Black anodized aluminium carrier with bright bare-metal machined pockets and a bare central bore

Finishing guide

Bare-metal contacts on anodized parts

Anodizing creates an electrically insulating aluminium-oxide layer on the surface, so any grounding or bonding area has to be kept uncoated or have the coating removed afterwards. There are two common approaches: mask the area before anodizing, or machine the coating away after it.

Why anodizing interrupts electrical continuity

Anodizing converts the outer skin of the aluminium into aluminium oxide. That layer is what gives the part its corrosion resistance, its hardness and its colour — and it is also a dielectric. A few micrometres of anodic coating can raise contact resistance enough to prevent reliable electrical bonding.

How much this matters depends on the part. For many purely structural components it is irrelevant. For electrically bonded housings, actuator components and shield interfaces it can be critical — an actuator housing bonding the motor casing to chassis ground, a joint housing carrying a shield termination, a stator cover with an M2.5 grounding screw.

On these parts, surface-finish requirements directly affect electrical performance, so the conductive contact areas should be defined before the machining and finishing process is planned.

Cross-section of an anodized wall showing film growth and a masked bare zone The anodic film grows roughly half outward from the original machined surface and half into the parent metal. Where the surface is masked, no film forms and the metal stays at its as-machined dimension and remains conductive. PARENT ALUMINIUM Anodic film part grows outward · part penetrates the metal Masked zone — bare metal, conductive stays at the as-machined dimension no film, no dimensional change coated: the surface shifts by part of the coating thickness

The dashed line is the as-machined surface. Everything to the left of the divider is coated; everything to the right was masked and therefore did not receive the anodic coating.

Route 1 — mask before anodizing

Masking prevents a selected face, bore or thread from receiving the anodic coating. Plugs, die-cut decals, purpose-made silicone stop-offs and hand- or robot-applied lacquer all do the job; which one is right depends on the geometry and the quantity.

  • Nothing is disturbed after coating. The masked feature largely retains its pre-anodize machined dimension — no additional setup, no re-fixturing, and no risk of chipping the coating at a cut edge.
  • Masking is well suited to production quantities. Once the mask tooling exists, the incremental cost per part is generally low and relatively stable across a production run.
  • It protects threads. Coating buildup on the thread flanks can reduce clearance and interfere with assembly; masking is the usual answer, and the face around the hole can be protected in the same operation.

Masking generally produces a less sharply defined coating boundary than machining, because there is always a small transition where the mask sat. The rack that carries the part through the process also leaves a contact point that cannot be coated, so it is worth placing that point on a non-functional face at the drawing stage rather than discovering it at inspection.

Masking is a well-established production process, but its repeatability depends on mask design, application and condition. Over repeated cycles, worn plugs or fixtures can allow small amounts of solution to reach the protected area, leaving coating where the drawing called for bare metal.

This variation is typically detected during inspection rather than controlled by the machining operation itself. Where the exposed-metal boundary or the final dimension is especially critical, post-anodize machining gives tighter control.

Route 2 — finish-machine after anodizing

The alternative is to anodize the whole part and then selectively remove the anodic coating where bare metal is required: a light finish cut on a face, a spot-face under a screw head, a bore taken to size, or a thread cut after coating.

The advantage is control: the coating is removed by a cutting tool working to a toolpath, so the location and size of the exposed area do not depend on how a mask performed in the process tank.

  • The boundary can be controlled more precisely — the bare-metal boundary and area are defined directly by the machining toolpath rather than by how well a mask was applied.
  • The final dimension is controlled directly. Where a feature is both a precision fit and a contact area, machining it last removes the coating-thickness allowance from the calculation.
  • It requires an additional setup — re-fixturing a finished, coated part with additional handling precautions to avoid damaging the finished surface, plus the risk of chipping the coating at the edge of the cut.
  • It intentionally removes local corrosion protection from the machined area. That is the intent, but it should be a deliberate decision rather than a side effect.
The trade in one line: masking is typically more economical, while post-anodize machining gives tighter control over the location and dimensions of the exposed metal. Where electrical continuity is critical, the additional machining operation may be preferable to relying solely on masking repeatability, and may justify the additional setup cost.

Which route for which feature

The question that settles it is what the bare-metal area is for. Many masking requests are driven primarily by dimensional requirements rather than conductivity — a tapped hole whose nut has to run freely, a seal groove, a locating hole. There the concern is that film build-up disturbs a size, and if a small amount of coating reaches the protected area, the result may be a cosmetic defect or a dimensional deviation.

Where the reason is electrical, the consequences of partial anodic coverage are different: coating left on part of a grounding pad raises contact resistance rather than shifting a dimension slightly. Masking is used successfully for electrical contact areas across the industry, so this is a selection question rather than a rule.

In practice we choose between the two on required contact resistance, boundary precision, corrosion protection, production volume and repeatability. Post-anodize machining is most useful where the conductive area or its dimensions must be tightly controlled.

Our typical approach by feature is shown below. Dimensional requirements are usually masked; for electrical requirements we more often machine after anodizing, depending on the contact-resistance and boundary requirements.
FeatureWhy it stays bareUsual route
Tapped hole, nut must run freelyDimensional — coating buildup on the thread flanks can interfere with assemblyMask
Sealing grooveDimensional — film changes the section and the seal squeezeMask
Dowel / locating holeDimensional — the finished position and size must remain within toleranceMask
Bearing bore or tight fitDimensional, but the final tolerance must be controlledMask, or machine after if the band is tight
Grounding / bonding padFunctional — it must maintain a low-resistance electrical connectionUsually machine after anodizing
Grounding-screw boss or threadFunctional — it is part of the grounding pathUsually machine after anodizing
Shield termination / EMC bond faceFunctional — partial anodic coverage can increase contact resistance and reduce bonding reliabilityUsually machine after anodizing

Production quantity changes the cost trade-off within the dimensional group: the higher the quantity, the more masking tends to pay. It shifts it less for electrical requirements, where the concern is contact resistance rather than a few micrometres of size.

What drives the cost of post-anodize machining

Machining after anodizing is not priced by how much metal comes off — the actual material removal is usually minimal. It is priced by the fixture and the mounting: building or refitting a fixture that holds a finished, coated part without marking it, plus the labour of loading and indicating each piece.

That gives you a design lever worth using before the part is frozen. Keep the features that need machining after anodizing inside one operation type. If every one of them can be reached in a single milling setup, adding another accessible feature — a tapped hole, a second pad, a spot-face — may add little incremental machining cost, because it can be completed within the same setup. But if one bare zone is a turned feature and another is a milled feature, the part needs an additional fixture and setup, and the cost increases more noticeably.

On planet carriers and joint housings this is usually easy to arrange, because the conductive faces tend to sit at the same end of the part. Grouping these features during the design stage can reduce later fixturing and setup cost.

What the film does to your dimensions

The coating does not simply sit on top of the part. Part of it builds up outward from the original surface and part of it penetrates into the parent metal, so an external surface grows and a bore diameter decreases. On a diameter the effect applies from both sides.

The split is not the same for both processes. As a nominal rule a Type II sulphuric coating builds up roughly a third of its thickness outward, while a Type III hardcoat is closer to half and half. Actual dimensional change varies with alloy and process conditions, so the figures below are nominal — we confirm the critical fits on your part rather than working from a table.

Our usual coating ranges and the nominal dimensional effect. The thicknesses are our facility's usual process, not an industry definition of Type II or Type III; build-up is nominal and varies with alloy and process.
ProcessFilm thicknessChange per faceChange on a diameterMicrohardness
Our usual Type II (cosmetic)3–5 µm≈ 1–1.7 µm≈ 2–3.5 µm≈ 300–400 HV
Our usual Type III (hardcoat)8–25 µm≈ 4–12.5 µm≈ 8–25 µm≈ 400–600 HV

Anodic coating hardness is measured as microhardness in Vickers (HV), not Rockwell C — the coating is a thin ceramic layer and a macro-indenter is not valid on it.

A worked example. A Ø50 H7 bore has a tolerance band of +0.025 / 0 mm, so the total tolerance band is 25 µm. At a 4 µm Type II coating the bore closes by roughly 3 µm, around an eighth of the band, which can often be accommodated without special compensation, depending on the starting machined size. At a 20 µm Type III coating it closes by roughly 20 µm, a large portion of the available tolerance band, before any machining variation is counted. A bore in that situation is normally masked, machined oversize by a calculated allowance, or finish-machined after coating.

A practical guide: thin Type II coatings can often be accommodated within an H7 band, while thicker Type III coatings frequently require an explicit allowance, masking, or post-anodize finishing. How much room you actually have depends on the nominal diameter, the coating thickness and where the machined dimension sits in the band — This should preferably be confirmed during quotation rather than discovered during final inspection.

Where the tolerance is measured — one of the most important notes on the drawing

A drawing that specifies Ø50 H7 and hard anodized without stating the sequence can be read two ways, and the two interpretations result in different finished dimensions. Read as pre-coating, we machine to the drawing dimension and the finished bore ends up undersize. Read as post-coating, we machine oversize by a calculated allowance, mask the bore, or machine it after coating.

Practice varies: some drawings dimension the machined substrate and control the coating separately in the finish notes. Where surface treatment can affect a critical tolerance, we confirm whether the requirement applies before or after finishing rather than making an assumption. Stating it on the drawing eliminates this ambiguity.

Calling it out on the drawing

GENERAL TOL: ISO 2768-mK
FINISH: BEAD BLAST + BLACK ANODIZE (TYPE II)
TOLERANCES APPLY TO FINISHED PART AFTER SURFACE TREATMENT

⌵x = NO ANODIZE, BARE METAL — ELECTRICAL CONTACT
  · FACE A (GROUND PAD)
  · 4× M2.5 AND SURROUNDING FACE
  · ⌀50 H7 BORE

A defined symbol with a clear legend is usually easier to interpret than a long general note: it puts the requirement on the face it applies to, and allows the programmer to identify the applicable surfaces directly from the drawing. Say why a zone is bare — "electrical contact" tells the shop it is functional, not cosmetic, and that a witness mark there is not acceptable.

Colour the faces in the 3D model. Where the CAD format preserves face colours, a colour-coded 3D model can make the affected surfaces easier to identify. The programmer can associate the post-anodize machining operation directly with those surfaces, rather than matching a symbol on a 2D sheet to a surface in space. On a casing with several bare areas on different planes, this is the difference between a firm quotation and one that requires additional contingency for interpretation uncertainty.
From our floor: the question we most often have to ask back is not where the bare-metal areas are — the drawing usually shows that. It is whether the toleranced fits are measured before or after anodizing. Answering that one line in your first email typically reduces back-and-forth and can shorten quotation lead time.

Bare aluminium re-oxidises — design for it

Aluminium forms a native oxide within minutes of being cut. It is only a few nanometres thick, unlike the anodic coating, but it means a bare contact face is never entirely oxide-free.

In practice the joint is designed around it. Fastener clamp load, a serrated washer designed to break through the native oxide layer, or a bonding strap will all establish metal-to-metal contact through it.

What this does mean is that a bare-metal area is not a permanent cosmetic feature. It will dull, and it may corrode over time, particularly in humid or aggressive environments, where the anodic coating would have protected it. Keep bare-metal areas as small as the electrical function allows, and put them where the assembly covers them.

When conductivity is required over a larger area: chemical conversion coating

Where most of the surface has to conduct, masking the majority of the part is not a practical approach. A chemical conversion coating — chem film or chromate conversion coating, specified under MIL-DTL-5541 — forms a very thin conversion layer that provides corrosion protection while maintaining much lower contact resistance than anodizing. Class 3 is intended for applications with a low-resistance requirement, such as bonding surfaces and chassis interfaces.

MIL-DTL-5541 Type II covers conversion coatings that contain no hexavalent chromium, and is commonly selected where RoHS compliance is required. Specific regulatory compliance should be confirmed against the chemistry and supplier documentation used for the job.

It is not a substitute for anodizing where hardness, wear resistance or a deep black cosmetic finish are required. It suits cases where the driving requirement is corrosion protection with retained conductivity across a whole surface rather than a localised pad.

Industry reference points for the electrical side: MIL-A-8625 covers anodic coatings and notes that they are insulating; MIL-DTL-5541 Type II Class 3 covers conductive conversion coatings; MIL-STD-464 is where the commonly referenced 2.5 mΩ value comes from, and there it applies to an individual faying-surface connection rather than to a whole installation.

How we hold it

The parts this guide covers — actuator casings, robot joint housings, gearbox covers, planet carriers — often combine a precision bore, a thin wall and a functional bare-metal area on the same component. We machine them on simultaneous 5-axis, which allows key bores and mating faces to be machined in one coordinate system where the geometry permits, reducing error introduced by repeated re-fixturing. Post-anodize bare-metal areas are completed in a separate repeatable setup when required.

Critical finished dimensions are verified after surface treatment using the measurement method appropriate to the feature, including CMM inspection where suitable (SEREIN CROMA-776, 700 × 700 × 600 mm, Renishaw PH10T head, in a temperature-controlled room), with a 2.5D optical VMM alongside it for flat work.

Related reading: Anodize Type II vs Type III for the finish itself, tolerances and ISO 2768 for what to tighten and what to leave general, and the application pages on planet carrier machining and robot actuator housing machining.

Black anodized aluminium gearbox housing half with bright bare-metal bearing bores and a bare sealing face

A black-anodized gearbox housing with its bearing bores and sealing face held bare. The bores are fits; the flange face carries the joint.

Common questions

Is anodized aluminium conductive?

No. The film is an aluminium-oxide ceramic and behaves as an insulator. Any surface requiring reliable electrical contact should either remain free of anodic coating — masked before anodizing — or have the coating removed afterwards.

Is it better to mask before anodizing or machine after?

It depends what the bare-metal area is for. Where the reason is dimensional — a tapped hole a nut must run freely in, a seal groove, a locating hole — masking is the usual choice and scales well. Where the reason is electrical, masking is also widely used, but coating left on part of a contact area raises contact resistance, so we weigh required contact resistance, boundary precision, volume and repeatability. Post-anodize machining is most useful where the conductive area or its dimensions must be tightly controlled.

How much does anodizing change a dimension?

Part of the coating builds up outward and part penetrates into the metal, so an external face grows and a bore closes. The split differs by process: nominally about a third outward for Type II and about half for Type III. Across our usual ranges that is roughly 1–1.7 µm per face at 3–5 µm Type II, and roughly 4–12.5 µm per face at 8–25 µm Type III, doubled on a diameter. It varies with alloy and process, so we confirm critical fits per job.

Do tolerances apply before or after surface treatment?

Unless the drawing says otherwise we read them as applying to the finished part after treatment, and we confirm it before cutting. It is one of the most consequential ambiguities on a drawing, because it directly affects the machining and finishing route.

Will a bare-metal area stay conductive?

A native oxide a few nanometres thick reforms within minutes. A properly designed clamped joint, serrated washer or bonding interface can establish reliable metal-to-metal contact through it, which is why grounding joints are designed around clamped contact rather than a permanently pristine surface.

Can you keep a threaded hole bare while anodizing the rest?

Yes — threaded holes and the face around them are routinely held bare through bead blast and anodize by masking. That is one finish with a protected zone, which is a different proposition from putting two different coatings on two zones of the same part.

Request a quote See all surface treatments

阳极氧化后,表面生成绝缘性的氧化铝膜,原有的金属接触面将失去直接导电能力。因此接地面、电磁搭接面和接地螺钉位置需要保持不成膜,或在氧化后将膜层去除。常用的两种做法是:入槽前遮蔽,或氧化后再加工。

为什么阳极氧化会切断接地回路

阳极氧化把铝件表层转化为氧化铝。这层膜带来耐蚀性、硬度和颜色,同时也是介电体。几微米的阳极氧化膜就可能显著提高接触电阻,使电气搭接失去可靠性。

影响程度因零件而异。对多数纯结构件而言影响不大;但对需要搭接的壳体类零件则很关键:执行器壳体需将电机外壳搭接到机身地,机器人关节壳体需引出屏蔽层,定子端盖上设有 M2.5 接地螺钉,都需要指定区域保持裸金属接触。

阳极氧化膜生长与遮蔽不氧化区示意剖面 氧化膜一部分向外生长、一部分向基体渗透。遮蔽区不成膜,尺寸保持加工态,并保持导电。 铝 基 体 阳极氧化膜 一部分向外生长 · 一部分渗入基体 遮蔽区 — 不氧化,可导电 尺寸保持加工态 不成膜,尺寸不变 成膜区:单面尺寸变化为部分膜厚

虚线为加工态表面。分界线左侧为成膜区,右侧为遮蔽区,因此未形成阳极氧化膜。

路线一:入槽前遮蔽

遮蔽是在阳极氧化前保护指定的面、孔或螺纹,使这些区域不形成氧化膜。橡胶塞、模切贴、定制硅胶保护套、手涂或机器人涂覆的保护漆都能做到,选哪种取决于结构和批量。

  • 处理后不再动刀。被遮蔽的特征基本保持阳极氧化前的机加工尺寸,不需要二次装夹,也不存在切削边缘崩膜的风险。
  • 适合批量生产。遮蔽工装建立后,单件增加的遮蔽成本通常较低,批量越大越经济。
  • 能保护螺纹。螺纹牙侧的膜层会减小配合间隙,严重时会影响螺钉装配;遮蔽是常规做法,螺纹孔周边接触面可以在同一工序中一并保护。

与后加工相比,遮蔽区的边界精度通常较低,并可能存在一定过渡区域。另外,挂具与零件的接触点必须导电,该处无法成膜,即常说的挂具印,建议在图纸阶段就将其安排在非功能面上。

遮蔽是成熟的量产工艺,但其一致性取决于遮蔽工装的设计、装配和使用状态。随着遮蔽工装反复使用,密封性能可能下降,从而产生局部渗液或保护区域局部成膜,在图纸要求不氧化的位置留下膜层。

这类偏差通常需要通过后续检验发现,机加工本身无法直接控制遮蔽过程中的渗液风险。对于边界或尺寸要求较高的功能面,氧化后加工的可控性更高。

路线二:氧化后精加工

另一种做法是整件先完成阳极氧化,再对需要保持裸金属的区域进行局部后加工:端面进行轻量精铣、螺钉头下锪一个平台、内孔铰到尺寸,或在氧化后攻丝。

这种做法的优势在于可控:膜层由刀具按刀路切除,裸金属区的位置和尺寸不依赖于遮蔽工装在槽内的密封一致性。

  • 边界位置可实现更高的加工控制精度,不氧化区域由刀路直接决定,而不取决于遮蔽的施加质量。
  • 最终尺寸可在后加工工序中直接控制。如果这个特征既是配合面又是导电面,最后加工可以避免将膜厚变化计入该特征的最终尺寸控制。
  • 要多一次装夹——已完成表面处理的零件重新装夹需要格外注意,切削边缘也存在崩膜风险。
  • 后加工区域会失去原有的阳极氧化防护层。这本来就是目的,但应当是主动选择,而不是顺带产生的结果。
一句话取舍:遮蔽通常成本更低,氧化后精加工则对裸金属区的位置和尺寸控制更为精确。若导电可靠性和边界精度要求较高,可优先考虑氧化后精加工,但需要增加二次装夹和加工成本,并避免将最终功能完全依赖于遮蔽工装的密封一致性。

不同特征怎么选

工艺选择主要取决于这块不氧化区域承担什么功能。客户提出遮蔽,多数时候是为了尺寸而不是为了导电——螺母要能顺畅拧入的螺纹孔、密封槽、定位销孔。这类情况担心的是膜厚影响尺寸;若遮蔽工装磨损导致少量处理液进入保护区域,通常表现为外观缺陷或尺寸与配合偏差。

若保留金属面的原因是电气,后果的性质不同:接触区局部残留膜层会提高接触电阻,而不只是尺寸小幅变化。行业内也广泛采用遮蔽来保留导电接触面,因此这是一个选型问题,而不是固定规则。实际选择时,我们依据接触电阻要求、边界精度、防腐要求、批量和一致性来判断;对导电区域或其尺寸需严格控制的场合,氧化后加工更合适。

本厂对各类特征的常规处理方式。尺寸要求通常用遮蔽;电气功能要求则根据接触电阻和边界精度要求,更多采用氧化后加工。
特征为什么要保持不氧化常用工艺选择
螺纹孔,螺母需顺畅拧入尺寸要求——螺纹牙侧膜层会减小配合间隙,影响装配遮蔽
密封槽尺寸要求——成膜改变槽形截面和密封件压缩量遮蔽
定位销孔尺寸要求——成品位置和尺寸需保持在公差内遮蔽
轴承孔或紧配合尺寸要求,且最终公差需受控遮蔽;公差带偏紧时氧化后加工
接地接触面 / 电气搭接面电气功能要求——需要保持低电阻电气连接多采用氧化后加工
接地螺钉安装凸台或螺纹电气功能要求——属于接地回路的一部分多采用氧化后加工
屏蔽层端接 / 电磁搭接面电气功能要求——局部成膜可能提高接触电阻并降低电磁搭接可靠性多采用氧化后加工

对于尺寸要求,生产批量会明显影响遮蔽与后加工之间的成本选择:量越大,遮蔽越划算。对电气功能要求的影响较小,因为那里关注的是接触电阻,而不是几微米的尺寸偏差。

氧化后加工的成本主要来自哪里

氧化后加工的成本不取决于切掉多少材料——实际切削量通常很小。成本主要在工装和装夹:要做一套能夹持已完成表面处理的零件、又不会碰伤它的工装,再加上逐件上下料和找正的工时。

由此得到一条在图纸定型之前就该用上的设计手段:把需要氧化后加工的特征放在同一类工序里。如果这些位置都能在一次铣削装夹内够到,再多加一处——一个螺纹孔、第二块接地面、一个沉台——通常只增加很少的加工成本,因为这些特征可在同一装夹内完成。但如果其中一处是车削特征、另一处是铣削特征,此时会增加独立工装和装夹工序,因此成本通常会明显上升。

行星架和关节壳体通常较容易做到这一点,因为导电面往往集中在零件的同一端。在设计阶段集中这些功能面,通常可以减少后续新增工装和二次装夹的成本。

膜厚对尺寸的影响

氧化膜不是单纯附着在表面:一部分向外生长,一部分向基体内渗透,因此外形尺寸增大、内孔尺寸减小,直径方向两侧同时受影响。

两种工艺的比例并不相同。按常用经验值,II 型约有三分之一的膜厚表现为外部增厚,III 型硬质氧化则接近一半。实际尺寸变化还与合金牌号和工艺条件有关,因此下表数值仅供参考,关键配合应结合实际合金、膜厚和工艺条件确认。

本厂常用膜厚范围及尺寸影响的参考值。表中膜厚为本厂常用工艺,并非 II 型 / III 型 的行业定义;外部增厚比例为经验值,随合金和工艺条件变化。
工艺膜厚单面变化直径变化显微硬度
本厂常用 II 型(装饰性)3–5 µm约 1–1.7 µm约 2–3.5 µm约 300–400 HV
本厂常用 III 型(硬质)8–25 µm约 4–12.5 µm约 8–25 µm约 400–600 HV

氧化膜硬度按显微硬度维氏(HV)计,不用洛氏 C(HRC)——膜层是很薄的陶瓷层,宏观压头在其上不成立。

举一个具体例子。Ø50 H7 内孔的公差带为 +0.025 / 0 mm,可用区间 25 µm。膜厚 4 µm 的 II 型氧化,孔径约收缩 3 µm,约占公差带的八分之一,通常无需专门处理。同样这个孔做 20 µm 的 III 型硬质氧化,孔径约收缩 20 µm,占用公差带的大部分,这还未计入加工波动。此类内孔通常采用遮蔽、按预计膜厚预留尺寸补偿量加工,或在表面处理后精加工。

参考判断:较薄的 II 型氧化通常可以在 H7 公差带内消化;较厚的 III 型硬质氧化则往往需要预留尺寸补偿量、遮蔽,或在氧化后精加工。实际余量取决于公称直径、膜厚以及加工尺寸在公差带内的位置,建议在报价阶段确认。

公差适用于表面处理前还是成品状态 —— 图纸上最重要的说明之一

一张图只写 Ø50 H7硬质阳极氧化,没有说明先后关系,即构成歧义,两种理解会得到不同的最终尺寸结果。如果按表面处理前尺寸理解,我们按图加工,成品孔径偏小;如果按成品尺寸理解,则需要按预计膜厚预留补偿量加工、遮蔽,或在氧化后精加工。

实际做法并不统一:有些图纸标注的是机加基体尺寸,膜层则在表面处理说明中单独控制。当表面处理可能影响关键公差时,我们会在开工前确认该要求按处理前还是处理后执行,而不作未经确认的假设。在图纸上写明可以永久消除这一疑问。

图纸怎么标注

通用公差:ISO 2768-mK
表面处理:喷砂 + 黑色阳极氧化(II 型)
公差按表面处理后的成品尺寸

⌵x = 不做阳极氧化 —— 导电接触面
  · A 面(接地面)
  · 4× M2.5 及周边端面
  · ⌀50 H7 内孔

明确的符号和图例通常比长段通用说明更容易正确执行:它把要求直接标在对应的几何面上,便于编程人员在三维模型中直接识别对应表面。也建议写明该区域保持不氧化的原因——注明"导电接触面",加工和表面处理人员即可明确判断这是功能面而非外观面,该区域应按功能面要求控制,不应出现影响接触或装配的表面缺陷。

在三维模型里用颜色区分不氧化面。图纸说明"要做什么",三维模型说明"做在哪里"。发送阳极氧化件时,最有价值的一份资料就是把不氧化面用不同颜色标出的三维模型。它直接省掉了理解和推断这一步:编程人员可以在三维模型中直接识别对应表面,并针对这些面编写氧化后的铣削工序,而不必把二维图上的符号逐一对应到空间中的某个曲面。对于不氧化区分布在多个不同平面上的壳体,这就是"能给出确定报价"和"只能按保守口径报价"的区别。
来自车间的建议:我们最常需要再次确认的,不是不氧化区在哪里——图纸一般都标得清楚,而是那些配合公差究竟按处理前还是处理后。在第一封邮件里把这一点写明,通常能省掉报价环节整整一天的往返沟通。

裸铝会重新氧化 —— 设计时要考虑

铝件切削后几分钟内就会长出自然氧化层,厚度只有几纳米,与阳极氧化膜不是一回事,但这也意味着"不氧化面"从来不是绝对的裸金属。实际使用中并不影响,因为接头本来就是按这个前提设计的:螺栓压紧力、能刺穿氧化层的齿形垫圈,或搭接编织带,都能穿透这层薄膜,实现金属与金属的直接接触。

需要注意的是,不氧化区不是长期稳定的外观特征。它会失去光泽,在潮湿环境中最终会在原本受氧化膜保护的位置出现腐蚀。因此不氧化区应在满足电气功能的前提下尽可能缩小,并优先布置在装配后被覆盖的位置。

整件导电的另一条路:铬酸盐转化膜(导电氧化)

如果零件大部分面积都需要导电,那么"大面积遮蔽"就是走错了方向。铬酸盐转化膜(化学转化膜,按 MIL-DTL-5541 标准)膜层极薄,在提供防腐蚀性能的同时保持导电性,其中 Class 3 专用于搭接面、机壳接口等低电阻要求的场景。MIL-DTL-5541 Type II 工艺采用非六价铬体系,常用于需要满足 RoHS 的场合;具体合规情况取决于实际使用的药水体系,我们会针对具体项目核对供应商文件。

它不能替代阳极氧化:需要硬度、耐磨或深黑外观时,仍然要走阳极氧化。当核心诉求是"整面既要防护又要导电"而不是"保住一小块导电区"时,转化膜才是对的答案。

电气侧可参考的标准:MIL-A-8625 规定阳极氧化膜,并指出其为绝缘层;MIL-DTL-5541 Type II Class 3 规定导电型转化膜;常被引用的 2.5 毫欧指标出自 MIL-STD-464,且该值针对单个搭接接触面,而非整套系统。

我们如何保证

本文涉及的这类零件——执行器壳体、机器人关节壳体、齿轮箱端盖、行星架——往往在同一个零件上同时有紧配合内孔、薄壁和功能性不氧化区。我们用五轴联动加工,把内孔、贴合面和不氧化面放在一次装夹内完成,它们之间的相互位置就不再取决于两套夹具是否一致。

表面处理后的配合尺寸在恒温计量室用三坐标复检(思瑞 CROMA-776,行程 700 × 700 × 600 mm,雷尼绍 PH10T 测头),平面类零件配合 2.5D 影像仪,并通过三坐标检测确认最终尺寸是否满足图纸要求。

延伸阅读:阳极氧化 II 型与 III 型了解膜层本身,公差与 ISO 2768了解哪些该严、哪些按通用公差,以及应用篇行星架加工机器人关节壳体加工

黑色阳极氧化铝合金齿轮箱壳体,轴承孔与密封面保持不氧化

黑色阳极氧化的齿轮箱壳体,轴承孔与密封面保持不氧化。内孔是配合面,法兰端面承担结合面功能。

常见问题

阳极氧化后的铝件还导电吗?

不导电。氧化膜是氧化铝陶瓷层,属于绝缘体。需要可靠导电的面应保持不形成氧化膜:入槽前遮蔽,或在氧化后去除膜层。

该选氧化前遮蔽,还是氧化后加工?

取决于这块不氧化面用来干什么。如果是尺寸原因——螺母要顺畅拧入的螺纹孔、密封槽、定位销孔——用遮蔽;遮蔽主要就是用在这类场合,批量越大越划算。如果是电气原因——接地面、搭接面、接地螺纹——则在氧化后加工。遮蔽靠工装,而工装会磨损;接地回路上局部成膜不是性能下降,而是功能失效。

阳极氧化会让尺寸变化多少?

一部分膜厚向外生长,一部分向基体渗透,因此外形尺寸增大、内孔尺寸减小。两种工艺比例不同:II 型约三分之一向外,III 型约一半。按本厂常用范围,3–5 µm 的 II 型单面约 1–1.7 µm,8–25 µm 的 III 型单面约 4–12.5 µm,直径方向翻倍。实际数值随合金和工艺变化,关键配合按零件确认。

图纸公差按处理前还是处理后?

实际做法并不统一,有些图纸标注的是机加基体尺寸。当表面处理可能影响关键公差时,我们会在开工前确认该要求按处理前还是处理后执行,而不作未经确认的假设。它决定了紧配合是遮蔽、预留尺寸补偿量,还是氧化后再精加工。

不氧化面能一直保持导电吗?

裸铝几分钟内就会重新生成几纳米厚的自然氧化层。这层膜很薄,螺栓压紧力、齿形垫圈或搭接带都能穿透,所以接地连接靠的是压紧接触的设计,而不是指望表面永远洁净。

能只让螺纹孔不上氧化膜吗?

可以。螺纹孔及其周边端面通过遮蔽,可以在喷砂和阳极氧化全过程中保持不氧化,这是本厂常规工序。注意这属于单一表面处理加保护区,与同一零件两个区域上两种不同镀层是两回事。

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