Machined aluminium twin-bore gearbox and actuator housing with counterbored bolt patterns

Application guide

Robot actuator housing machining

The machining challenge in a robot joint or actuator housing is not usually one individual feature. It is maintaining the relationship between several precision features on a thin-walled structure designed to minimise mass.

Coaxial bearing bores, a flat output flange, a thin structural wall and a bare-metal contact area all have to be controlled on the same component. This guide covers how each is held, and why they are best machined in one setup.

Coaxial bores drive gear alignment

The housing maintains alignment of the gearset along a common axis. Whether the drive is a planetary stack, a strain-wave unit with a circular spline, or a cycloidal design, the bearing seats at each end of the housing define where that axis actually sits. If they disagree, the gears run misaligned regardless of the accuracy of the gears themselves.

Bearing and spline seats in this class of part are commonly specified at H7, and H6 where the design is tight on runout. For example, depending on the applicable ISO size range, a 70 mm bore gives a band of roughly 30 µm at H7 and 19 µm at H6.

The size band is usually the more straightforward requirement. The harder one is coaxiality between the bores — a relationship rather than a dimension, which measuring each bore individually will not confirm.

If a housing drawing tolerances each bore tightly but never says how the bores relate to each other, it is under-specified. Add the coaxiality callout and the datum it references — it is the requirement that actually protects the gearset.

Thin walls, and why they move

Robotics housings are weight-driven, so wall thickness is reduced as far as the structure allows — low single millimetres is common. The cutter is rarely the limit. Distortion is.

  • Clamping force elastically deforms a thin wall. A wall held round in the fixture can relax into an oval when released, after the bore was machined round.
  • Cutting force deflects the workpiece. The tool pushes the wall away and it recovers behind the cut, leaving a bore that measures differently along its length.
  • Residual stress redistributes as material is removed. Taking most of a billet away lets the remaining material move, which is why a part can be in tolerance at the machine and out of it the next morning.

The solution is a controlled process rather than heavier cutting or clamping: rough with material left on, allow the part to stabilise between operations, then take light finishing passes with fixturing that supports the wall rather than squeezing it. It is slower than cutting the part in one pass, and it is the difference between a housing that measures correctly once and one that measures correctly every time. The general treatment is in thin-wall aluminium machining.

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

A housing half with its bearing bores and sealing rib held bare through the anodize. The bores are fits; the rib is a joint face.

The output flange has to be flat

The face where the housing meets the output stage — or the next link in the arm — carries the joint. If it is not flat, bolting it up pulls the housing out of shape and pushes the bores it was supposed to protect out of alignment. Worse, the distortion concentrates stress at whichever bolt closes last, which is a fatigue problem rather than an assembly problem.

This is why a flange face on this class of part usually carries two separate controls rather than a generic surface note: a flatness requirement on the face itself, and an orientation requirement — typically perpendicularity — to the bearing-bore datum axis. Flatness is a form control and takes no datum; the relationship to the axis has to be called out separately.

It is also why the face and the bores are best cut in the same setup. Machined separately, their relationship carries the additional re-fixturing error between the two setups.

The post-anodize fit problem

Many aluminium actuator housings are anodized — for wear resistance, for corrosion protection, or to achieve a required cosmetic finish such as black anodizing. That has a direct dimensional consequence for the bores: part of the coating builds up outward from the bore surface, nominally about a third of its thickness for Type II and about half for Type III, so a toleranced bore closes.

Across our usual ranges, a 3–5 µm Type II coating reduces a bore diameter by roughly 2–3.5 µm, which an H7 band usually absorbs. An 8–25 µm Type III hardcoat reduces it by roughly 8–25 µm, which on a 50 mm H7 bore can take up much of the band before any machining variation is counted. Such a bore is normally masked, machined oversize by a calculated allowance, or finish-machined after coating — a decision best taken at quotation rather than at inspection.

Worth knowing when you choose: a production mask is a fixture applied by hand, and its repeatability depends on mask design, application and condition. Over repeated cycles a worn seal can allow solution to reach the protected area. Where the exposed area or the final dimension is especially critical, post-anodize machining gives tighter control.

The same page covers the other half of the problem: keeping bonding and grounding faces conductive. See bare-metal contacts on anodized parts.

Bare zones, bonding and EMC

Because an actuator housing encloses the motor, encoder and drive electronics, the housing often forms part of the system's EMC and grounding strategy. Shield terminations, chassis bonds and grounding screws all require a metallic path, and the anodic coating that protects the housing will interrupt that path unless specific faces are kept uncoated or machined afterwards.

Practically, that means the housing drawing should identify: the ground pad and what it bonds to, any threaded hole taking an earth screw, and whether the bare-metal area is functional (a witness mark is not acceptable) or merely cosmetic. Bonding requirements in this space are often written against MIL-STD-464, where the frequently quoted 2.5 milliohm figure applies to an individual faying-surface connection rather than to a whole installation — worth knowing when a drawing note quotes it without context.

Machining the set, not just the part

An actuator is rarely a single part. A build typically includes a casing, a gearbox cover, a stator cover, an electronics cover, an output shaft, one or two planet carriers, an input shaft and a rotor support — parts that have to fit each other, not only satisfy their own drawings individually.

Machining them as a matched set and inspecting them together catches interface problems that per-part inspection can pass over: a bore and a shaft each in tolerance but at opposite ends of their bands, or a cover flange that is flat but not parallel to its mating face. For prototype builds, successful assembly often depends on controlling these interfaces as a system rather than evaluating each component in isolation.

Tote of turned aluminium actuator housing sleeves after machining

Turned housing sleeves in production. Prototype and production run on the same floor, so the process that proves out on the first pieces is the process that scales.

From our floor: the two questions that most often hold up an actuator quote are whether the bore tolerances are measured before or after surface treatment, and what the bores are coaxial to. Both are one line on the drawing. Answering them up front usually moves the quote a full day earlier. A third thing helps just as much and costs nothing: colour the no-anodize faces differently in the STEP file, so the post-anodize milling operation can be written straight against them.

How we hold it

Housings run on simultaneous 5-axis so the bores, the flange face and the bare-metal areas share a single setup and their mutual position depends on the machine rather than on re-fixturing. Milling envelope is 2000 × 1200 × 800 mm on 5-axis and 2500 × 1200 × 800 mm on 3-axis, with a minimum feature size of Ø0.50 mm; turning goes to Ø500 × 580 mm, with Swiss work on bar from Ø32–42 mm for the shafts.

Inspection is on a temperature-controlled CMM (SEREIN CROMA-776, 700 × 700 × 600 mm, Renishaw PH10T) with a 2.5D optical VMM alongside, reporting coaxiality, flatness and the post-treatment fits as related features. Certification is ISO 9001:2015, IATF 16949:2016 and AS9100D / EN 9100:2018, with batch-level material traceability. Quotes in 48 hours, no minimum order.

Related reading: planet carrier machining, 6061 vs 7075, and the industry page for robotics CNC machining.

Common questions

What tolerance do actuator housing bores need?

Bearing and circular-spline seats are commonly specified at H7, and H6 where the design is tight on runout. What usually matters more than the size band is coaxiality between the bores at each end of the housing, because that is what keeps the gearset aligned along its axis.

Why machine a housing in one setup?

Coaxiality, flange perpendicularity and the bare contact zone are relationships between features, not properties of any one feature. In one simultaneous 5-axis setup those relationships depend on the machine's accuracy; split across setups they depend on how well the fixtures agreed, which is a larger and less predictable error.

How thin can a housing wall be?

Weight-driven robotics housings often run walls in the low single millimetres. The limit is rarely the cutter — it is distortion, because a thin wall moves under clamping load and springs back under cutting force. The answer is staged machining with roughing, a settling pause and light finishing passes, plus fixturing that supports rather than squeezes.

Do you machine the whole actuator set or single parts?

Either. Housings, covers, output shafts, planet carriers and bearing flanges can be machined as a matched family and inspected together — usually what a prototype build actually needs, because the parts have to fit each other rather than just fit their own drawings.

Can grounding zones be kept bare through anodizing?

Yes. Faces and threaded holes carrying an electrical connection are held bare through bead blast and anodize by masking, or the film is machined away afterwards where the boundary has to be exact or the feature is also a toleranced fit.

Request a quote Robotics CNC machining

机器人关节或执行器壳体的加工难点,通常不在于某一个特征本身,而在于多个关键特征之间的相互位置必须同时得到保证;同时零件通常采用薄壁轻量化设计,整体刚性有限。

具有严格轴线关系要求的轴承孔、平整的输出法兰面、薄壁结构和导电接触面,这些特征及其相互位置都需要在同一个零件上同时受控。本文逐项说明各项如何保证,以及为什么关键关联特征应尽量在同一坐标系和装夹条件下完成。

同轴孔系决定齿轮对中

壳体的职责是把整套齿轮系约束在一条轴线上。无论传动形式是行星组、带刚轮的谐波单元,还是摆线结构,壳体两端的轴承位就定义了这条轴线的实际位置。若两端轴承孔的轴线关系超差,齿轮系可能在偏心或偏斜状态下运行;即使齿轮本身精度很高,也可能因此受到影响。

这一类零件的轴承位和刚轮安装位常见按 H7 标注,对跳动要求严格的设计会用到 H6——以 70 mm 孔为例,H7 公差带约 30 µm,H6 约 19 µm。尺寸公差往往是相对容易的部分,更难的是控制两端孔轴线之间的几何关系——它是一种位置关系,而非单一尺寸;仅分别测量两个孔的直径,无法验证两条轴线之间的几何关系。

如果壳体图纸把每个孔的尺寸标得很严,却没有说明孔与孔之间的关系,仅有孔径公差还不足以完整定义这一功能要求。建议根据所采用的 GD&T / GPS 标准明确相应的几何公差及基准体系——这一几何关系对保持齿轮系对中非常重要。

薄壁为什么会走形

机器人壳体以轻量化为导向,在满足结构强度的前提下尽可能减薄壁厚,局部壁厚常只有数毫米,具体取决于结构和载荷要求。限制通常不是刀具,而是变形。

  • 夹紧力会使薄壁区域产生弹性变形。加工时看似合格,松夹后回弹可能导致孔径、圆度或位置发生变化。
  • 切削力会使工件变形。切削力会使薄壁发生弹性偏移,刀具通过后材料回弹,孔沿轴向各处测出来的尺寸就不一致。
  • 残余应力会释放。从整块料上去掉大部分材料后,剩下的材料会移动——这就是零件在机床上合格、第二天早上超差的原因。

可行的做法是依靠工艺控制,而不是加大切削量或夹紧力:粗加工留余量,安排中间稳定工序,再用轻切削精加工,同时工装尽量增加支撑面积并降低局部夹紧力。这比一次重切削完成慢,但更有利于获得稳定的批次一致性,而不是只在单次测量中满足公差。通用做法见薄壁铝件加工

黑色阳极氧化铝合金齿轮箱壳体,轴承孔与密封筋保持不氧化

阳极氧化后仍保持不氧化的壳体轴承孔与密封筋。孔是配合面,筋是结合面。

输出法兰面的平面度与方向关系

壳体与输出级、或与机械臂下一节连接的端面承担整个接头。如果法兰面平面度不足,装配拧紧后可能使壳体产生附加变形,进一步影响轴承孔系的对中关系。变形还可能在局部连接区域产生附加载荷和应力集中,因此这不仅影响装配,也可能影响长期疲劳寿命。

因此这类零件的法兰面通常需要两项分开的要求,而不是笼统的表面说明:端面自身的平面度,以及相对轴承孔基准轴线的方向要求(通常为垂直度)。平面度属于形状公差,不引用基准;与轴线的位置关系需要单独标注。

在结构和加工条件允许时,端面与关键孔系也应尽量在同一装夹内建立几何关系。分开加工时,两者的位置关系会额外引入两次装夹之间的重复定位误差。

氧化后的配合问题

很多铝合金执行器壳体需要做阳极氧化,用于耐磨、防腐,或满足黑色等外观要求。这直接影响精密配合孔的最终尺寸:氧化膜有一部分从孔壁向内生长(II 型约为膜厚的三分之一,III 型约为一半),因此公差孔的孔径会减小。

普通 II 型阳极氧化(本厂常用膜厚 3–5 µm)通常使孔径减小约 2–3.5 µm,实际值随合金和工艺条件变化,对部分 H7 配合可以通过预先的尺寸控制进行容纳;硬质阳极氧化(8–25 µm)名义上约减小 8–25 µm,对 50 mm 的 H7 孔来说,还没算加工波动就已占用公差带的较大比例。此时通常需要考虑遮蔽、预留尺寸补偿量或氧化后精加工。这类工艺选择应在报价和工艺规划阶段确定,而不是留到最终检验时再处理。

选型时还要知道一点:遮蔽通常需要逐件安装保护工装或遮蔽材料,工装反复使用后可能发生磨损,从而影响密封和重复性,处理液可能进入保护区域,在图纸要求不氧化的位置形成膜层。对于边界位置或最终尺寸要求较高的区域,氧化后精加工通常能提供更直接的尺寸控制。

关于接地面和电气搭接面的处理方式,可参见阳极氧化件的导电接触面

不氧化区域、搭接与电磁兼容

由于执行器壳体同时包覆电机、编码器和驱动电子元件,壳体也是系统接地与 EMC 设计的一部分。屏蔽层端接、机壳搭接和接地螺钉都需要金属通路,而阳极氧化膜会增加接触电阻并阻隔直接金属导通,除非指定面保持不成膜或在氧化后加工去除。

具体来说,壳体图纸应当标明:接地面的位置及其搭接对象、承担接地螺钉的螺纹孔,以及该不氧化区域属于功能面(不接受挂具印或夹伤)还是仅为外观。这一领域的搭接要求常引用 MIL-STD-464;需要注意的是,常被引用的 2.5 毫欧指标针对的是单个搭接接触面,而不是整套系统——图纸上不带上下文引用这个数字时,值得留意。

做的是整套零件,不只是单件

执行器很少只有一个零件。一台样机通常包括壳体、齿轮箱端盖、定子端盖、电气端盖、输出轴、一到两个行星架、输入轴和转子支撑——需要保证配套零件之间的实际装配关系,而不仅是分别满足各自的单件尺寸要求。

作为配套零件一并加工、统一检测,能发现单件检测发现不了的接口问题:孔和轴各自合格但分别落在公差带两端;端盖法兰平但与配合面不平行。对样机项目而言,最终判断标准通常是整套零件能否顺利装配并实现设计功能,而不仅是每个零件单独通过尺寸检验。

加工完成的铝合金执行器壳体套筒批量周转

批量生产中的车削壳体套筒。打样与量产在同一厂完成,打样阶段验证通过的工艺,就是放量时沿用的工艺。

来自车间的建议:最常拖慢执行器报价的两个问题是:孔的公差按表面处理前还是处理后计,以及孔的同轴度相对什么基准。两者在图纸上都只是一行字。提前写明,报价通常能提前整整一天。还有一件同样有用、且不增加任何成本的事:在 STEP 文件里把不氧化区域用不同颜色标出,氧化后的铣削工序就能直接针对这些面来编写。

我们如何保证

壳体在五轴联动上加工。在几何条件允许时,关键孔系和法兰基准尽量在同一装夹内完成,以减少多次装夹带来的重复定位误差;需要氧化后加工的功能面则采用独立、可重复定位的二次工序。五轴行程 2000 × 1200 × 800 mm,三轴 2500 × 1200 × 800 mm,最小特征 Ø0.50 mm;车削可至 Ø500 × 580 mm,配套轴类可走 Ø32–42 mm 棒料的走心机。

检测在恒温计量室的三坐标(思瑞 CROMA-776,700 × 700 × 600 mm,雷尼绍 PH10T)配合 2.5D 影像仪完成,关键轴线关系、法兰平面度与方向要求,以及表面处理后的最终配合尺寸,可作为关联特征进行检测和记录。资质为 ISO 9001:2015、IATF 16949:2016 与 AS9100D / EN 9100:2018,材料按批次可追溯。48 小时报价,无起订量。

延伸阅读:行星架加工6061 还是 7075,以及行业页机器人零件加工

常见问题

执行器壳体的孔要控到什么公差?

轴承位与刚轮安装位常见按 H7 标注,对跳动要求严格的设计用 H6。除孔径尺寸外,两端孔轴线之间的几何关系同样重要,它会直接影响齿轮系能否保持设计要求的对中状态。

为什么壳体要一次装夹加工?

同轴度、法兰垂直度和不氧化区域都是特征之间的关系,不是单个特征的属性。在一次五轴联动装夹内,这些关系可在同一坐标系中建立,从而减少重复装夹误差;拆成多次装夹,则会引入多套夹具和多次定位带来的累积误差。

壁厚能做到多薄?

以轻量化为导向的机器人壳体,壁厚常做到几毫米以内。限制通常不是刀具而是变形:薄壁在夹紧力下产生弹性变形,切削力下发生弹性偏移并在切削后回弹,残余应力也会随材料去除重新分布。可行做法是粗加工、安排中间稳定工序、轻切削精加工,配合高支撑、低局部夹紧力的工装。

能整套零件一起做吗?

可以。壳体、端盖、输出轴、行星架和轴承法兰可作为配套零件一并加工、统一检测——样机阶段通常需要的正是这一点,因为需要保证配套零件之间的实际装配关系,而不仅是分别满足各自的单件尺寸要求。

接地面能在阳极氧化中保持不氧化吗?

可以。承担电气连接的端面和螺纹孔通过遮蔽即可在喷砂和阳极氧化全过程保持不氧化;若边界要求特别清晰,或该特征同时是公差配合,则在氧化后把膜层加工掉。

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Robotics components machined at Fenva Precision

Actuator components

Robot joint and actuator housings, prototype through production.

Housings, covers, output shafts and carriers, machined on simultaneous 5-axis so the bores, the flange face and the bare-metal areas share one setup, and inspected together on a temperature-controlled CMM. Quote in 48 hours, no minimum order.