Prosecution Insights
Last updated: April 19, 2026
Application No. 18/383,856

SYSTEMS AND METHODS FOR REDUCING VIBRATIONAL DISTURBANCES

Non-Final OA §102
Filed
Oct 25, 2023
Examiner
JARRETT, RYAN A
Art Unit
2116
Tech Center
2100 — Computer Architecture & Software
Assignee
Nikon Corporation
OA Round
1 (Non-Final)
81%
Grant Probability
Favorable
1-2
OA Rounds
2y 10m
To Grant
88%
With Interview

Examiner Intelligence

Grants 81% — above average
81%
Career Allow Rate
695 granted / 861 resolved
+25.7% vs TC avg
Moderate +8% lift
Without
With
+7.7%
Interview Lift
resolved cases with interview
Typical timeline
2y 10m
Avg Prosecution
20 currently pending
Career history
881
Total Applications
across all art units

Statute-Specific Performance

§101
8.2%
-31.8% vs TC avg
§103
29.9%
-10.1% vs TC avg
§102
34.3%
-5.7% vs TC avg
§112
20.0%
-20.0% vs TC avg
Black line = Tech Center average estimate • Based on career data from 861 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 . 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)(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. Claims 21-45 are rejected under 35 U.S.C. 102(a)(2) as being anticipated by Pivac US 2021/0291362. Pivac discloses: 21. A system comprising: a vibration dampening module (e.g., Figs. 1A-1B: 142,143,111), wherein the vibration dampening module comprises an active vibration dampener (e.g., Figs. 5A-5C: #571,572, [0110]: “robot base 111 includes active members, each including a linear actuator 571...each having a mass 572”, Figs. 8A-8B: #871,872, [0117]: “linear actuators 871.1, 872.1 having masses 871.2, 872.2 mounted thereon”) and a passive vibration dampener (e.g., Figs. 8A-8B: #873-876, [0118]: “pairs of structural members 873-876…can be configured to provide passive damping”), wherein the vibration dampening module is coupled to a mechanical positioning system (e.g., Figs. 1A-1B: #141, Figs. 8A-8B: #141, [0112]: “boom base 141”) and a payload (e.g., Figs. 1A-1B: #112,113, [0061]: “robot arm 112 and an end effector 113”, [0122]: “Whilst a number of different damping mechanisms have been described independently, it will be appreciated that these could be used in combination. For example, this system could include damping arrangements in the robot base and in the boom, with combinations of different damping arrangements being used depending on the nature of the movement of the robot base”), and wherein the vibration dampening module is configured to operate in two or more different directions (e.g., [0110]-[0111]: “six degrees of freedom”). 22. The system of claim 21, wherein the active vibration dampener is configured to operate in three different directions (e.g., [0111]). 23. The system of claim 21, wherein the active vibration dampener is configured to operate in four different directions (e.g., [0111]). 24. The system of claim 21, wherein the active vibration dampener is configured to operate in five different directions (e.g., [0111]). 25. The system of claim 21, wherein the active vibration dampener is configured to operate in six different directions (e.g., [0111]). 26. The system of claim 21, wherein the active vibration dampener comprises an actuator (e.g., Figs. 5A-C: 571.1, 571.2, 571.3, [0110]: “linear actuator 571.1, 571.2, 571.3”). 27. The system of claim 26, wherein the actuator comprises one of a two-axis actuator, a three-axis actuator, a four-axis actuator, a five-axis actuator and a six-axis actuator (e.g., [0111]). 28. The system of claim 26, wherein the actuator comprises one of a two-axis piezoelectric actuator, a three-axis piezoelectric actuator, a four-axis piezoelectric actuator, a five-axis piezoelectric actuator and a six-axis piezoelectric actuator (e.g., [0111], [0245]). 29. The system of claim 21, wherein the active vibration dampener (e.g., Fig. 1 #142,143,111) is located between the mechanical positioning system (e.g., Fig. 1 #141) and the payload (e.g., Fig. 1 #112,113). 30. The system of claim 29, wherein the passive vibration dampener (e.g., Fig. 1 #142,143, Fig. 8A-8B #873-876) is located between the mechanical positioning system (e.g., Fig. 1 #141) and the payload (e.g., Fig. 1 #112,113). 31. The system of claim 21, wherein the vibration dampening module (e.g., Fig. 1A #142,143,111) is located between the mechanical positioning system (e.g., Fig. 1A #141) and the payload (e.g., Fig. 1 #112,113). 32. The system of claim 21, wherein the mechanical positioning system comprises a robotic system (e.g., Fig. 1 #141,142, [0112]: “boom base 141”, “boom 142”). 33. The system of claim 32, wherein the robotic system comprises a robotic arm (e.g., Fig. 1 #141,142, [0112]: “boom base 141”, “boom 142”). 34. The system of claim 21, wherein the payload comprises an optical system (e.g., [0245]). 35. The system of claim 34, wherein the optical system comprises a laser system (e.g., [0245]). 36. The system of claim 34, wherein the optical system comprises an optical manufacturing system (e.g., [0245]). 37. The system of claim 36, wherein the optical manufacturing system comprises a laser manufacturing system (e.g., [0245]). 38. The system of claim 21, wherein the payload comprises one of a manufacturing system, a metrology system, a positioning system and a robotic hand gripper (e.g., Fig. 1A). 39. The system of claim 21, wherein the active vibration dampener is configured to dampen vibrations of the payload characterized by a characteristic frequency of 30 Hertz (Hz) to 30 kilohertz (kHz) (e.g., [0065]). 40. The system of claim 21, wherein the passive vibration dampener is configured to dampen vibrations of the payload characterized by a characteristic frequency of at most 300 Hz (e.g., [0065]). 41. The system of claim 21, wherein the passive vibration dampener comprises an elastomeric material (e.g., [0118]). 42. The system of claim 21, wherein the active vibration dampener (e.g., Fig. 8A #872) is coupled to the mechanical positioning system (e.g., Fig. 8A #141) and the passive vibration dampener (e.g., Fig. 8A #873) is coupled to the payload (e.g., Fig. 8A #111). 43. The system of claim 21, wherein the active vibration dampener (e.g., Fig. 8A #871) is coupled to the payload (e.g., Fig. 8A #111) and the passive vibration dampener (e.g., Fig. 8A #874) is coupled to the mechanical positioning system (e.g., Fig. 8A #141). 44. The system of claim 21, further comprising: one or more sensors configured to measure one or more dynamical properties associated with at least one of the mechanical positioning system and the payload (e.g., [0098]); and one or more controllers configured to receive the one or more dynamical properties and to direct the active vibration dampener to compensate for vibrations of at least one of the mechanical positioning system and the payload based on the one or more dynamical properties (e.g., [0099]-[0101]). 45. The system of claim 44, wherein the one or more sensors comprise one or more members selected from the group consisting of: position sensors, velocity sensors, accelerometers, force sensors, and torque sensors (e.g., [0098]). Conclusion Any inquiry concerning this communication or earlier communications from the examiner should be directed to RYAN A JARRETT whose telephone number is (571)272-3742. The examiner can normally be reached M-F 9:00-5:30. 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, Kenneth Lo can be reached at 571-272-9774. 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. /RYAN A JARRETT/Primary Examiner, Art Unit 2116 02/05/26
Read full office action

Prosecution Timeline

Oct 25, 2023
Application Filed
Nov 27, 2023
Response after Non-Final Action
Feb 05, 2026
Non-Final Rejection — §102 (current)

Precedent Cases

Applications granted by this same examiner with similar technology

Patent 12596350
Linear Actuator Buckling Force Control
2y 5m to grant Granted Apr 07, 2026
Patent 12596356
METHOD AND SYSTEM FOR LOCALIZATION OF FAULTS IN AN INDUSTRIAL MANUFACTURING PLANT
2y 5m to grant Granted Apr 07, 2026
Patent 12593646
Automated Fault Detection in Microfabrication
2y 5m to grant Granted Mar 31, 2026
Patent 12591218
INDUSTRIAL DIGITAL TWIN MODEL ENVIRONMENT
2y 5m to grant Granted Mar 31, 2026
Patent 12591219
INDUSTRIAL INTERNET OF THINGS SYSTEMS FOR ABNORMAL ANALYSIS, METHODS, AND STORAGE MEDIUM THEREOF
2y 5m to grant Granted Mar 31, 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
81%
Grant Probability
88%
With Interview (+7.7%)
2y 10m
Median Time to Grant
Low
PTA Risk
Based on 861 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