EP3921113A1 - Verfahren zur trennung eines ersten mechanischen teils von einem zweiten mechanischen teil - Google Patents
Verfahren zur trennung eines ersten mechanischen teils von einem zweiten mechanischen teilInfo
- Publication number
- EP3921113A1 EP3921113A1 EP20709268.5A EP20709268A EP3921113A1 EP 3921113 A1 EP3921113 A1 EP 3921113A1 EP 20709268 A EP20709268 A EP 20709268A EP 3921113 A1 EP3921113 A1 EP 3921113A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- mechanical part
- mechanical
- blade
- reinforcement
- cooling
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
- B23P19/04—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for assembling or disassembling parts
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09J—ADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
- C09J5/00—Adhesive processes in general; Adhesive processes not provided for elsewhere, e.g. relating to primers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P6/00—Restoring or reconditioning objects
- B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24C—ABRASIVE OR RELATED BLASTING WITH PARTICULATE MATERIAL
- B24C1/00—Methods for use of abrasive blasting for producing particular effects; Use of auxiliary equipment in connection with such methods
- B24C1/10—Methods for use of abrasive blasting for producing particular effects; Use of auxiliary equipment in connection with such methods for compacting surfaces, e.g. shot-peening
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24C—ABRASIVE OR RELATED BLASTING WITH PARTICULATE MATERIAL
- B24C5/00—Devices or accessories for generating abrasive blasts
- B24C5/005—Vibratory devices, e.g. for generating abrasive blasts by ultrasonic vibrations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B26—HAND CUTTING TOOLS; CUTTING; SEVERING
- B26F—PERFORATING; PUNCHING; CUTTING-OUT; STAMPING-OUT; SEVERING BY MEANS OTHER THAN CUTTING
- B26F3/00—Severing by means other than cutting; Apparatus therefor
- B26F3/06—Severing by using heat
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
- B64C11/20—Constructional features
- B64C11/205—Constructional features for protecting blades, e.g. coating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
- B64C11/20—Constructional features
- B64C11/26—Fabricated blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/40—Maintaining or repairing aircraft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/005—Repairing methods or devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/04—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2603/00—Vanes, blades, propellers, rotors with blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B43/00—Operations specially adapted for layered products and not otherwise provided for, e.g. repairing; Apparatus therefor
- B32B43/006—Delaminating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
- B64C2027/4733—Rotor blades substantially made from particular materials
- B64C2027/4736—Rotor blades substantially made from particular materials from composite materials
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09J—ADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
- C09J2301/00—Additional features of adhesives in the form of films or foils
- C09J2301/50—Additional features of adhesives in the form of films or foils characterized by process specific features
- C09J2301/502—Additional features of adhesives in the form of films or foils characterized by process specific features process for debonding adherents
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/324—Blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/10—Manufacture by removing material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/502—Thermal properties
- F05D2300/5024—Heat conductivity
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
Definitions
- the cooling unit 38 comprises a reservoir 42 of pressurized cooling fluid and a pressure reducing valve 44 capable of receiving the fluid coming from the reservoir 42 and of delivering it under a determined pressure.
- This pressure reducer is connected to a conduit 46, supplied with pressurized cooling fluid, which extends close to the reinforcement 14.
- the end of the conduit 46 comprises a nozzle 48 which is configured to spray the cooling fluid onto the surface of the valve. reinforcement 14.
- Liquid nitrogen is sprayed at a temperature of -200 ° C.
- the adhesive film 16 is cooled by thermal conduction through the reinforcement 14.
- the nitrogen application time therefore depends on the thickness and the nature of the metal reinforcement 14, as well as on the desired temperature in the adhesive film 16 to cause it to break.
- the second part that is to say the reinforcement 14 is subjected to a compressive stress in a direction D substantially perpendicular to a surface of the adhesive film 16. .
- This compressive stress is a mechanical stress corresponding to a shock exerted on the surface of the metal reinforcement 14.
- This compression wave has the advantage of being transformed into a tensile wave at the interface between the reinforcement 14 and the adhesive film 16 of the makes the difference in mechanical impedance between the reinforcement 14 and the adhesive film 16.
- the change in mechanical rigidity at the interface between two materials induces the reflection of part of the incident wave compression into a tensile wave.
- These components comprise a generator 50, converting a source of electrical energy supplying the generator into a sinusoidal electrical signal. This signal feeds a converter 52, which converts the sinusoidal electrical signal into sinusoidal vibrating waves. These vibratory waves are transmitted to an amplifier 54, which amplifies them. The amplifier 54 amplifies the vibratory waves intended for a sonotrode 56 which is able to mechanically transmit the vibratory waves. At one end of the sonotrode 56 is at least one transmission finger 58, also called an "indenter”, which receives the vibratory waves from the sonotrode 56, which is arranged in contact with the reinforcement 14 of the second part, and which is suitable for them. mechanically transmit to the reinforcement 14.
- the transmission finger or fingers 58 of the sonotrode 58 exert the mechanical stress by hammering by ultrasound, as we have seen, substantially in the direction D substantially perpendicular to a surface of the adhesive film 16 ..
- the assembly 32 of the tooling 30 enables the two stages of cooling and stressing to be carried out simultaneously. These two operations are carried out in a coverage zone C of the leading edge 20 of the blade 12 by the tooling 30, and more particularly by the fingers 58 of the sonotrode 56 immediately after passage of the nozzle 48.
- the zone C is of a length I less than the length L of the leading edge 14 of the vane 12.
- the tool 40 is therefore moved along the entire length L of the leading edge 14 of the vane 12, as illustrated FIGS. 3 and 4.
- the coverage area C first undergoes cooling by the nozzle 48 and then immediately after the mechanical stress by the transmission fingers 58.
- the immediate proximity of the fingers 58 to the nozzle 48 prevents the leading edge 20 from heating up and the cooling from losing its effectiveness.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Forests & Forestry (AREA)
- Life Sciences & Earth Sciences (AREA)
- Organic Chemistry (AREA)
- Architecture (AREA)
- Transportation (AREA)
- Manufacturing & Machinery (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
- Adhesives Or Adhesive Processes (AREA)
- Automatic Assembly (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
- Laminated Bodies (AREA)
- Cooling Or The Like Of Electrical Apparatus (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1901069A FR3092267B1 (fr) | 2019-02-04 | 2019-02-04 | Procédé de désolidarisation d'une première pièce mécanique d'une deuxième pièce mécanique |
PCT/FR2020/050178 WO2020161426A1 (fr) | 2019-02-04 | 2020-02-04 | Procede de desolidarisation d'une premiere piece mecanique d'une deuxieme piece mecanique |
Publications (1)
Publication Number | Publication Date |
---|---|
EP3921113A1 true EP3921113A1 (de) | 2021-12-15 |
Family
ID=67441235
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20709268.5A Pending EP3921113A1 (de) | 2019-02-04 | 2020-02-04 | Verfahren zur trennung eines ersten mechanischen teils von einem zweiten mechanischen teil |
Country Status (8)
Country | Link |
---|---|
US (1) | US11731221B2 (de) |
EP (1) | EP3921113A1 (de) |
JP (1) | JP2022524292A (de) |
CN (1) | CN113474117B (de) |
BR (1) | BR112021015211A2 (de) |
CA (1) | CA3128288A1 (de) |
FR (1) | FR3092267B1 (de) |
WO (1) | WO2020161426A1 (de) |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9700819D0 (en) * | 1997-01-16 | 1997-03-05 | Gkn Westland Helicopters Ltd | Method of and apparatus for removing a metallic component from attachmet to a helicopter blade |
FR2787366B1 (fr) | 1998-12-17 | 2001-02-16 | Eurocopter France | Procede et dispositif d'enlevement d'une plaque retenue par adhesif a une piece support |
FR2791293B1 (fr) * | 1999-03-23 | 2001-05-18 | Sonats Soc Des Nouvelles Appli | Dispositifs de traitement de surface par impacts |
DE60105830T2 (de) * | 2001-12-21 | 2006-03-09 | Siemens Ag | Verfahren zum Entfernen einer Metallschicht eines Schichtsystems |
DE102008036713A1 (de) * | 2008-08-07 | 2010-02-11 | Technische Universität Carolo-Wilhelmina Zu Braunschweig | Verfahren zum Trennen zweier über zumindest eine Klebschicht miteinander verklebter Objekte |
US9409383B2 (en) * | 2008-12-22 | 2016-08-09 | Apple Inc. | Layer-specific energy distribution delamination |
FR2970197B1 (fr) | 2011-01-11 | 2013-12-20 | Snecma | Procede de desolidarisation/solidarisation par induction d'une piece mecanique magnetique collee a une piece mecanique. |
FR2989607B1 (fr) * | 2012-04-19 | 2014-05-09 | Snecma | Procede de realisation d'un renfort metallique avec insert pour la protection d'un bord d'attaque en materiau composite |
FR2992243B1 (fr) * | 2012-06-20 | 2015-02-13 | Snecma | Procede de decollement par choc laser |
FR2993896B1 (fr) * | 2012-07-26 | 2014-08-22 | Snecma | Procede de collage et de decollement entre deux pieces utilisant un adhesif charge |
KR102112905B1 (ko) * | 2014-06-27 | 2020-05-19 | 에리히 탈너 | 제1 기판을 제거하기 위한 샘플 홀더, 장치 및 방법 |
FR3025735B1 (fr) * | 2014-09-17 | 2016-12-09 | Europe Tech | Procede de traitement d'une piece composite |
FR3043685B1 (fr) * | 2015-11-13 | 2021-03-12 | Snecma | Procede de collage d'un film de protection sur une piece de forme complexe |
US10138732B2 (en) * | 2016-06-27 | 2018-11-27 | United Technologies Corporation | Blade shield removal and replacement |
FR3056605B1 (fr) | 2016-09-29 | 2020-12-18 | Safran Aircraft Engines | Dispositif de traitement chimique d'une piece de turbomachine munie d'un element de surface metallique |
US20190061073A1 (en) * | 2017-08-25 | 2019-02-28 | United Technologies Corporation | Separating adhesively bonded lap joints |
-
2019
- 2019-02-04 FR FR1901069A patent/FR3092267B1/fr active Active
-
2020
- 2020-02-04 US US17/427,321 patent/US11731221B2/en active Active
- 2020-02-04 EP EP20709268.5A patent/EP3921113A1/de active Pending
- 2020-02-04 JP JP2021544546A patent/JP2022524292A/ja active Pending
- 2020-02-04 CN CN202080015784.9A patent/CN113474117B/zh active Active
- 2020-02-04 CA CA3128288A patent/CA3128288A1/en active Pending
- 2020-02-04 BR BR112021015211-3A patent/BR112021015211A2/pt unknown
- 2020-02-04 WO PCT/FR2020/050178 patent/WO2020161426A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
CN113474117B (zh) | 2024-02-20 |
CA3128288A1 (en) | 2020-08-13 |
CN113474117A (zh) | 2021-10-01 |
US11731221B2 (en) | 2023-08-22 |
FR3092267A1 (fr) | 2020-08-07 |
JP2022524292A (ja) | 2022-05-02 |
US20220143766A1 (en) | 2022-05-12 |
WO2020161426A1 (fr) | 2020-08-13 |
BR112021015211A2 (pt) | 2021-09-28 |
FR3092267B1 (fr) | 2021-04-09 |
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