Prosecution Insights
Last updated: April 19, 2026
Application No. 18/990,756

COMPRESSOR AND REFRIGERATION CYCLE DEVICE

Non-Final OA §102§103
Filed
Dec 20, 2024
Examiner
DAVIS, MARY ALICE
Art Unit
3746
Tech Center
3700 — Mechanical Engineering & Manufacturing
Assignee
Carrier Japan Corporation
OA Round
1 (Non-Final)
77%
Grant Probability
Favorable
1-2
OA Rounds
2y 10m
To Grant
99%
With Interview

Examiner Intelligence

Grants 77% — above average
77%
Career Allow Rate
718 granted / 929 resolved
+7.3% vs TC avg
Strong +32% interview lift
Without
With
+32.3%
Interview Lift
resolved cases with interview
Typical timeline
2y 10m
Avg Prosecution
26 currently pending
Career history
955
Total Applications
across all art units

Statute-Specific Performance

§101
0.5%
-39.5% vs TC avg
§103
36.4%
-3.6% vs TC avg
§102
27.4%
-12.6% vs TC avg
§112
26.6%
-13.4% vs TC avg
Black line = Tech Center average estimate • Based on career data from 929 resolved cases

Office Action

§102 §103
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 . DETAILED ACTION 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. CLAIM INTERPRETATION The presence of claim limitations that are preceded by the phrases “wherein” often raises a question as to the limiting effect of the claim limitations (see MPEP §2111.04). The Examiner has interpreted the limitations following the phrase “wherein” as positively being claimed (i.e. the claim limitations are required and/or the claim limitations following the “wherein clause” limits the structure), where “wherein” is being used as a transitional phrase. Election/Restrictions Applicant’s election without traverse of Species I and Sub-Species B in the reply filed on February 2, 2026 is acknowledged. Claims 6 and 8 are withdrawn from further consideration pursuant to 37 CFR 1.142(b) as being drawn to a nonelected species. Claim 7 is withdrawn with respect to depending on claim 6. Election was made without traverse in the reply filed on February 2, 2026. Restriction requirement is made FINAL. Specification The title of the invention is not descriptive. A new title is required that is clearly indicative of the invention to which the claims are directed. The following title is suggested: COMPRESSOR WITH INJECTION FLOW INTO THE COMPRESSION CHAMBER AND REFRIGERATION CYCLE DEVICE. 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. Claims 1-3, 5, 7, and 9 are rejected under 35 U.S.C. 102(a)(1) as being anticipated by JP ‘210 (Japanese Patent Publication JP 52-063210 U, a machine translation was provided in the IDS filed on December 20, 2024 and is utilized in the rejection below). Regarding claim 1, JP ‘210 discloses: a compressor (see Figures 2 and 3 and claim that recites a compressor), comprising: an annular cylinder (8) (see Figures 2 and 3), which constitutes a cylinder chamber (13, 14) including a suction chamber (13) for sucking a refrigerant and a compression chamber (14) for compressing the refrigerant (see Figure 3, Page 2); a rotation shaft (see Marked up Figures 2 and 3 of JP’210), which includes an eccentric portion (see Marked up Figure 2 of JP’210) arranged in the cylinder chamber (see Marked up Figures 2 and 3 of JP’210); a roller (9), which is fitted into the eccentric portion and eccentrically rotates with respect to a center of axis of the rotation shaft in the cylinder chamber (see Figures 2 and 3); a flat blade (15), which advances or retracts in the cylinder chamber according to an eccentric rotation of the roller and partitions the cylinder chamber into the suction chamber (13) and the compression chamber (14) (see Figure 3, and claim); and an injection flow channel (5, 18) branching from a cyclic circuit (see Figure 1, that shows the injection flow channel branching from a cyclic circuit), through which the refrigerant circulates (see Figure 1, and Page 2), and guiding a part of the refrigerant circulating through the cyclic circuit to the compression chamber (see Figure 1, and Page 2, where the refrigerant enters the compression chamber via (5)), wherein the injection flow channel includes at least a blade groove (18) formed in a surface portion facing the compression chamber (see Figure 3), of side surface portions constituting a pair on the blade (see Marked up Figure 3 that shows that there are side surface portions that are a pair on the blade) and facing a circumferential direction with respect to the center of axis of the rotation shaft (see Figure 3), and a surface on which the part of the refrigerant flows into the blade groove is flush with a surface discharging the part of the refrigerant from the blade groove to the compression chamber (see Figure 3). PNG media_image1.png 309 578 media_image1.png Greyscale PNG media_image2.png 479 690 media_image2.png Greyscale Regarding claim 2, JP ‘210 discloses: a compressor (see Figures 2 and 3 and claim that recites a compressor), comprising: an annular cylinder (8) (see Figures 2 and 3), which constitutes a cylinder chamber (13, 14) including a suction chamber (13) for sucking a refrigerant and a compression chamber (14) for compressing the refrigerant (see Figure 3, Page 2); a rotation shaft (see Marked up Figures 2 and 3 of JP’210), which includes an eccentric portion (see Marked up Figure 2 of JP’210) arranged in the cylinder chamber (see Marked up Figures 2 and 3 of JP’210); a roller (9), which is fitted into the eccentric portion and eccentrically rotates with respect to a center of axis of the rotation shaft in the cylinder chamber (see Figures 2 and 3); a substantially flat blade (15), which advances or retracts in the cylinder chamber according to an eccentric rotation of the roller and partitions the cylinder chamber into the suction chamber (13) and the compression chamber (14) (see Figure 3, and claim), wherein the cylinder and the blade include an injection flow channel (see Marked up Figure 3 of JP’210) branching from a cyclic circuit (see Figure 1, that shows the injection flow channel branching from a cyclic circuit), through which the refrigerant circulates (see Figure 1, and Page 2), and guiding a part of the refrigerant circulating through the cyclic circuit to the compression chamber (see Figure 1, and Page 2, where the refrigerant enters the compression chamber via (5)), the cylinder includes: a blade hole (see Marked up Figure 3 of JP’210), which is open to an inner peripheral part (see Marked up Figure 3 of JP’210), extends outwardly along a diameter direction, and accommodates the blade (see Marked up Figure 3 of JP’210); a spring (11) (see Marked up Figure 3 of JP’210), which presses the blade against the roller in the blade hole (see Figure 3, see claim); and a spring insertion hole (see Marked up Figure 3 of JP’210) in which the spring is arranged (see Marked up Figure 3 of JP’210), the injection flow channel includes: a blade groove (see Marked up Figure 3 of JP’210) formed in a groove shape (see Marked up Figure 3 of JP’210 that shows the blade groove is in a groove shape) in a surface portion facing the compression chamber (see Marked up Figure 3 of JP’210), of side surface portions (see Marked up Figure 3 of JP’210) constituting a pair on the blade (see Marked up Figure 3 of JP’210) and facing a circumferential direction with respect to the center of axis of the rotation shaft (see Figure 3); and a cylinder flow channel (see Marked up Figure 3 of JP’210) open to be communicable with the blade groove on a wall portion opposed to the surface portion facing the compression chamber of the blade in the blade hole (see Marked up Figure 3 of JP’210), and the blade groove is arranged on the surface portion facing the compression chamber of the blade (see Marked up Figure 3 of JP’210) so as not to overlap with the spring insertion hole in the circumferential direction (see Figure 3. The Examiner would like to note that negative limitations do not have to be specifically recited in the prior art, but the prior art has to only show that the claimed negative feature is not there. In Figure 3 the spring insertion hole does not show that it overlaps in the circumferential direction). Regarding claim 3, JP ‘210 discloses: an end portion in a retraction side of the blade in the blade groove does not reach an end surface portion in the retraction side of the blade (see Figure 3, where the Examiner would like to note that negative limitations do not have to be specifically recited in the prior art, but the prior art has to only show that the claimed negative feature is not there. JP’210 in Figure 3 appears that once in a retracted state a retraction side of the blade in the blade groove does not reach an end surface portion in the retraction side of the blade), and in a state where the blade is most retracted with respect to the cylinder chamber in the blade hole, the end portion is located closer to the center of axis of the rotation shaft than the spring insertion hole is (see Figure 3, the Examiner would like to note that the end portion of the blade (i.e. the tip) will always be closer to the center axis of rotation shaft than the spring insertion hole, since the spring insertion hole is at the base of the blade). Regarding claim 5, JP ‘210 discloses: the blade groove has a longitudinal side along an advancing/retracting direction in the blade hole (see Figure 2), and a groove cross-section area of the blade groove (18) intersecting a longitudinal direction is approximately constant over the entire longitudinal direction (see Figure 2, where it is constant over the entire longitudinal direction). Regarding claim 7, JP ‘210 discloses: the groove cross-section area of the blade groove (see Marked up Figure 2 of JP’210 that shows the groove cross-section area of the blade groove (length width), where the width is smaller than the aperture) is smaller than or equal to an aperture area of the aperture in the cylinder flow channel in the wall portion of the blade (see Marked up Figure 2 of JP’210 that shows groove cross-section area is smaller than the aperture area since the aperture area is the length times the width of the aperture. The Examiner would like to note that in addition to the aperture area including the wide section being wider and longer than the groove, the aperture also includes the smaller aperture that is connected to the larger aperture, that also has an area. The area of the entire aperture in the cylinder flow channel is larger than the groove. Since a single figure (Figure 2) appears to show the necessary relative dimensions of a the groove cross-section area of the blade groove is smaller than or equal to an aperture area of the aperture in the cylinder flow channel in the wall portion of the blade (see discussion above), it is deemed inherent, absent evidence to the contrary, that the groove cross-section area of the blade groove is indeed smaller or equal to the aperture area. See MPEP 2112, V). Regarding claim 9, JP ‘210 discloses: a refrigeration cycle device (see Figure 1), comprising: the compressor of any one of claims 1 and 2 (see discussion above); a condenser (2) connected to the compressor (1) (see Figure 1, Page 2); an expansion device (3) connected to the condenser (see Figure 1, Page 2); and an evaporator (4) (in Figure 1 the evaporator is labeled (5), however, Page 2 clarifies that the evaporator is connected to the expansion device and “sequentially connected to form a refrigeration cycle”) connected to the expansion device (see Figure 1, Page 2). 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 4 is rejected under 35 U.S.C. 103 as being unpatentable over JP ‘210 in view of MASAO (Chinese Patent Publication CN 104806522 A, a machine translation was provided with the foreign reference in the IDS filed on December 20, 2024 and is utilized in the rejection below). Regarding claim 4, JP ‘210 discloses: the claimed invention (see above), however, fails to disclose multiple cylinders (JP’210 is a single cylinder compressor), and therefore, fails to disclose the rotation shaft includes the plurality of eccentric portions equidistantly arranged in the circumferential direction at intervals in a direction of the center of axis, and the cylinder includes the plurality of cylinder chambers each accommodating one of the plurality of eccentric portions, and while the rotation shaft rotates once, the compression chamber, the blade groove, and the cylinder flow channel are in communication with each other at an angle range smaller than an equidistant angle of the plurality of eccentric portions. Regarding claim 4, MASAO teaches: the rotation shaft (see Marked up Figure 9 of MASAO) includes the plurality of eccentric portions (see Marked up Figure 9 of MASAO) equidistantly arranged in the circumferential direction at intervals in a direction of the center of axis (see Marked up Figure 9 of MASAO, ¶0046, ¶0048, since there are 2 cylinders they are offset by 180º), and the cylinder includes the plurality of cylinder chambers (33a, 33b) (see Figure 10) each accommodating one of the plurality of eccentric portions (see Figures 9 and 10), and while the rotation shaft rotates once, the compression chamber (33a), the blade groove (75a), and the cylinder flow channel (the cylinder flow channel is formed with (10)) are in communication with each other at an angle range smaller than an equidistant angle of the plurality of eccentric portions (see Figure 10 that shows at 180º the blade groove is closed, ¶0091-¶0094 discloses setting the coolant injection start and stop angles, since at 180º, which is the equidistant angle of the plurality of eccentric portions, since they are offset by 180º, is closed than it would be inherent that the cylinder flow channel are in communication with each other at an angle range smaller than an equidistant angle of the plurality of eccentric portions). It would have been obvious to a person having ordinary skill in the art at the time of the invention was made to have multiple cylinders wherein the rotation shaft includes the plurality of eccentric portions equidistantly arranged in the circumferential direction at intervals in a direction of the center of axis, and the cylinder includes the plurality of cylinder chambers each accommodating one of the plurality of eccentric portions, and while the rotation shaft rotates once, the compression chamber, the blade groove, and the cylinder flow channel are in communication with each other at an angle range smaller than an equidistant angle of the plurality of eccentric portions in the compressor of JP ‘210, in order to provide the desired output, where increasing the number of cylinders allows for an increase in output due to two cylinders are providing compression instead of just a single cylinder. PNG media_image3.png 560 805 media_image3.png Greyscale Additional Prior Art The prior art made of record and not relied upon is considered pertinent to applicant's disclosure. MORISHITA (Japanese Patent Publication JP 2012-251485 A) discloses a plurality of cylinders offset by 180º (see Figures 1 and 3) including an injection hole (146) and injection tube (144) (see Figures 3 and 4). Communication Any inquiry concerning this communication or earlier communications from the examiner should be directed to MARY DAVIS whose telephone number is (571)272-9965. The examiner can normally be reached M-F, 8 am-4pm. 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, Essama Omgba can be reached at (469) 295-9278. 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. /Mary A Davis/Primary Examiner, Art Unit 3746
Read full office action

Prosecution Timeline

Dec 20, 2024
Application Filed
Feb 21, 2026
Non-Final Rejection — §102, §103 (current)

Precedent Cases

Applications granted by this same examiner with similar technology

Patent 12590584
SUPERCHARGED INTERNAL COMBUSTION ENGINE WITH INTAKE PORT TIMING SHUTTERS CONTROLLING THE AIR MASS FLOWING INTO THE SUPERCHARGER
2y 5m to grant Granted Mar 31, 2026
Patent 12583003
DEVICES FOR DISPENSING FLUIDS
2y 5m to grant Granted Mar 24, 2026
Patent 12584483
PUMP AND METHOD TO ATTENUATE PULSES AT THE DISCHARGE
2y 5m to grant Granted Mar 24, 2026
Patent 12580443
FAN MOTOR COOLING
2y 5m to grant Granted Mar 17, 2026
Patent 12571394
SCROLL COMPRESSOR WITH BLOCKING PART FOR OIL SEPARATION
2y 5m to grant Granted Mar 10, 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
77%
Grant Probability
99%
With Interview (+32.3%)
2y 10m
Median Time to Grant
Low
PTA Risk
Based on 929 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