CN1056645A - 改进的高温钎焊合金及有关方法 - Google Patents

改进的高温钎焊合金及有关方法 Download PDF

Info

Publication number
CN1056645A
CN1056645A CN91103414A CN91103414A CN1056645A CN 1056645 A CN1056645 A CN 1056645A CN 91103414 A CN91103414 A CN 91103414A CN 91103414 A CN91103414 A CN 91103414A CN 1056645 A CN1056645 A CN 1056645A
Authority
CN
China
Prior art keywords
cobalt
alloy
surplus
weight
boron
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN91103414A
Other languages
English (en)
Inventor
阿德里安·M·贝尔兰
小查尔斯·H·克赖舍
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of CN1056645A publication Critical patent/CN1056645A/zh
Pending legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C11/00Alloys based on lead
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24Selection of soldering or welding materials proper
    • B23K35/30Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
    • B23K35/3046Co as the principal constituent
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24Selection of soldering or welding materials proper
    • B23K35/30Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/07Alloys based on nickel or cobalt based on cobalt

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Powder Metallurgy (AREA)
  • Electric Connection Of Electric Components To Printed Circuits (AREA)

Abstract

一种钴基的高温钎焊合金,它具有如下组成(按 重量计):镍约8.5%-12.5%,铬约24%-40%,钨约 0%-9%,碳约0.03%-0.6%,硼约0.01%-3.5%,Si 约0.1-11%,锰最高达约2%,铪约0.1%-3%,钽约 0.1%-8%,锆约0%-1%,钛0%-约1%,余量为 钴。该钎焊合金用于钴基叶轮机部件超耐热合金的 修复。

Description

本发明涉及合金制品的修复,更具体地说,涉及用活化扩散合拢焊合方法,对用坏的燃气轮机喷咀进行修复时使用的钎焊合金组合物。
有许多钴基合金,既可用于制造又可用于修复高温运转的燃气轮机部件(包括燃烧室、涡轮叶片、喷咀等)。
美国专利NOS  4,830,934;4,614,296;4,381,944;4,285,459;4,058,415;3,355,287;3,276,865;3,271,140;及4,396,577,中公开了用于生产和/或修复超耐热合金制品的钴基合金典型实例。
这些部件在高温操作条件下运转期间,会发生各种类型的损坏或损耗。例如,由于热循环、外部物体的撞击和/或腐蚀会导致裂纹。众所周知,这些部件的成本比较高,因此修复这些部件当然比更换这些部件更为合算。
本发明涉及一种长期暴露在腐蚀高温操作条件下环境造成损坏的燃气轮机部件修复时所用的改进钎焊合金组合物。这些钎焊合金组合物特别适用于活化扩散焊合方法的修复中,例如,通过钎焊一种钎焊合金和喷咀之基质金属的特殊形式混合物来修复喷咀。具体地说,修复的完成是通过含钎焊合金和母合金粉之混合物的熔敷物进行钎焊。真空钎焊循环引起钎焊合金熔融并与母材合金粉和母材基质表面熔合。然后,采用后钎焊扩散热处理循环以促进进一步内扩散。所得之修复区的机械性能接近母材合金的机械性能。
按照本发明之钎焊合金是具有高铬含量并含有作为熔点降低添加剂B和Si的钴基合金。后者是使钎焊合金熔融而不熔融母材合金构件所必需的。
本发明之钴基合金还特别含有能形成MC的主要元素Ta和Hf。
因此,本发明的一个最佳实施方案,提供了以下组成(重量%)的钎焊合金:
镍  约8.5%-约12.5%
铬  约24%-约40%
钨  约0%-约9%
碳  约0.03%-约0.6%
硼  约0.01%-约3.5%
硅  约0.1%-约11%
锰  最高达约2%
铪  约0.1%-约3%
钽  约0.1%-约8%
锆  约0%-约1%
钛  约0%-约1%
钴  余量
本发明之合金耐高温(1200-1900°F),而且在上述温度范围内具有优良的机械特性以及抗氧化性能和抗腐蚀性能。
由以下详细叙述可明显地看出本发明的其它目的和优点。
本发明之钎焊合金特别适用具有以下重量百分组成的已知钴基超耐热合金叶轮机喷咀:
Ni  10%
Cr  29%
W  7%
C  0.35%
B  0.015%
Si  0.1%
Mn  0.1%
Hf  1%
Ta  0.5%
Zr  0.5%
Ti  0.2%
Co  余量
本发明之合金还被配制成能适用于另一种新式的含以下重量百分成分的钴基超耐热基底材料:
Ni  10%
Cr  29%
W  7%
C  0.25%
Si  0.9%
Mn  0.6%
Co  余量
上述两种情况的主要目的都是保持上述“母材”合金的机械和耐环境特性,同时还降低作为良好钎焊特征的钎焊合金(而不是母材合金)的熔融温度。
本发明包括具有以下组成(重量)范围的Co基合金:
镍  约8.5%-约12.5%
铬  约24%-约40%
钨  约0%-9%
碳  约0.03%-约0.6%
硼  约0.01%-约3.5%
硅  约0.1%-约11%
锰  最高达约2%
铪  约0.1%-约3%
钽  约0.1%-约8%
锆  约0%-约1%
钛  0%-约1%
钴  余量
按照本发明的第一种典型合金具有以下组成:
镍  10%
铬  29%
钨  7%
碳  0.1%
硼  2.5%
硅  2.5%
锰  0.6%
铪  2%
钽  2%
锆  0%
钛  0%
钴  余量
按照本发明的第二种典型合金具有以下组成:
镍  10%
铬  29%
钨  3.5%
碳  0.1%
硼  1%
硅  7%
锰  0.6%
铪  0.1%
钽  4%
锆  0%
钛  0%
钴  余量
如上所述,本发明之合金配方中含有作为熔点降低添加剂的硼和硅。这是为保证在钎焊时使钎焊合金混合物熔融但母材合金不熔融所必需的。硼在这方面是有利的,但却不利于好的抗氧化性。因此,本发明合金还含有主要形成MC的元素钽和铪以增加抗氧化性能。由于这些难熔元素(也包括Zr和Ti)也是公知的最热稳定的硼化物生成物、因此MB2或MB型难熔硼化物应作为离散颗粒在钎焊区中形成。不过它可能会抑制硼迁移离开钎焊区,但却能使会削弱强度和延展性的原状(script)或低共熔状硼化物结构的出现率减为最少。
本发明提供了一种钴基高温钎焊合金,上面列举其组成范围和其中两种有代表性合金的具体组成。本发明还提供了用上述钴基高温钎焊合金修复钴基超耐热合金基材的方法,它包括制备具有上述组成的粉状钎焊合金和钴基超耐热合金粉未的混合物;用它进行修复时,将本发明之钎焊合金和母材金属粉末的混合物在用坏待修的叶轮机喷咀(或其它部件)位置上进行真空钎焊的修复。真空钎焊使钎焊合金与母材合金粉以及母材基体表面熔融。然后用普通的后钎焊扩散热处理循环进一步促进内扩散并使硼迁移离千钎焊区。因此,硼对表面抗腐蚀性的影响减为最小。
使用本发明合金,可使修复区的机械特性与母材合金的相近。
因此,本发明钎焊合金提供了在约1200°-1900°F的温度范围内具有优良的抗氧化性和抗腐蚀性以及优良的机械性能,从而使叶轮机喷咀(或其它部件)的修复区具有类似于母材合金的机械特性。
对本发明目前被认为是最实际和最佳实施方案进行了描述,应理解本发明并非仅限于已公开的实施方案,相反,它还适合于包括在权利要求精神和范畴内的各种修改方案和等同方案。

Claims (9)

1、一种钴基的高温钎焊合金,它含有(按重量计):
镍  约      8.5%-12.5%
铬  约      24%-40%
钨  约      0%-9%
碳  约      0.03%-0.6%
硼  约      0.01%-3.5%
硅  约      0.1%-11%
锰  最高达  2%
铪  约      0.1%-3%
钽  约      0.1%-8%
锆  约      0%-1%
钛          0%-约1%
钴          余量。
2、根据权利要求1的合金,它主要由以下元素组成(按重量计):
镍  10%
铬  29%
钨  7%
碳  0.1%
硼  2.5%
硅  2.5%
锰  0.6%
铪  2%
钽  2%
钴  余量。
3、根据权利要求1的合金,它主要由以下元素组成(按重量计):
镍  10%
铬  29%
钨  3.5%
碳  0.1%
硼  1%
硅  7%
锰  0.6%
铪  0.1%
钽  4%
钴  余量。
4、一种修复钴基超耐热合金基材的方法,该方法包括以下步骤:
(a)制备粉末状钎焊合金组合物和所述钴基超耐热合金粉末的混合物;所述钎焊合金组合物主要由以下元素组成(按重量计)
镍  约8.5%-12.5%
铬  约24%-40%
钨  约0%-9%
碳  约0.03%-0.6%
硼  约0.01%-3.5%
硅  约0.1%-11%
锰  最高量达约2%
铪  约0.1%-3%
钽  约0.1%-8%
锆  约0%-1%
钛  0%-约1%
钴  余量
(b)在所述钴基耐热合金基材的待修复部位上真空沉积所述混合物,从而导致所述钎焊合金粉熔融并与所述钴基超耐热合金粉和所述钴基超耐热合金基材熔合。
5、根据权利要求4的方法,它还包括以下步骤:
(c)热处理修复区以促进内扩散和迁移硼离开所述区。
6、根据权利要求4的方法,其中所述钎焊合金主要由以下元素组成(按重量计):
Ni  10%
Cr  29%
W  7%
C  0.1%
B  2.5%
Si  2.5%
Mn  0.6%
Hf  2%
Ta  2%
Co  余量。
7、根据权利要求4的方法,其中所述钎焊合金主要由以下元素组成(按重量计):
Ni  10%
Cr  29%
W  3.5%
C  0.1%
B  1%
Si  7%
Mn  0.6%
Hf  0.1%
Ta  4%
Co  余量。
8、根据权利要求4的方法,其中所述钴基超耐热合金基材具有主要由以下元素构成的组成(按重量计):
Ni  10%
Cr  29%
W  7%
C  0.35%
B  0.015%
Si  0.1%
Mn  0.1%
Hf  1%
Ta  0.5%
Zr  0.5%
Ti  0.2%
Co  余量。
9、根据权利要求4的方法,其中所述基材具有主要由以下元素构成的组成(按重量计):
Ni  10%
Cr  29%
W  7%
C  0.25%
Si  0.9%
Mn  0.6%
Co  余量。
CN91103414A 1990-05-18 1991-05-17 改进的高温钎焊合金及有关方法 Pending CN1056645A (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US524,982 1990-05-18
US07/524,982 US5066459A (en) 1990-05-18 1990-05-18 Advanced high-temperature brazing alloys

Publications (1)

Publication Number Publication Date
CN1056645A true CN1056645A (zh) 1991-12-04

Family

ID=24091439

Family Applications (1)

Application Number Title Priority Date Filing Date
CN91103414A Pending CN1056645A (zh) 1990-05-18 1991-05-17 改进的高温钎焊合金及有关方法

Country Status (7)

Country Link
US (1) US5066459A (zh)
EP (1) EP0457503B1 (zh)
JP (1) JP3145428B2 (zh)
KR (1) KR100207803B1 (zh)
CN (1) CN1056645A (zh)
DE (1) DE69108290T2 (zh)
NO (1) NO911915L (zh)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100457369C (zh) * 2006-08-17 2009-02-04 贵研铂业股份有限公司 一种高温钴基合金粉末钎料
CN101209516B (zh) * 2005-12-27 2010-10-13 株式会社东芝 无铅焊料、焊接接合产品及电子元件
CN102172900A (zh) * 2010-12-15 2011-09-07 安泰科技股份有限公司 一种无砟板磨轮的制造方法
CN1994656B (zh) * 2005-12-15 2012-05-30 通用电气公司 钎焊合金组合物
CN102581517A (zh) * 2012-04-05 2012-07-18 郑州机械研究所 钎焊铝电解用惰性阳极与金属导电杆的高温钎料
CN107201474A (zh) * 2016-03-16 2017-09-26 优频科技材料股份有限公司 硬面合金材料
CN110106420A (zh) * 2019-05-15 2019-08-09 西迪技术股份有限公司 一种Co基高温合金及其制备方法和应用
CN113302326A (zh) * 2019-01-07 2021-08-24 西门子能源全球有限两合公司 用于增材制造的Co合金

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5139738A (en) * 1990-12-18 1992-08-18 General Electric Company Corrosion resistant filler weld alloys
US5182080A (en) * 1990-12-27 1993-01-26 General Electric Company Advanced high-temperature brazing alloys
US5666643A (en) * 1995-02-23 1997-09-09 General Electric Company High temperature braze material
KR100199449B1 (ko) * 1996-12-30 1999-06-15 정종순 코발트 기초 내열합금
US5916518A (en) 1997-04-08 1999-06-29 Allison Engine Company Cobalt-base composition
US20030221756A1 (en) * 1997-09-29 2003-12-04 Isover Saint Gobain Cobalt based alloy, article made from said alloy and method for making same
JP3629920B2 (ja) * 1997-10-20 2005-03-16 株式会社日立製作所 ガスタービン用ノズル,発電用ガスタービン,Co基合金及び溶接材料
DE19747931C1 (de) * 1997-10-30 1999-07-08 Lemfoerder Metallwaren Ag Kugelgelenk
US6210812B1 (en) * 1999-05-03 2001-04-03 General Electric Company Thermal barrier coating system
US6355356B1 (en) * 1999-11-23 2002-03-12 General Electric Company Coating system for providing environmental protection to a metal substrate, and related processes
US7360991B2 (en) * 2004-06-09 2008-04-22 General Electric Company Methods and apparatus for fabricating gas turbine engines
US8075839B2 (en) * 2006-09-15 2011-12-13 Haynes International, Inc. Cobalt-chromium-iron-nickel alloys amenable to nitride strengthening
US20090041611A1 (en) * 2007-08-07 2009-02-12 General Electric Company Braze alloy composition with enhanced oxidation resistance and methods of using the same
US8075662B2 (en) * 2008-04-25 2011-12-13 United Technologies Corporation Nickel braze alloy composition
JP2009285664A (ja) 2008-05-27 2009-12-10 Toshiba Corp ロウ付け補修材料およびその材料を使用したロウ付け補修方法
US8273148B2 (en) 2009-01-30 2012-09-25 Untied Technologies Corporation Nickel braze alloy composition
DE102009036405A1 (de) 2009-08-06 2011-02-10 Mtu Aero Engines Gmbh Reparatur von Turbinenbauteilen und Lotlegierung hierfür
US10076811B2 (en) 2011-11-03 2018-09-18 Siemens Energy, Inc. Structural braze repair of superalloy component
EP2969380B1 (en) * 2013-03-14 2020-05-06 Siemens Energy, Inc. Method for brazing a rene 80 superalloy substrate
DE102014200121A1 (de) 2014-01-08 2015-07-09 Siemens Aktiengesellschaft Manganhaltige Hochtemperaturlotlegierung auf Kobaltbasis, Pulver, Bauteil und Lotverfahren
CN106238961A (zh) * 2016-08-23 2016-12-21 安徽华东光电技术研究所 一种适用于行波管阴极钎焊焊料及制备方法
JP7153488B2 (ja) * 2018-07-09 2022-10-14 山陽特殊製鋼株式会社 肉盛用又は溶射用の粉末

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1449338A (en) * 1921-06-18 1923-03-20 Haynes Stellite Co Alloy and process of making the same
US2763547A (en) * 1955-06-09 1956-09-18 Allegheny Ludlum Steel Cast alloys
US3028235A (en) * 1958-12-29 1962-04-03 Gen Electric Cobalt base brazing alloy
NL136758C (zh) * 1963-10-21 1900-01-01
US3366478A (en) * 1965-07-21 1968-01-30 Martin Marietta Corp Cobalt-base sheet alloy
US3549356A (en) * 1969-01-06 1970-12-22 Gen Electric High temperature corrosive resistant cobalt-base alloys
US3837838A (en) * 1972-12-18 1974-09-24 M Mohammed High strength, ductile cobalt-base dental alloy
US4124737A (en) * 1976-12-30 1978-11-07 Union Carbide Corporation High temperature wear resistant coating composition
US4478638A (en) * 1982-05-28 1984-10-23 General Electric Company Homogenous alloy powder
US4381944A (en) * 1982-05-28 1983-05-03 General Electric Company Superalloy article repair method and alloy powder mixture
JPS6052545A (ja) * 1983-09-02 1985-03-25 Mitsubishi Metal Corp 溶融ガラス接触部材用Co基耐熱合金
JPH0243813B2 (ja) * 1984-06-13 1990-10-01 Mitsubishi Metal Corp Gasutaabinyokokyodocokitainetsugokin
US4618474A (en) * 1985-01-25 1986-10-21 Asahi Fiber Glass Company, Limited Co-base heat resistant alloy
US4765817A (en) * 1985-06-18 1988-08-23 Owens-Corning Fiberglas Corporation Corrosion resistant cobalt-base alloy containing hafnium
US4830934A (en) * 1987-06-01 1989-05-16 General Electric Company Alloy powder mixture for treating alloys

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1994656B (zh) * 2005-12-15 2012-05-30 通用电气公司 钎焊合金组合物
CN101209516B (zh) * 2005-12-27 2010-10-13 株式会社东芝 无铅焊料、焊接接合产品及电子元件
CN100457369C (zh) * 2006-08-17 2009-02-04 贵研铂业股份有限公司 一种高温钴基合金粉末钎料
CN102172900A (zh) * 2010-12-15 2011-09-07 安泰科技股份有限公司 一种无砟板磨轮的制造方法
CN102172900B (zh) * 2010-12-15 2013-01-09 安泰科技股份有限公司 一种无砟板磨轮的制造方法
CN102581517A (zh) * 2012-04-05 2012-07-18 郑州机械研究所 钎焊铝电解用惰性阳极与金属导电杆的高温钎料
CN102581517B (zh) * 2012-04-05 2015-02-11 郑州机械研究所 钎焊铝电解用惰性阳极与金属导电杆的高温钎料
CN107201474A (zh) * 2016-03-16 2017-09-26 优频科技材料股份有限公司 硬面合金材料
CN107201474B (zh) * 2016-03-16 2022-05-06 优频科技材料股份有限公司 硬面合金材料
CN113302326A (zh) * 2019-01-07 2021-08-24 西门子能源全球有限两合公司 用于增材制造的Co合金
CN110106420A (zh) * 2019-05-15 2019-08-09 西迪技术股份有限公司 一种Co基高温合金及其制备方法和应用

Also Published As

Publication number Publication date
DE69108290T2 (de) 1995-11-09
US5066459A (en) 1991-11-19
EP0457503B1 (en) 1995-03-22
KR100207803B1 (ko) 1999-07-15
JPH04254544A (ja) 1992-09-09
NO911915L (no) 1991-11-19
KR910020190A (ko) 1991-12-19
DE69108290D1 (de) 1995-04-27
JP3145428B2 (ja) 2001-03-12
NO911915D0 (no) 1991-05-16
EP0457503A1 (en) 1991-11-21

Similar Documents

Publication Publication Date Title
CN1056645A (zh) 改进的高温钎焊合金及有关方法
CN1288266C (zh) 镍基耐热硬质合金
JP5068927B2 (ja) ニッケル系ろう合金組成、その関連方法及び物品
EP1859880B1 (en) Nickel alloy for repairs
JP4264490B2 (ja) ニッケル基ろう付材
US5735448A (en) Method of repairing surface and near surface defects in superalloy articles such as gas turbine engine components
CN1038951C (zh) 腐蚀的超耐热合金或者耐热钢零件的重新磨光及重新磨光的零件
EP0340300B1 (en) High temperature metal alloy mixtures for filling holes and repairing damages in superalloy bodies
JP5721189B2 (ja) 耐熱性Ni基合金及びその製造方法
US10335878B2 (en) Ni—Ti—Cr near ternary eutectic alloy for gas turbine component repair
EP1226896A2 (en) Nickel-base braze material and braze repair method
CN114769772B (zh) 一种提升gh3536/gh4738合金接头强度的真空钎焊方法
WO2018116810A1 (ja) Ni基耐熱合金
CN114310033A (zh) 一种活化扩散剂及其应用
US10221702B2 (en) Imparting high-temperature wear resistance to turbine blade Z-notches
JP2006255767A (ja) 熱間で使用する金型用Ni基肉盛粉末および熱間用金型
EP2392687A1 (en) Method for manufacturing an oxidation resistant component with improved high temperature strength and corresponding oxidation resistant component with improved high temperature strength
EP0340296B1 (en) Method of repairing damages in superalloys
JP3893133B2 (ja) Ni基合金部材およびその製造方法
CN114571024B (zh) 一种减少gh3536蜂窝与gh4738环件组合件溶蚀的真空钎焊工艺
WO2023027054A1 (ja) ニッケル基超合金及びその粉末、並びにニッケル基超合金造形体の製造方法
CN117182381A (zh) 一种高温单晶合金钎焊材料及方法
CN111001923A (zh) 一种搅拌工具表面处理方法
JPH01241A (ja) 超耐熱合金
Tsao et al. Suppressing effect of 1 wt.% nano-TiO 2 addition into low Ag content Sn-Ag-Cu solder alloy on the intermetallic growth with Cu substrate during isothermal aging

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C01 Deemed withdrawal of patent application (patent law 1993)
WD01 Invention patent application deemed withdrawn after publication