbles naturally accumulate at low-pressure (para. 7) near the rotational axis, and teaches providing a vent path (bypass) in fluidic communication with coolant passages removes such air to prevent overheating and flow blockage (para. 33). PNG media_image2.png 792 452 media_image2.png Greyscale PNG media_image3.png 380 472 media_image3.png Greyscale It would have been obvious to a person of ordinary skill in the art (PHOSITA) during the time of the claimed invention to modify the cooling system of Weidman to include plurality of air vents in direct fluidic communication with a plurality of radial coolant passages. A PHOSITA would recognize that the cooling system of Weidman, which includes rotating coolant passages (including radial passages), would be subject to the same problem of trapped air or gas bubbles causing localized overheating and flow blockage as taught by Huber. Incorporating an air vent to be in fluidic communication with a radial coolant passage would be advantageous since doing so ensures effective removal of air throughout the system to improve cooling efficiency, prevent overheating, and enhance reliability of the rotating electric machine. Claim 17/16 The electric machine fluid cooling system of claim 16, wherein the plurality of radial coolant passages (passage extending from pump 148 into 112 and 138) are equally spaced with regard to a radial plane. Claim 18/16 The electric machine fluid cooling system of claim 16, wherein: a central axis of the plurality of air vents (12/13; Huber) are parallel to a rotational axis of a rotor (110; Huber); a central axis (19; Huber) of the inlet coolant passage is coaxial to the rotational axis of the rotor; and a central axis (19; Huber) of the outlet coolant passage is coaxial to the rotational axis of the rotor (110; Huber). Claim(s) 7-8, and 15 are rejected under 35 U.S.C. 103 as being unpatentable over Weidman as modified by Huber in view of Daimler (DE 29924452 U1). Claim 7/1 The electric machine fluid cooling system of claim 1, but is silent to teaching: further comprising an outlet coolant passage in fluidic communication with a gearbox. Daimler conversely teaches an electric machine (1) comprising a fluid cooling system, wherein the electric machine (1) further comprises of outlet coolant passages (5, 14, and 16) in fluidic communication with a gearbox (2). PNG media_image4.png 732 1006 media_image4.png Greyscale PNG media_image5.png 712 894 media_image5.png Greyscale A person having ordinary skill in the art (PHOSITA) would have found it obvious to further modify Weidman as modified by Huber to include an outlet coolant passage in fluidic communication with a gearbox, as taught by Daimler, because integrating cooling systems across mechanically coupled components is a well-established design consideration in the art. Daimler demonstrates that routing coolant to a gearbox provides predictable benefits, such as improved heat dissipation, enhanced lubrication performance, and increased overall system reliability. A PHOSITA would have been motivated to implement such a modification to optimize thermal efficiency and reduce component wear in systems where an electric machine is operatively coupled to a gearbox. Claim 8/7/1 The electric machine fluid cooling system of claim 7, wherein an electric machine housing (3; Daimler) is directly coupled to a gearbox housing (4; Daimler). Claim 15/12 The method of claim 12, but is silent to: further comprising flowing coolant from an outlet coolant passage to a gearbox, wherein the outlet coolant passage is included in the electric machine fluid cooling system. Daimler conversely teaches an electric machine (1) comprising a fluid cooling system, wherein the electric machine (1) further comprises of outlet coolant passages (5, 14, and 16) in fluidic communication with a gearbox (2). PNG media_image4.png 732 1006 media_image4.png Greyscale PNG media_image5.png 712 894 media_image5.png Greyscale A person having ordinary skill in the art (PHOSITA) would have found it obvious to further modify Weidman as modified by Huber to include an outlet coolant passage in fluidic communication with a gearbox, as taught by Daimler, because integrating cooling systems across mechanically coupled components is a well-established design consideration in the art. Daimler demonstrates that routing coolant to a gearbox provides predictable benefits, such as improved heat dissipation, enhanced lubrication performance, and increased overall system reliability. A PHOSITA would have been motivated to implement such a modification to optimize thermal efficiency and reduce component wear in systems where an electric machine is operatively coupled to a gearbox. Allowable Subject Matter Claims 3-6, 14, and 19-20 are objected to as being dependent upon rejected base claims, but would be allowable if rewritten in independent form including all of the limitations of the base claims and any intervening claims. Claim 3/2/1 Claim 3 is allowed. The following is a statement of reasons for the indication of allowable subject matter: As for claim 3, Weidman as modified by Huber teaches: The electric machine fluid cooling system of claim 2; The prior art fails to teach or fairly suggest, alone or in obvious combination, inter alia: a bearing nozzle that extends from the cavity to a bearing cavity that is axially adjacent to the rotor shaft bearing. 3. Claims 4-6 stand allowed over all prior art based on their virtue of depending on claim 3. 4. Any comments considered necessary by applicant must be submitted no later than the payment of the issue fee and, to avoid processing delays, should preferably accompany the issue fee. Such submissions should be clearly labeled “Comments on Statement of Reasons for Allowance.” Claim 14/12 Claim 14 is allowed. The following is a statement of reasons for the indication of allowable subject matter: As for claim 14, Weidman as modified by Huber teaches: The method of claim 12; The prior art fails to teach or fairly suggest, alone or in obvious combination, inter alia: the electric machine fluid cooling system further includes a bearing nozzle that extends from a cavity to a bearing cavity that is axially adjacent to a rotor shaft bearing; and the bearing nozzle is radially aligned. 3. Any comments considered necessary by applicant must be submitted no later than the payment of the issue fee and, to avoid processing delays, should preferably accompany the issue fee. Such submissions should be clearly labeled “Comments on Statement of Reasons for Allowance.” Claim 19/16 Claim 19 is allowed. The following is a statement of reasons for the indication of allowable subject matter: As for claim 19, Weidman as modified by Huber teaches: The electric machine fluid cooling system of claim 16; The prior art fails to teach or fairly suggest, alone or in obvious combination, inter alia: a bearing nozzle that extends from a cavity to a bearing cavity that is axially adjacent to a rotor shaft bearing. 3. Claim 20 stands allowed over all prior art based on their virtue of depending on claim 19. 4. Any comments considered necessary by applicant must be submitted no later than the payment of the issue fee and, to avoid processing delays, should preferably accompany the issue fee. Such submissions should be clearly labeled “Comments on Statement of Reasons for Allowance.” Conclusion Any inquiry concerning this communication or earlier communications from the examiner should be directed to AHMED F SECK whose telephone number is (571)272-4638. The examiner can normally be reached Monday - Friday 7:30 am - 4:30 pm. 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, Christopher Koehler can be reached at (571) 272-3560. 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. /AHMED F SECK/Examiner, Art Unit 2834 /CHRISTOPHER M KOEHLER/Supervisory Patent Examiner, Art Unit 2834
Read full office action

Prosecution Timeline

May 07, 2024
Application Filed
Apr 06, 2026
Non-Final Rejection mailed — §103 (current)

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Prosecution Projections

1-2
Expected OA Rounds
69%
Grant Probability
87%
With Interview (+18.5%)
2y 11m (~11m remaining)
Median Time to Grant
Low
PTA Risk
Based on 103 resolved cases by this examiner. Grant probability derived from career allowance rate.

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