ASTM D2651-01(2008)
(Guide)Standard Guide for Preparation of Metal Surfaces for Adhesive Bonding
Standard Guide for Preparation of Metal Surfaces for Adhesive Bonding
ABSTRACT
This guide covers procedures for preparing various wrought metal surfaces for adhesive bonding. Surface treatment methods involving both mechanical and chemical techniques are included for aluminum alloys, stainless steel, carbon steel, titanium alloys, magnesium alloys, and copper and copper alloys. For aluminum alloys: vapor or non-etching alkaline degreasing; sulfuric acid-sodium dichromate or sulfuric acid-ferric sulfate solution etching; phosphoric and sulfuric acid anodizing; propriety cleaning; secondary bonding; brush plate bond etching; mechanical abrasion; electrochemical cleaning; and anodic etching may be used. For stainless steel: mechanical methods such as wire brushing, rubbing with metal wool, hand sanding, and dry sand, grit, or vapor blast honing; etching using sulfuric-nitric-hydrofluoric, hydrochloric-orthosphosphoric-hydrofluoric, sulfuric-sodium dichromate, sodium metasilicate, and hydrochloric-sulfuric-dichromate acid solutions; and vigorous scouring with wet cloth and commercial household cleaner may be used. Same mechanical methods as that employed in stainless steel and chemical etching by nitric-phosphoric acid solution may be used for carbon steel preparation. For titanium alloys: mechanical abrasion; hydrochloric-orthophosphoric-hydrofluoric acid solution etching; and chromic acid or fluoride anodizing may be used. Surface preparation for magnesium alloys which is closely associated with corrosion prevention shall involve vapor, alkaline-detergent solution, chromic acid, and sodium hydroxide acid degreasing; anodic treatment; and the use of conversion coatings and wash primers. Nitric acid-ferric chloride solution degreasing; sulfuric acid-dichromate-ferric sulfate solution etching; and chemical treatment by nitric-acid-sodium chlorite solutions may be used for copper and copper alloy preparation.
SCOPE
1.1 This guide covers procedures that have proved satisfactory for preparing various wrought metal surfaces for adhesive bonding. It does not address the preparation of cast metals.
1.2 Surface preparation methods are included for:
MetalSection Aluminum Alloys 7 Stainless Steel 8 Carbon Steel 9 Titanium Alloys10 Magnesium Alloys
Copper and Copper Alloys11
12
1.3 Procedures included herein are based on the commercial practice of numerous agencies and organizations. The methods may be revised or supplemented, as necessary, to include methods based on proven performance.
1.4 The surface preparation of metal systems used for qualification and quality control testing of the adhesive should be agreed upon by both manufacturer and user.
1.5 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only.
1.6 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
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Designation: D2651 − 01 (Reapproved2008)
Standard Guide for
Preparation of Metal Surfaces for Adhesive Bonding
This standard is issued under the fixed designation D2651; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
This standard has been approved for use by agencies of the Department of Defense.
INTRODUCTION
It is impossible and impractical to present a single surface-preparation method for a metal group,
such as aluminum alloys, stainless steels, magnesium alloys, etc.The wide variety of individual alloys
and heat treatments under each group, the fact that certain adhesives exhibit specific compatibilities
with surface preparation and the complexity and nature of parts being bonded preclude the use of an
all-inclusive procedure for a metal group. Procedures for aluminum alloys are well standardized,
possiblybecausemorebondinghasbeendonewiththesealloys.Preliminarytestsshouldbeconducted
with the specific adhesive and the exact lot of metals to determine performance.This is especially true
for stainless steel. The adhesive manufacturers’ recommendation should also be considered.
1. Scope priate safety and health practices and determine the applica-
bility of regulatory limitations prior to use.
1.1 This guide covers procedures that have proved satisfac-
tory for preparing various wrought metal surfaces for adhesive
2. Referenced Documents
bonding. It does not address the preparation of cast metals.
2.1 ASTM Standards:
1.2 Surface preparation methods are included for:
D907 Terminology of Adhesives
Metal Section
D1125 Test Methods for Electrical Conductivity and Resis-
Aluminum Alloys 7
Stainless Steel 8
tivity of Water
Carbon Steel 9
D2674 Methods ofAnalysis of Sulfochromate Etch Solution
Titanium Alloys 10
Magnesium Alloys 11 Used in Surface Preparation of Aluminum
Copper and Copper Alloys 12
D3933 Guide for Preparation of Aluminum Surfaces for
1.3 Proceduresincludedhereinarebasedonthecommercial
Structural Adhesives Bonding (Phosphoric Acid Anodiz-
practice of numerous agencies and organizations. The methods
ing)
may be revised or supplemented, as necessary, to include
2.2 ASM International Document:
methods based on proven performance.
Metals Handbook Volume V
1.4 The surface preparation of metal systems used for
2.3 Military Specifications:
qualification and quality control testing of the adhesive should
MIL-A-8625 Type II, Anodic Coatings for Aluminum and
be agreed upon by both manufacturer and user.
Aluminum Alloys
1.5 The values stated in SI units are to be regarded as the
MIL-M-3171 Magnesium Alloy, Processes for Pretreatment
standard. The values given in parentheses are for information
and Prevention of Corrosion
only.
MIL-M-45202 Magnesium Alloy, Anodic Treatment of
1.6 This standard does not purport to address all of the
safety concerns, if any, associated with its use. It is the
responsibility of the user of this standard to establish appro-
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
Standards volume information, refer to the standard’s Document Summary page on
the ASTM website.
1 3
ThisguideisunderthejurisdictionofASTMCommitteeD14onAdhesivesand Available from American Society of Metals (ASM International), 9639 Kins-
is the direct responsibility of Subcommittee D14.80 on Metal Bonding Adhesives. man Rd., Materials Park, OH 44073-0002, http://www.asminternational.org.
Current edition approved April 1, 2008. Published April 2008. Originally Available from Standardization Documents Order Desk, DODSSP, Bldg. 4,
approved in 1967. Last previous edition approved in 2001 as D2651 – 01. DOI: Section D, 700 Robbins Ave., Philadelphia, PA 19111-5098, http://
10.1520/D2651-01R08. www.dodssp.daps.mil.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
D2651 − 01 (2008)
2.4 SAE Standards: lar treatment method, such as, titration for hexavalent chro-
Aerospace Material Specification 2470 E Anodic Treatment mium (CrO ), iron, chlorides, aluminum, etc. A pH reading or
of Aluminum Base Alloy, Chromic Acid Treatment acid content of trichloroethane vapor degreasing solution, or
both, should be obtained. Standards should be established and
3. Terminology
records kept for such tests on each lot or vat of solution.
Recordsshouldindicatethecontinuousconditionsofsolutions,
3.1 Definitions—Many of the terms in this guide are defined
such as amount of constituents added to bring solutions within
in Terminology D907.
limits, amount of contaminants present and date prepared (see
4. Apparatus Methods D2674).
4.1 Trays or Pans, suitable for preparation of laboratory
5.4 Room Conditions for surface preparation as well as
specimens and small parts. Generally in production, a series of other adhesive bonding operations should be controlled for
tanks containing the necessary solutions is arranged with
temperatures of 18 to 24°C (65 to 75°F), relative humidity of
overhead cranes to transport parts to be prepared.Tanks should 40 to 65 %, air-filtered to remove dust and pressure maintained
be lined with suitable materials to resist the solutions, and
at slightly higher than ambient.
methodsforcirculatingthesolutionsandheatingwithtempera- 5.4.1 The time and conditions between surface preparation
ture controls should be included if required.
and applying adhesive primer, if used, and bonding are critical.
Usually, the time should not exceed 8 h and parts should be
4.2 Hooks, Baskets, Clamps, or other holding devices, may
covered or wrapped in Kraft paper. Prepared surfaces can
beusedtoconveypartsbeingprepared.Theuseofa300Series
change their characteristics on standing and adhesives vary
stainless steel for such equipment is suggested. Other metals
widely in their tolerance of adherend surface conditions. In
may be used if they are resistant to the solution used.
production bonding of complicated or large parts, the time
interval may exceed 8 h. Investigation should be made to
5. Conditions
determine the time limitation of the adhesive and the rate of
5.1 Handling—All parts during and after processing and
change on the surface of the adherend. On the basis of the
before bonding should be handled as little as possible and only
results of such an investigation, it may be possible to extend
with clean, lint-free cotton or nylon fabric gloves.
the length of time and establish standards for the interval
5.2 Water used for preparing solutions should be distilled,
between surface preparation and adhesive application to fit
steam condensate, demineralized, deionized or otherwise
production schedules. Contaminating operations in the area
treated, if necessary, to obtain a condition of not more than 50
should be avoided. Especially detrimental are paint or other
ppm of solids and have a pH between 5.5 and 10, or not more
spraying operations, processes using powdered materials, oil
than 50 ppm of dissolved solids and not over 30 micromhs
vapors from pumps and other machinery and spraying of mold
conductance (see Test Methods D1125). Rinsing may be done
release agents.
bysprayorbydippinginatankinwhichthewateriscirculated
5.5 Common Steps:
and constantly being renewed by an overflow method. After
5.5.1 Remove ink markings or stamped identifications from
removing from any rinse the water-break test is commonly
the metals. This can be accomplished by wiping with a cloth
used. If the water film is discontinuous, it indicates that the
wetted with a variety of commercial solvents, such as acetone,
process is unsatisfactory and must be repeated (see 5.5.4).
methyl ethyl ketone, lacquer thinner and naphtha.
Other methods, such as indicator paper and contact angle, have
5.5.2 The preferred degreasing method is vapor degreasing
been used to determine the effectiveness of the process.
with 1,1,1-trichloroethane. Commercial vapor degreasing
Rinsing should be sufficiently long and vigorous to assure
equipment is usually used. This equipment has a deep tank
removal of soluble residue chemicals, or particles. Critical
with provision for heating a chlorinated solvent to 82 to 87°C
specific temperatures are specified for the rinse water in some
(180 to 190°F). Parts are suspended in the vapor zone above
processes. Where not specified, temperature is not critical. The
the hot liquid and allowed to remain until there is condensation
number of times a process may be repeated depends upon the
and run off (approximately 5 min). This step is repeated if
amount of metal removed in relation to the tolerance require-
necessary until all visible contamination is removed. The parts
ments for the part and whether clad or bare metal is used.
are raised above the tank and allowed to dry thoroughly.
Generally, not more than two repeat treatments are permitted.
Previously bonded parts, such as honeycomb core materials,
NOTE 1—No entirely foolproof method exists to determine bondability
are usually not degreased due to difficulty in removing residue.
of a metal surface after preparation.Trial bonding followed by testing and
5.5.3 Following vapor degreasing, mechanical or chemical
evaluation against mechanical strength standards should be conducted to
cleaning methods are usually employed.
determine initial and continuous effectiveness of a method.
5.5.4 A water-break test is a common method used to
5.3 Solutions—The life of solutions should be standardized.
analyze surface cleanliness. This test depends on the observa-
The useful life of solutions depends upon the number and size
tion that a clean surface (one that is chemically active or polar)
of the parts being prepared. Solutions should be sampled
will hold a continuous film of water, rather than a series of
periodically and analyzed for materials pertinent to the particu-
isolated droplets. This is known as a water-break-free condi-
tion. A break in the water film indicates a soiled or contami-
nated area. Distilled water should be used in the test, and a
Available from Society of Automotive Engineers (SAE), 400 Commonwealth
Dr., Warrendale, PA 15096-0001, http://www.sae.org. drainage time of about 30 s should be allowed. Any trace of
D2651 − 01 (2008)
residual cleaning solution should be removed or a false 7.4.4 Sulfuric Acid Anodizing—Amethod found suitable for
conclusion may be made. If a water-break-free condition is not bare aluminum (nonclad), machined, or chemically milled
observed on the treated surface, it should not be used for parts which must be corrosion protected is to anodize with
bonding. The surface should be recleaned until the test is sulfuric acid. Do not seal the anodized parts with boiling water
passed. If continuous failures occur, the treating process itself before bonding. Do not allow the time interval between
should be analyzed to determine the cause of the problem. treatment and bonding to exceed 72 h, and cover or wrap all
parts during the interval with a non-contaminating vapor
6. Report
barrier material.
6.1 Thereportforallmethodsconsistsofflowcharts,record
NOTE 2—Details of the process are contained in Specification AMS
sheets or other methods that indicate all steps in the surface
2470 E or Military Specification MIL-A-8625.
preparation used, with spaces for entries made upon comple-
7.4.5 Proprietary Cleaners—Some proprietary, commer-
tion of each step.
cially available metal surface preparations have been found
suitable for preparing the surfaces for adhesive bonding.
ALUMINUM ALLOYS
Full-scale property tests should be run with the metal surfaces
so prepared with the adhesive in question before accepting the
7. Procedure
process.
7.1 Aluminum alloys may be pretreated with many different
7.4.6 Secondary Bonding—When secondary bonding
methods, using both acidic and basic cleaners.
(bonding of parts that contain previously bonded areas) or
7.2 A typical pretreatment would normally involve the
repair of a disbonded assembly in service is necessary, it is
following steps:
usually impossible and undesirable to immerse these parts in
7.2.1 Vapor degrease or non-etching alkaline cleaner,
surface-preparation solutions without destroying or harming
7.2.2 Rinse,
the original adhesive bond. Satisfactory surface preparations
7.2.3 Acid or alkaline, and
have been accomplished by using paste-type etchants. These
7.2.4 Rinse.
paste systems can be made by adding fumed silica to the
sulfuric-dichromic acid solutions. The application of these
7.3 After 7.2.4, the parts may be dried or they may be given
an anodizing treatment. pastesystemsallowsfortheiruseinfairlycontrolledareas.The
etching time is generally 10 to 20 min. Exercise extreme care
7.4 Typical pretreatments are listed in 7.4.1. Refer to the
to ensure removal of all traces of the etchant. A thorough
appropriate literature for details on cleaning techniques and
rinsing with distilled water may be necessary to ensure
procedures.
complete removal. Several commercial products are available.
7.4.1 Alkaline degreasing solutions may be used instead of,
Somecommercialcompoundsundertheclassificationof“wash
or in addition to, vapor degreasing. Commercially available
primers” have been found to perform satisfactorily in place of
proprietary solutions may be used. A common degreasing
the paste type systems. Bond strengths obtained using either of
method is to immerse for 10 min at 70 to 82°C (160 to 180°F)
these surface preparations are somewhat lower than those from
in the following solution by weight: 3.0 parts sodium metasili-
the immersion processes.
cate, 1.5 parts sodium hydroxide, 0.5 parts sodium dodecyl-
7.4.7 Brush Plate Bond Etch (Stylus Method):
benzene sulfonate, such as Nacconol 90G , to 133.0 parts
water. 7.4.7.1 General—This method of electrochemical surface
preparation, although not widely known, has been effectively
7.4.2 Acid etching solutions typically used are the follow-
ing: demonstrated for small batch runs where tanks and other
capital-intensive methods might have been used.Almost all of
7.4.2.1 Sulfuric Acid/Sodium Dichromate (optimized FPL
etch). thesolutions,“brushes”(orstyli),andelectricalpowersupplies
are proprietary. When this method is used, the entire “family”
Material Concentration
Sulfuric Acid (66°Be or Baume) 38 to 41.5 oz/gal (287.9 to 310.0 g/L)
of proprietary items should be used; mixed usage of items
Sodium Dichromate 4.1 to 9.0 oz/gal (28–67.3 g/L)
between vendors should not occur.
Aluminum Alloy–2024 bare 0.2 oz/gal (1.5 g/L), min
T
...
This document is not anASTM standard and is intended only to provide the user of anASTM standard an indication of what changes have been made to the previous version. Because
it may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current version
of the standard as published by ASTM is to be considered the official document.
Designation:D2651–90(Reapproved 1995) Designation: D 2651 – 01 (Reapproved 2008)
Standard Guide for
Preparation of Metal Surfaces for Adhesive Bonding
This standard is issued under the fixed designation D 2651; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (e) indicates an editorial change since the last revision or reapproval.
This standard has been approved for use by agencies of the Department of Defense.
INTRODUCTION
It is impossible and impractical to present a single surface-preparation method for a metal group,
such as aluminum alloys, stainless steels, magnesium alloys, etc.The wide variety of individual alloys
and heat treatments under each group, the fact that certain adhesives exhibit specific compatibilities
with surface preparation and the complexity and nature of parts being bonded preclude the use of an
all-inclusive procedure for a metal group. Procedures for aluminum alloys are well standardized,
possiblybecausemorebondinghasbeendonewiththesealloys.Preliminarytestsshouldbeconducted
with the specific adhesive and the exact lot of metals to determine performance.This is especially true
for stainless steel. The adhesive manufacturers’ recommendation should also be considered.
1. Scope
1.1 This guide covers procedures that have proved satisfactory for preparing various wrought metal surfaces for adhesive
bonding. It does not address the preparation of cast metals.
1.2 Surface preparation methods are included for:
Metal Section
Aluminum Alloys 7
Aluminum Alloys 8
Stainless Steel 8
Stainless Steel 9
Carbon Steel 9
Carbon Steel 10
Titanium Alloys10 11
Titanium Alloys 11
Magnesium Alloys 12
Copper and Copper Alloys11 13
Magnesium Alloys 12
Copper and Copper Alloys 13
1.3 Proceduresincludedhereinarebasedonthecommercialpracticeofnumerousagenciesandorganizations.Themethodsmay
be revised or supplemented, as necessary, to include methods based on proven performance.
1.4 The surface preparation of metal systems used for qualification and quality control testing of the adhesive should be agreed
upon by both manufacturer and user.
1.5This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility
of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory
limitations prior to use.
1.5 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only.
1.6 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility
of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory
limitations prior to use.
This guide is under the jurisdiction of ASTM Committee D-14 on Adhesives and is the direct responsibility of Subcommittee D14.80 on Metal Bonding Adhesives.
Current edition approved Nov. 30, 1990. Published January 1991. Originally published as D2651–67. Last previous edition D2651–79(1984).
This guide is under the jurisdiction of ASTM Committee D14 on Adhesives and is the direct responsibility of Subcommittee D14.80 on Metal Bonding Adhesives.
Current edition approved April 1, 2008. Published April 2008. Originally approved in 1967. Last previous edition approved in 2001 as D 2651 – 01.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.
D 2651 – 01 (2008)
2. Referenced Documents
2.1 ASTM Standards:
D 907Terminology Relating to Adhesives Terminology of Adhesives
D 1125 Test Methods for Electrical Conductivity and Resistivity of Water
D 2674 Methods of Analysis of Sulfochromate Etch Solution Used in Surface Preparation of Aluminum
D 3933 Guide for Preparation of Aluminum Surfaces for Structural Adhesives Bonding (Phosphoric Acid Anodizing)
2.2 ASM International Document:
Metals Handbook Volume V
2.3 Military Specifications:
MIL-A-8625 Type II, Anodic Coatings for Aluminum and Aluminum Alloys
MIL-M-3171 Magnesium Alloy, Processes for Pretreatment and Prevention of Corrosion
MIL-M-45202 Magnesium Alloy, Anodic Treatment of
2.4 SAE Standards:
Aerospace Material Specification2470—AnodicSpecification 2470 E Anodic Treatment of Aluminum Base Alloy, Chromic
Acid Treatment
3. Terminology
3.1 Definitions—Many of the terms in this guide are defined in Terminology D 907.
4.
5. Apparatus
4.1
5.1 Trays or Pans, suitable for preparation of laboratory specimens and small parts. Generally in production, a series of tanks
containing the necessary solutions is arranged with overhead cranes to transport parts to be prepared. Tanks should be lined with
suitable materials to resist the solutions, and methods for circulating the solutions and heating with temperature controls should
be included if required.
4.2
5.2 Hooks, Baskets, Clamps, or other holding devices, may be used to convey parts being prepared. The use of a 300 Series
stainless steel for such equipment is suggested. Other metals may be used if they are resistant to the solution used.
5.
6. Conditions
5.1
6.1 Handling—All parts during and after processing and before bonding should be handled as little as possible and only with
clean, lint-free cotton or nylon fabric gloves.
5.2Water6.2 Water used for preparing solutions should be distilled, steam condensate, demineralized, deionized or otherwise
treated, if necessary, to obtain a condition of not more than 50 ppm of solids and have a pH between 5.5 and 10, or not more than
50 ppm of dissolved solids and not over 30 micromhosmicromhs conductance (see Test Methods D 1125). Rinsing may be done
by spray or by dipping in a tank in which the water is circulated and constantly being renewed by an overflow method. After
removing from any rinse the water-break test is commonly used. If the water film is discontinuous, it indicates that the process
is unsatisfactory and must be repeated (see 5.5.46.5.4). Other methods, such as indicator paper and contact angle, have been used
to determine the effectiveness of the process. Rinsing should be sufficiently long and vigorous to assure removal of soluble residue
chemicals, or particles. Critical specific temperatures are specified for the rinse water in some processes. Where not specified,
temperature is not critical. The number of times a process may be repeated depends upon the amount of metal removed in relation
to the tolerance requirements for the part and whether clad or bare metal is used. Generally, not more than two repeat treatments
are permitted.
Asurfactant that has been found suitable for this purpose consists of a 50% mixture of a cationic and a fluochemical surfactant such as Zonyl FSC manufactured by E.I.
DuPont, Wilmington, DE 19898.
For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Customer Service at service@astm.org. For Annual Book of ASTM Standards
volume information, refer to the standard’s Document Summary page on the ASTM website.
Annual Book of ASTM Standards, Vol 15.06.
Available from American Society of Metals (ASM International), 9639 Kinsman Rd., Materials Park, OH 44073-0002, http://www.asminternational.org.
Annual Book of ASTM Standards, Vol 11.01.
Available from Standardization Documents Order Desk, DODSSP, Bldg. 4, Section D, 700 Robbins Ave., Philadelphia, PA 19111-5098, http://www.dodssp.daps.mil.
Available from ASM International, Metals Park, OH 44073.
Available from Society of Automotive Engineers (SAE), 400 Commonwealth Dr., Warrendale, PA 15096-0001, http://www.sae.org.
D 2651 – 01 (2008)
NOTE 1—No entirely foolproof method exists to determine bondability of a metal surface after preparation. Trial bonding followed by testing and
evaluation against mechanical strength standards should be conducted to determine initial and continuous effectiveness of a method.
5.3
6.3 Solutions—The life of solutions should be standardized. The useful life of solutions depends upon the number and size of
the parts being prepared. Solutions should be sampled periodically and analyzed for materials pertinent to the particular treatment
method, such as, titration for hexavalent chromium (CrO ), iron, chlorides, aluminum, etc. A pH reading or acid content of
trichloroethane vapor degreasing solution, or both, should be obtained. Standards should be established and records kept for such
tests on each lot or vat of solution. Records should indicate the continuous conditions of solutions, such as amount of constituents
added to bring solutions within limits, amount of contaminants present and date prepared (see Methods D 2674).
5.4
6.4 Room Conditions for surface preparation as well as other adhesive bonding operations should be controlled for
temperatures of 18 to 24°C (65 to 75°F), relative humidity of 40 to 65 %, air-filtered to remove dust and pressure maintained at
slightly higher than ambient.
5.4.1The6.4.1 The time and conditions between surface preparation and applying adhesive primer, if used, and bonding are
critical. Usually, the time should not exceed 8 h and parts should be covered or wrapped in Kraft paper. Prepared surfaces can
change their characteristics on standing and adhesives vary widely in their tolerance of adherend surface conditions. In production
bonding of complicated or large parts, the time interval may exceed 8 h. Investigation should be made to determine the time
limitationoftheadhesiveandtherateofchangeonthesurfaceoftheadherend.Onthebasisoftheresultsofsuchaninvestigation,
it may be possible to extend the length of time and establish standards for the interval between surface preparation and adhesive
application to fit production schedules. Contaminating operations in the area should be avoided. Especially detrimental are paint
or other spraying operations, processes using powdered materials, oil vapors from pumps and other machinery and spraying of
mold release agents.
5.56.5 Common Steps:
56.5.1 Remove ink markings or stamped identifications from the metals. This can be accomplished by wiping with a cloth
wetted with a variety of commercial solvents, such as acetone, methyl ethyl ketone, lacquer thinner and naphtha.
5.5.2The6.5.2 The preferred degreasing method is vapor degreasing with 1,1,1-trichloroethane. Commercial vapor degreasing
equipment is usually used. This equipment has a deep tank with provision for heating a chlorinated solvent to 82 to 87°C (180 to
190°F). Parts are suspended in the vapor zone above the hot liquid and allowed to remain until there is condensation and run off
(approximately 5 min). This step is repeated if necessary until all visible contamination is removed. The parts are raised above the
tank and allowed to dry thoroughly. Previously bonded parts, such as honeycomb core materials, are usually not degreased due
to difficulty in removing residue.
56.5.3 Following vapor degreasing, mechanical or chemical cleaning methods are usually employed.
5.5.46.5.4 Awater-break test is a common method used to analyze surface cleanliness.This test depends on the observation that
a clean surface (one that is chemically active or polar) will hold a continuous film of water, rather than a series of isolated droplets.
This is known as a water-break-free condition. A break in the water film indicates a soiled or contaminated area. Distilled water
should be used in the test, and a drainage time of about 30 s should be allowed. Any trace of residual cleaning solution should
be removed or a false conclusion may be made. If a water-break-free condition is not observed on the treated surface, it should
not be used for bonding. The surface should be recleaned until the test is passed. If continuous failures occur, the treating process
itself should be analyzed to determine the cause of the problem.
6.
7. Report
7.1 The report for all methods shall consistconsists of flow charts, record sheets or other methods that indicate all steps in the
surface preparation used, with spaces for entries made upon completion of each step.
ALUMINUMALLOYS
7.8. Procedure
78.1 Aluminum alloys may be pretreated with many different methods, using both acidic and basic cleaners.
7.2A8.2 A typical pretreatment would normally involve the following steps:
78.2.1 Vapor degrease or non-etching alkaline cleaner,
78.2.2 Rinse,
78.2.3 Acid or alkaline, and
7.2.48.2.4 Rinse.
7.3After 7.2.4
8.3 After 8.2.4, the parts may be dried or they may be given an anodizing treatment.
7.4Typical pretreatments are listed in 7.4.1
8.4 Typicalpretreatmentsarelistedin8.4.1.Refertotheappropriateliteraturefordetailsoncleaningtechniquesandprocedures.
D 2651 – 01 (2008)
7.4.1
8.4.1 Alkaline degreasing solutions may be used instead of, or in addition to, vapor degreasing. Commercially available
proprietary solutions may be used. A common degreasing method is to immerse for 10 min at 70 to 82°C (160 to 180°F) in the
following solution by weight: 3.0 parts sodium metasilicate, 1.5 parts sodium hydroxide, 0.5 parts sodium dodecylbenzene
sulfonate, such as Nacconol 90G , to 133.0 parts water.
78.4.2 Acid etching solutions typically used are the following:
78.4.2.1 Sulfuric Acid/Sodium Dichromate (optimized FPL etch).
Material Concentration
Sulfuric Acid (66°Be or Baume) 38 to 41.5 oz/gal (287.9 to 310.0 g/L)
Sodium Dichromate 4.1 to 9.0 oz/gal (28–67.3 g/L)
Aluminum Alloy–2024 bare 0.2 oz/gal (1.5 g/L), min
Temperature 66 to 71°C (150 to 160°F)
Immersion Time 12 to 15 min
78.4.2.2 P-2 Etch (Sulfuric Acid/Ferric Sulfate).
Material Concentration
Sulfuric acid (6.5 to 9.5 N) 27 to 36 % by weight
Ferric sulfate 135 to 165 g/L (18 to 22 oz/gal)
Temperature 60 to 65°C (140 to 150°F)
Immersion Time 10 to 12 min
7.4.3
8.4.3 Phosphoric Acid Anodizing can be performed in accordance with Guide D 3933.
7.4.4
8.4.4 Sulfuric Acid Anodizing—A method found suitable for bare aluminum (nonclad), machined, or chemically milled parts
which must be corrosion protected is to anodize with sulfuric acid.The anodized parts shall not be sealed Do not seal the anodized
parts with boiling water before bonding. The Do not allow the time interval between treatment and bonding should not to exceed
72 h, and al
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