Prosecution Insights
Last updated: July 17, 2026
Application No. 18/281,744

MULTI-TUBE VIBRATION DAMPER HAVING ADJUSTABLE DAMPING FORCE FOR A VEHICLE

Final Rejection §103
Filed
Sep 12, 2023
Priority
Mar 12, 2021 — DE 10 2021 202 418.1 +1 more
Examiner
HSIAO, JAMES K
Art Unit
3616
Tech Center
3600 — Transportation & Electronic Commerce
Assignee
thyssenkrupp AG
OA Round
2 (Final)
77%
Grant Probability
Favorable
3-4
OA Rounds
3m
Est. Remaining
92%
With Interview

Examiner Intelligence

Grants 77% — above average
77%
Career Allowance Rate
612 granted / 796 resolved
+24.9% vs TC avg
Strong +15% interview lift
Without
With
+15.1%
Interview Lift
resolved cases with interview
Typical timeline
3y 1m
Avg Prosecution
29 currently pending
Career history
826
Total Applications
across all art units

Statute-Specific Performance

§101
0.8%
-39.2% vs TC avg
§103
57.0%
+17.0% vs TC avg
§102
17.4%
-22.6% vs TC avg
§112
4.5%
-35.5% vs TC avg
Black line = Tech Center average estimate • Based on career data from 796 resolved cases

Office Action

§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 . 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. Claims 7,8, 11, and 12 are rejected under 35 U.S.C. 103 as being unpatentable over Schmidt (US-20210062887) in view of Pancaldi (EP-1953394). It is noted that Pancaldi (EP-1953394) is in English and has been referred to below directly. Regarding claim 7, Schmidt discloses a multi-tube vibration damper (10) for a vehicle having adjustable damping (via 342), comprising: a damper inner tube (12/38) at least filled partially with a damping medium, and including a damper inner tube wall, wherein the damper inner tube wall includes a damper inner tube inner face and a damper inner tube outer face (fig 2, at least the inner periphery of 12 and/or 38); a piston rod (14) arranged movably within the damper inner tube (fig 1); a working piston (16) arranged movable together with the piston rod, by means of which an interior of the damper inner tube is divided into a working chamber on the piston rod side (221) and a working chamber remote from the piston rod (222); a damper outer tube (28) having a damper outer tube wall, wherein the damper outer tube is arranged coaxially around the damper inner tube (figs 1-2), and a compensation chamber (30) is defined between the damper outer tube and the damper inner tube; a damping module (342) having a connecting piece (46), wherein the damping module is arranged on the outside of the damper outer tube wall (fig 2), and the connecting piece (46) runs fluid-tightly from the damping module through a damper outer tube wall opening (fig 2) configured for creating a fluid connection between the working chamber (222) remote from the piston rod and the damping module (342) and configured to open fluid-tightly into a damper inner tube wall opening (42); and a conduit (42/44), wherein the conduit (42/44) protrudes into the interior of the damper inner tube and opens into the interior of the damper inner tube in the damper inner tube wall opening (fig 2), wherein the connecting piece is arranged coaxially inside the conduit (fig 2). Schmidt discloses wherein a flow connection or conduit may be guided by way of an adapter sleeve (38) which is inserted in the inner cylinder but lacks wherein the conduit is formed integrally from the damper wall. Pancaldi teaches wherein there is a provision for a kind of shock absorber which entails providing a hole in a cylinder/tube wall (2), arranging respective sleeves (19/7), welding them (20, fig 2), and connecting by means of the duct ([0011]). Pancaldi also teaches an improvement in order to avoid delicate points and improve manufacturing costs through a reduction of parts and operation ([0011-0016]). Pancaldi teaches a manufacturing technique of the cylinder wherein “flowdrilling” is used to produce an inwardly projecting conduit (7), collar (21), and bush (22) (fig 3). The conduit (7/22/21) formed integrally from a damper tube (2) wall ([0030-0031]), wherein the conduit protrudes into the interior of the damper inner tube (2) and opens into the interior of the damper inner tube in the damper inner tube wall opening (fig 3), wherein a connecting piece (23) is arranged coaxially inside the conduit (fig 3). It would have been obvious to one of ordinary skill in the art before the effective filing date of the claimed invention to substitute the flow connection of an adapter sleeve of Schmidt with the “flowdrilled” conduit of Pancaldi at least in order to reduce production and manufacturing cost while improving durability and function (Pancaldi [0010-0016]). Regarding claim 7, the combination of Schmidt and Pancaldi as set forth above teaches wherein a geometric transition structure (Pancaldi, fig 3 at least the transition from the wall to 22) is formed in between the damper inner tube wall and the conduit, wherein the geometric transition includes a bulge into the compensation chamber, (Pancaldi, fig 3, 22 bulging into 4, and [0031] at least the result of “flowdrilling”, wherein the rest of the material forms a bush 22 in the intrados of the part being machined. The resulting collar 21 and bush 22 can be even thicker than the original material). It would have been obvious to one of ordinary skill in the art before the effective filing date of the claimed invention to include a bulge into the chamber as the flowdrilling that forms the bulge produces an increased strength at the junction (Pancaldi, [0031, the assembly constituted by the collar 21 and the bush 22 thus provided is very tough and strong, and it is also possible to use installations which provide very intense mechanical stresses.) Regarding claim 8, the combination of Schmidt and Pancaldi as set forth above teaches wherein the damper inner tube wall opening is cylindrical (22), including a cylindrical edge (Pancaldi, fig 3). Regarding claim 11, the combination of Schmidt and Pancaldi as set forth above teaches wherein the geometric transition structure includes as a stepped profile (Pancaldi, fig 3, 22, wherein the flat portion of 22 adjacent the cylinder wall has been interpreted as stepped to the opening 7). Regarding claims 8-11, it would have been obvious to one of ordinary skill in the art before the effective filing date of the claimed invention to substitute the flow connection of an adapter sleeve of Schmidt with the “flowdrilled” conduit of Pancaldi at least in order to reduce production and manufacturing cost while improving durability and function (Pancaldi [0010-0016]). Regarding claim 12, Schmidt discloses wherein the, connecting piece (46) opening into the damper inner tube wall opening is sealed against the damper inner tube outer face (at least an outer periphery of 12/38 which includes 44) by means of a sealing ring (48) in the mouth region. Response to Arguments Applicant's arguments filed 3/4/2026 have been fully considered but they are not persuasive. Regarding claim 7, Applicant argues that the prior art of record lacks “wherein a geometric transition structure is formed in between the cylindrical damper inner tube wall and the conduit, wherein the geometric transition structure includes a bulge into the compensation chamber”, Examiner respectfully disagrees. As set forth above, Pancaldi ([0031]) teaches wherein a geometric transition structure is formed through heat-flow drilling (or flow-drilling). The heat generated by friction softens the material: the resulting malleability ensures the possibility to provide a hole without chip-forming, but merely by transferring material from one region to another. While the tool acts on the material, part of the tool forms a collar 21 around the upper surface of the part being machined. The rest of the material forms a bush 22 in the intrados of the part being machined. The resulting collar 21 and bush 22 can be even thicker than the original material. As seen in at least fig 3, it has been interpreted that element 22 bulges into the chamber 4 . Conclusion THIS ACTION IS MADE FINAL. 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 JAMES K HSIAO whose telephone number is (571)272-6259. The examiner can normally be reached 9-5, Monday-Friday. 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, Robert Siconolfi can be reached at 571-272-7124. 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. /J.K.H/Examiner, Art Unit 3616 /Robert A. Siconolfi/Supervisory Patent Examiner, Art Unit 3616
Read full office action

Prosecution Timeline

Sep 12, 2023
Application Filed
Dec 16, 2025
Non-Final Rejection mailed — §103
Mar 04, 2026
Response Filed
Jun 02, 2026
Final Rejection mailed — §103 (current)

Precedent Cases

Applications granted by this same examiner with similar technology

Patent 12679495
BICYCLE SUSPENSION COMPONENTS
5y 6m to grant Granted Jul 14, 2026
Patent 12680593
VALVE AND SHOCK ABSORBER
3y 0m to grant Granted Jul 14, 2026
Patent 12650154
DAMPING-VALVE DEVICE WITH A PROGRESSIVE DAMPING-FORCE CHARACTERISTIC CURVE
2y 10m to grant Granted Jun 09, 2026
Patent 12643363
ADJUSTMENT ASSEMBLY FOR COMPENSATING A LENGTH VARIATION OF A SPRING ELEMENT AND WHEEL SUSPENSION ASSEMBLY FOR A VEHICLE
3y 1m to grant Granted Jun 02, 2026
Patent 12637205
AIRCRAFT LANDING GEAR TORQUE LINK ASSEMBLY
2y 8m to grant Granted May 26, 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

3-4
Expected OA Rounds
77%
Grant Probability
92%
With Interview (+15.1%)
3y 1m (~3m remaining)
Median Time to Grant
Moderate
PTA Risk
Based on 796 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