Prosecution Insights
Last updated: July 17, 2026
Application No. 19/041,717

METHOD FOR REMOVING A METAL INSERT

Non-Final OA §102§103
Filed
Jan 30, 2025
Priority
Aug 02, 2022 — EU 22188214.5 +1 more
Examiner
WOLCOTT, BRIAN P
Art Unit
3711
Tech Center
3700 — Mechanical Engineering & Manufacturing
Assignee
Nordex Energy SE & Co. KG
OA Round
3 (Non-Final)
78%
Grant Probability
Favorable
3-4
OA Rounds
1y 4m
Est. Remaining
99%
With Interview

Examiner Intelligence

Grants 78% — above average
78%
Career Allowance Rate
452 granted / 583 resolved
+7.5% vs TC avg
Strong +30% interview lift
Without
With
+30.3%
Interview Lift
resolved cases with interview
Typical timeline
2y 10m
Avg Prosecution
38 currently pending
Career history
613
Total Applications
across all art units

Statute-Specific Performance

§101
0.2%
-39.8% vs TC avg
§103
73.4%
+33.4% vs TC avg
§102
10.4%
-29.6% vs TC avg
§112
15.4%
-24.6% vs TC avg
Black line = Tech Center average estimate • Based on career data from 583 resolved cases

Office Action

§102 §103
DETAILED ACTION Continued Examination Under 37 CFR 1.114 A request for continued examination under 37 CFR 1.114, including the fee set forth in 37 CFR 1.17(e), was filed in this application after final rejection. Since this application is eligible for continued examination under 37 CFR 1.114, and the fee set forth in 37 CFR 1.17(e) has been timely paid, the finality of the previous Office action has been withdrawn pursuant to 37 CFR 1.114. Applicant's submission filed on 3/11/2026 has been entered. Response to Arguments Claims 1 and 15 were amended. Claim 21 was added. Regarding the amendments to claims 1 and 15 Applicant argues the connecting layer of Caruso is not directly between the metal insert and the fibrous material in a radial direction of the wind turbine rotor blade part since Fig 6 and the corresponding description at Col 8, In. 32-33, only shows/describes element 64 as being disposed between 46 and 52 and not between 46 and 40 or 42. However, upon review of Col 8, In. 30-36, Caruso states "the root assembly 30 may also include a bonding agent 64 configured within the radial gap 44, e.g. between the various surfaces between the root inserts 46 and/or spacers 52. Thus the bonding agent 64 is configured to promote surface adhesion and/or resin transfer throughout the root assembly 30 during the manufacturing process." Examiner respectfully disagrees the bonding agent must be limited to the spaces between 46 and 52. It appears Caruso teaches using the bonding agent within the radial gap 44 between the various surfaces (i.e. all surfaces) of the root inserts and/or spacers to promote surface adhesion and/or resin transfer thought the root assembly. More specifically, it appears Caruso at least suggests applying a boding agent between the inner and/or outer radial surfaces of the insert and the fibrous material 40 and/or 42. Regarding added claim 21, Applicant argues Caruso teaches a process of removing an insert that differs from Applicant's claimed invention since according to Caruso the entirety of the insert 46 which includes the metal bushing would be removed. However, there is nothing in the claim that precludes more than metal bushing being removed during the removal process, further there is nothing the claims preventing the claimed "metal insert" to include non-metallic material. As such, it appears Caruso teaches the invention of claim 21 substantially as claimed. 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) 1, 2, 4-8, 10-12, 15 and 21 is/are rejected under 35 U.S.C. 102(a)(1) as anticipated by or, in the alternative, under 35 U.S.C. 103 as obvious over Caruso et al. (US 10060411), hereinafter: “Caruso”. In Regard to Claim 1 Caruso teaches: A method for removing a metal insert(46) from a wind turbine rotor blade part(16,32,40,42), the method comprising: providing the wind turbine rotor blade part(40,42; Col 10, ln. 22-42), the wind turbine rotor blade part including a fibrous composite material(Col 6, ln. 21-36) and the metal insert(46) held in the fibrous composite material(Fig 3), wherein the metal insert is configured to fasten the wind turbine rotor blade part to a wind turbine rotor hub(18) or to another wind turbine rotor blade part(the metal insert is structurally capable of fastening the wind turbine rotor blade to another wind turbine rotor blade part; Col 3, ln. 7-22), the wind turbine rotor blade further including a connecting layer(50,64) disposed directly between the metal insert and the fibrous composite material(Fig 3) in a radial direction of the wind turbine rotor blade part(Col 8, In. 30-36, states "the root assembly 30 may also include a bonding agent 64 configured within the radial gap 44, e.g. between the various surfaces between the root inserts 46 and/or spacers 52. Thus the bonding agent 64 is configured to promote surface adhesion and/or resin transfer throughout the root assembly 30 during the manufacturing process." Caruso teaches using the bonding agent within the radial gap 44 between the various surfaces (i.e. all surfaces) of the root inserts and/or spacers to promote surface adhesion and/or resin transfer thought the root assembly) and which connects the metal insert to the fibrous composite material in a stable manner(Col 6, ln. 27-65; Col 10, ln. 23-42), wherein the connecting layer is a coating or a film(portion 64 of the connecting layer body is a plastic film; Col 8, ln. 30-44) and the fibrous composite material is a cured material(Col 8, ln. 30-67; Col 10, ln. 43-55; Fig 14); weakening the connecting layer such that the connecting layer is connecting the metal insert to the fibrous composite material in a less stable manner(via heat; Col 10, ln. 23-42); and, removing the metal insert from the fibrous composite material(Col 10, ln. 23-42). In the alternative, should Applicant disagree with the interpretation of Caruso above, Caruso at least suggests applying a bonding agent between the inner and/or outer radial surfaces of the insert and the fibrous material 40 and/or 42. Therefore, it would have been obvious to one of ordinary skill in the art before the effective filing date of the claimed invention to modify Caruso to apply a connecting layer directly radially between the metal insert 42 and the fibrous composite material 40 to promote additional surface adhesion and/or resin transfer between the metal insert 42 and the fibrous composite material 40(Col 8, In. 30-36). In Regard to Claim 2 Caruso teaches: The method of claim 1(see rejection of claim 1 above), wherein the method is a repair method and further comprises: inserting another metal insert into a cavity in the fibrous composite material at a position where the removed metal insert was arranged(“insert 46 may be reheated, removed, and replaced in the event of damage and/or manufacturing defects”; Col 10, ln. 23-42). In Regard to Claim 4 Caruso teaches: The method of claim 1(see rejection of claim 1 above), further comprising: manufacturing of the wind turbine rotor blade part(100) including curing the fibrous composite material in a mold(66; Col 8, ln. 30-67; Fig 14); arranging the metal insert and the connecting layer at their desired positions(Step 104; Fig 14; Col 9, ln. 1-30); and, connecting the metal insert in a stable manner to the fibrous composite material via the connecting layer(Step 110; Fig 14; Col 9, ln. 1-30). In Regard to Claim 5 Caruso teaches: The method of claim 4(see rejection of claim 4 above), wherein said manufacturing of the wind turbine rotor blade part includes applying the connecting layer to at least one of an outer surface of the metal insert and a surface of a layer of a fiber material(connecting layer 50 is applied to the outer surface of 48; Col 6, ln. 36-56; Fig 3). In Regard to Claim 6 Caruso teaches: The method of claim 4(see rejection of claim 4 above), wherein said manufacturing of the wind turbine rotor blade part includes placing in a gap(radial gap 44) between the metal insert and the fibrous composite material(radial gap 44 extends bushing 48 of 46 and 40,42) an adhesive which forms the connecting layer(50 fills the radial gap between 48 and 40,42; Fig 3-5). In Regard to Claim 7 Caruso teaches: The method of claim 4(see rejection of claim 4 above), wherein said manufacturing of the wind turbine rotor blade part includes infusion of a resin into a mold(66) in which a fiber material(64) and the metal insert are arranged(Col 8, ln. 30 to Col 9, ln. 30). In Regard to Claim 8 Caruso teaches: The method of claim 1(see rejection of claim 1 above), wherein the connecting layer includes a polymeric material(Col 6, ln. 36-56; Col 7 ln. 3-36). In Regard to Claim 10 Caruso teaches: The method of claim 1(see rejection of claim 1 above), wherein the wind turbine rotor blade part includes a joining surface(33) configured to be arranged next to a wind turbine rotor blade hub(18; Fig 1-2); the metal insert defines a longitudinal direction(parallel to 24) and includes a circumferential surface(inner and/or outer circumferential surface of 46) embedded into the fibrous composite material(Fig 3-5), a front surface arranged at the joining surface(surface of 46 flush with 33), and a back surface embedded into the fibrous composite material(surface of 46 distal to the front surface; Fig 10); and, the connecting layer covers an entirety of the circumferential surface(connecting layer 50 covers an entirety of the inner and/or outer circumferential surfaces). In Regard to Claim 11 Caruso teaches: The method of claim 10(see rejection of claim 10 above), wherein the connecting layer further covers the back surface(the connecting layer 50 extends to cover the back surface; Fig 10). In Regard to Claim 12 Caruso teaches: The method of claim 1(see rejection of claim 1 above), wherein said weakening the connecting layer is carried out by applying heat(via heat; Col 10, ln. 23-42). In Regard to Claim 15 Caruso teaches: A wind turbine rotor blade part(16,32) comprising: a fibrous composite material(40,42; Col 6, ln. 21-36); a metal insert(46) held in said fibrous composite material(Fig 3); said metal insert being configured to fasten the wind turbine rotor blade part to a wind turbine rotor hub(18) or to another wind turbine rotor blade part(the metal insert is structurally capable of fastening the wind turbine rotor blade to another wind turbine rotor blade part; Col 3, ln. 7-22); a connecting layer(50,64) a connecting layer(50,64) disposed directly between the metal insert and the fibrous composite material(Fig 3) in a radial direction of the wind turbine rotor blade part(Col 8, In. 30-36, states "the root assembly 30 may also include a bonding agent 64 configured within the radial gap 44, e.g. between the various surfaces between the root inserts 46 and/or spacers 52. Thus the bonding agent 64 is configured to promote surface adhesion and/or resin transfer throughout the root assembly 30 during the manufacturing process." Caruso teaches using the bonding agent within the radial gap 44 between the various surfaces (i.e. all surfaces) of the root inserts and/or spacers to promote surface adhesion and/or resin transfer thought the root assembly); said connecting layer connecting said metal insert to said fibrous composite material in a stable manner(Col 6, ln. 27-65; Col 10, ln. 23-42); said connecting layer being a coating or a film(portion 64 of the connecting layer body is a plastic film; Col 8, ln. 30-44) and said fibrous composite material is a cured material(Col 8, ln. 30-67; Col 10, ln. 43-55; Fig 14); wherein the wind turbine rotor blade part is configured to enable a weakening of said connecting layer such that said connecting layer connects said metal insert to said fibrous composite material in a less stable manner(via heat; Col 10, ln. 23-42); and, said metal insert is configured to be removed from said fibrous composite material(Col 10, ln. 23-42). In the alternative, should Applicant disagree with the interpretation of Caruso above, Caruso at least suggests applying a bonding agent between the inner and/or outer radial surfaces of the insert and the fibrous material 40 and/or 42. Therefore, it would have been obvious to one of ordinary skill in the art before the effective filing date of the claimed invention to modify Caruso to apply a connecting layer directly radially between the metal insert 42 and the fibrous composite material 40 to promote additional surface adhesion and/or resin transfer between the metal insert 42 and the fibrous composite material 40(Col 8, In. 30-36). In Regard to Claim 21 Caruso teaches: A method for removing a metal insert(46) from a wind turbine rotor blade part(16,32,40,42), the method comprising: providing the wind turbine rotor blade part(40,42; Col 10, ln. 22-42), the wind turbine rotor blade part including a fibrous composite material(Col 6, ln. 21-36) and the metal insert(46) held in the fibrous composite material(Fig 3), wherein the metal insert is configured to fasten the wind turbine rotor blade part to a wind turbine rotor hub(18) or to another wind turbine rotor blade part(the metal insert is structurally capable of fastening the wind turbine rotor blade to another wind turbine rotor blade part; Col 3, ln. 7-22), the wind turbine rotor blade further including a connecting layer(50,64) disposed between the metal insert and the fibrous composite material(Fig 3; 64 is between 46 and 40/42 since a line extending at an angle from 46 would pass through both 64 and 40/42, further because the junction of 46/52 extends the full height of the radial gap between 46 and 52 64 also connects 46 to 40/42; in another interpretation - Col 8, In. 30-36, states "the root assembly 30 may also include a bonding agent 64 configured within the radial gap 44, e.g. between the various surfaces between the root inserts 46 and/or spacers 52. Thus the bonding agent 64 is configured to promote surface adhesion and/or resin transfer throughout the root assembly 30 during the manufacturing process." Caruso teaches using the bonding agent within the radial gap 44 between the various surfaces (i.e. all surfaces) of the root inserts and/or spacers to promote surface adhesion and/or resin transfer thought the root assembly) and which connects the metal insert to the fibrous composite material in a stable manner(Col 6, ln. 27-65; Col 10, ln. 23-42), wherein the connecting layer is a coating or a film(portion 64 of the connecting layer body is a plastic film; Col 8, ln. 30-44) and the fibrous composite material is a cured material(Col 8, ln. 30-67; Col 10, ln. 43-55; Fig 14); weakening the connecting layer such that the connecting layer is connecting the metal insert to the fibrous composite material in a less stable manner(via heat; Col 10, ln. 23-42); and, removing only the metal insert from the fibrous composite material(Col 10, ln. 23-42; there is nothing the claims preventing the claimed "metal insert" to include non-metallic material, as such, since 46 in the metal insert because includes metal, “only” the metal insert is removed). In the alternative, should Applicant disagree with the interpretation of Caruso above, Caruso at least suggests applying a bonding agent between the inner and/or outer radial surfaces of the insert and the fibrous material 40 and/or 42. Therefore, it would have been obvious to one of ordinary skill in the art before the effective filing date of the claimed invention to modify Caruso to apply a connecting layer directly radially between the metal insert 42 and the fibrous composite material 40 to promote additional surface adhesion and/or resin transfer between the metal insert 42 and the fibrous composite material 40(Col 8, In. 30-36). Claim(s) 3 and 14 is/are rejected under 35 U.S.C. 103 as being unpatentable over Caruso in view of Martini et al. (NPL Document 1), hereinafter: “Martini”. In Regard to Claim 3 Caruso teaches: The method of claim 1(see rejection of claim 1 above), Caruso fails to teach: wherein the method is a recycling method and further comprises: recycling at least one of the metal insert and the fibrous composite material after the metal insert has been removed from the fibrous composite material. Martini teaches: A method of recycling wind turbine blades wherein pyrolysis or solvolysis is used to separate the blade into three different materials, glass, metal and fillers for recycling(section 1.2, Fig 2). Therefore, it would have been obvious to one having ordinary skill in the art before the effective filing date of the claimed invention, to modify Caruso to incorporate the teachings of Martini to recycle the metal insert and/or the fibrous composite material decrease the cost of landfill disposal, and resell the amount of recycled raw material for a profit(section 1.2). In Regard to Claim 14 Caruso teaches: The method of claim 1(see rejection of claim 1 above), Caruso fails to teach: wherein said weakening the connecting layer is carried out by applying a solvent Martini teaches: A method of recycling wind turbine blades wherein pyrolysis or solvolysis is used to separate the blade into three different materials, glass, metal and fillers for recycling(section 1.2, Fig 2). Therefore, it would have been obvious to one of ordinary skill in the art before the effective filing date of the claimed invention to modify Martini to incorporate the teachings of Martini to use solvolysis instead of heat to weaken the connecting layer since solvolysis works better than pyrolysis for carbon fiber based composites(section 1.2, Fig 2) Claim(s) 9 is/are rejected under 35 U.S.C. 103 as being unpatentable over Caruso in view of Cundiff et al. (US 6589618), hereinafter: “Cundiff”. In Regard to Claim 9 Caruso teaches: The method of claim 1(see rejection of claim 1 above), Caruso fails to teach: wherein the connecting layer includes a ceramic material Cundiff teaches: A method of manufacturing a blade made of composite material using a resin transfer molding process wherein the composite fiber includes a ceramic material(“ceramics”; Col 10, ln. 7-19). It would have been obvious to one having ordinary skill in the art before the effective filing date of the claimed invention to have modified Caruso to incorporate the teachings of Cundiff to use ceramic fiber material to construct the connecting layer as Cundiff teaches the use of a “ceramic fiber material” is a known material suitable for making composite wind turbine blades. It would have been obvious to one having ordinary skill in the art at the time of the invention to have selected a “ceramic fiber material” because it is merely the selection of an art known material suitable for the construction of composite wind turbine blades. In further support of this position, the selection of a known material to make an abradable coating prior to the invention was held to be obvious see In re Leshin, 277 F.2d 197, 125 USPQ 416 (CCPA 1960). Claim(s) 13 is/are rejected under 35 U.S.C. 103 as being unpatentable over Caruso in view of Woods et al. (US 6585839), hereinafter: “Woods”. In Regard to Claim 13 Caruso teaches: The method of claim 1(see rejection of claim 1 above), wherein said weaking the connecting layer is carried out by applying heat to the thermoplastic inserts(Col 10, ln. 22-42). Caruso fails to teach: wherein said weakening the connecting layer is carried out by applying ultrasound Woods teaches: Woods teaches it is known to use ultrasonic heating to heat thermoplastic material to enabling bonding and thus fabrication of composite parts(Col 2, ln. 20-29; Col 4, ln. 1-54). Therefore, it would have been obvious to one of ordinary skill in the art before the effective filing date of the claimed invention to modify Caruso to incorporate the teachings of Woods to weaken the connecting layer by applying ultrasonic heating because ultrasonic heating does not depend upon a thermal driver to effect energy transfer to the composite material, is instantaneously modulatable, and it provides deep, penetrating heating in the plastic matrix beyond mere surface heating(Col 2, ln. 21-28) Conclusion Any inquiry concerning this communication or earlier communications from the examiner should be directed to BRIAN P WOLCOTT whose telephone number is (571)272-9837. The examiner can normally be reached M-F 8:00am-4:30pm. 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, Nicholas Weiss can be reached at 571-270-1775. 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. /BRIAN P WOLCOTT/Primary Examiner, Art Unit 3711
Read full office action

Prosecution Timeline

Show 3 earlier events
Nov 19, 2025
Final Rejection mailed — §102, §103
Feb 04, 2026
Interview Requested
Feb 13, 2026
Applicant Interview (Telephonic)
Feb 13, 2026
Examiner Interview Summary
Feb 19, 2026
Response after Non-Final Action
Mar 11, 2026
Request for Continued Examination
Apr 01, 2026
Response after Non-Final Action
May 04, 2026
Non-Final Rejection mailed — §102, §103 (current)

Precedent Cases

Applications granted by this same examiner with similar technology

Patent 12680761
CONVECTIVE SUBSTRATE COOLING WITH MINIMAL PRESSURE CHANGE
3y 4m to grant Granted Jul 14, 2026
Patent 12680467
VARIABLE CAPACITY TURBOCHARGER
1y 4m to grant Granted Jul 14, 2026
Patent 12654823
MAST NAVIGATION LIGHT
3y 1m to grant Granted Jun 16, 2026
Patent 12655773
LIGHT WEIGHT FAN CASING CONFIGURATIONS FOR ENERGY ABSORPTION
1y 10m to grant Granted Jun 16, 2026
Patent 12648389
COMPACT MODULAR GAS DISTRIBUTION PLUMBING AND HEATING SYSTEM FOR MULTI-STATION DEPOSITION MODULES
3y 2m to grant Granted Jun 02, 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
78%
Grant Probability
99%
With Interview (+30.3%)
2y 10m (~1y 4m remaining)
Median Time to Grant
High
PTA Risk
Based on 583 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