Five-axis machining centre cutting an aluminium planetary reducer component on a trunnion table

Application guide

Planet Carrier Machining: How Pin-Bore Accuracy Affects Load Sharing

A planetary reducer gets its torque density by dividing load across several planets instead of one gear pair. Accurate pin location in the carrier helps the planets share that load as intended; position errors can cause one planet to engage more heavily than the others, reducing fatigue life.

Real load sharing also depends on gear errors, carrier deflection, pin flexibility, bearing stiffness and any floating members in the design. The carrier is one of the larger contributors a machine shop controls directly.

What the carrier actually controls

The carrier is a structural part with a metrology job. It holds each planet pin at a fixed radius and a fixed angular spacing, keeps the two flanges square to the output axis, and transmits the resulting torque to the output shaft. Every one of those functions is a machining feature:

  • Pin-bore position — radius and angular spacing, which influence which planet begins carrying load first and how the load divides.
  • Bore-to-bore consistency — the bores must match each other, not just their nominal size.
  • Alignment of corresponding pin bores in the two flanges — misalignment tilts the planet pin relative to the gearbox axis.
  • Perpendicularity of the flange faces to the gearbox datum axis, and parallelism between opposing flange faces where the assembly requires it.
  • The output interface — spline or bolted flange, located relative to the same functional datum system.
Machined aluminium planet carrier plate with pin bores and a bolted pin pattern

A carrier plate with its pin pattern. Everything the gearset does downstream depends on where those holes ended up relative to each other and to the output axis.

Pin-bore position is the load-sharing lever

If every planet pin sat at exactly the right radius and spacing, the planets would share load evenly. In practice there is always some residual position error, and a pin-position error can cause one planet to enter load earlier than the others and carry a disproportionate share of the load.

Gear-design literature often analyses pin-spacing errors in the tens-of-micrometres range in published examples, with planet bores matched to each other within single-digit micrometres in some published load-sharing studies, and examines pin-position standard deviations of a few micrometres.

These are illustrative figures from published analysis and should not be used as general drawing tolerances. The required tolerance for a given design depends on gear geometry, architecture, stiffness and the target load-sharing factor. What does generalise is the direction: for load sharing, consistency in pin-axis position is often as important as the individual bore-diameter tolerance.

A drawing can tightly control bore diameter yet still allow excessive variation in the pin pattern. For load sharing, the relative position of the pin axes must therefore be controlled in addition to bore size.

Why the two flanges are bored together

Most carriers are a two-plate structure — a flanged body and a cover, or two flanges joined by webs — and each planet pin spans both. If the two halves are bored in separate operations, the pin's parallelism to the output axis depends on the agreement between two setups. Inspection can identify the resulting error, but it cannot eliminate the setup-to-setup tolerance stack.

A common approach is to clamp the flanges together in their assembled relationship and bore the pin holes through both at once, so their alignment is established in the same machining setup rather than through two independent setups. It costs a fixture and a dedicated operation, and it reduces one of the major process-related sources of pin-axis misalignment. For designs where pin alignment is critical to load sharing, machining the corresponding bores in one setup is generally the preferred process.

We do the same thing in a different way for one-piece carriers: bore the pin holes, the output interface and the bearing seats in a single simultaneous 5-axis setup, so their relationship is controlled within one coordinate system, reducing error introduced by repeated re-fixturing.

Parallelism, perpendicularity and the face relationship

A carrier can meet individual size tolerances and still fail functionally if the geometric relationships are out of tolerance. The flange faces have to be perpendicular to the datum axis, parallel to each other where the assembly requires it, and flat enough that bolting the assembly together does not pull the pins out of line.

Bolt-up distortion is a real failure mode: a carrier that measures within tolerance in the unassembled condition can move out of tolerance after the assembly is bolted and torqued.

This is why carrier drawings usually include more geometric callouts than size callouts, and why the inspection report should verify the relevant geometric relationships, not only individual dimensions. Where a feature is functional, it is worth tolerancing it geometrically and stating the datum it references.

Material, and what it means for the finish

Common carrier materials and the machining consequences.
MaterialChosen whenMachining / finish note
6061-T6 aluminiumApplications sensitive to weight and rotating inertia; moderate torque.Easy to hold tight bores. If anodized, the film closes the bores — see below.
7075-T6 aluminiumHigher strength at the same weight.Stronger but less corrosion-tolerant; anodize behaviour differs from 6061.
Structural steel (e.g. S235JR / 1.0038)Higher-load, cost-sensitive applications where mass is less critical.Bare carbon steel can develop surface rust quickly in storage or sea freight, particularly in humid conditions — specify a coating or protective oil, or ask us to.
Case-hardening steelWhere pin bores see high contact stress.Heat treatment can introduce distortion; critical bores are finish-ground or hard-turned afterwards.

A carrier drawing with no surface-treatment callout is a question rather than a default, so we ask rather than assume. This matters most on steel components, where an omitted surface-treatment note can result in corrosion during storage or transport.

If the carrier is aluminium and anodized

Part of the anodic coating builds up outward from the bore surface, so the bore closes. The nominal build-up differs by process — roughly a third of the coating thickness for Type II, about half for Type III — so a 3–5 µm Type II coating typically closes a bore by only a few micrometres, while an 8–25 µm hardcoat can take up much of an H7 band before any machining variation is counted.

Where that matters, the bores are normally masked, machined oversize by a calculated allowance, or finish-machined after coating.

Carriers frequently also need bare-metal areas for a ground path or a sensor reference. The full treatment of that is in bare-metal contacts on anodized parts.

Where backlash actually comes from

Backlash is a system-level characteristic influenced by gear accuracy, bearing arrangement, preload, fits, carrier geometry and assembly. The carrier is one contributor rather than the sole determining component.

In practice, carrier accuracy cannot compensate for errors in the other gear components, but carrier error can compromise the performance of an otherwise accurate gearset.

From our floor: one of the most useful things a carrier drawing can include is an explicit datum scheme — which face is A, which bore is B, and what the pin pattern is positioned to. A common issue we see is a tight positional callout with no stated datums, which usually requires additional clarification or contingency in the quotation.

How we machine and verify them

Carriers run on simultaneous 5-axis so the pin pattern, the output interface and the bearing seats share one setup. Envelope is 2000 × 1200 × 800 mm on 5-axis and 2500 × 1200 × 800 mm on 3-axis, with turning to Ø500 × 580 mm for the shaft and flange work that goes with a reducer build.

Verification is on a temperature-controlled CMM — SEREIN CROMA-776, 700 × 700 × 600 mm measuring volume, Renishaw PH10T motorised probe head — reporting pin-bore position, parallelism, perpendicularity and the flange relationships as a set rather than as isolated dimensions. Certification is ISO 9001:2015, IATF 16949:2016 and AS9100D / EN 9100:2018, with material traceable by batch.

Related reading: robot actuator housing machining, tolerances and ISO 2768, and the industry page for robotics CNC machining.

Common questions

Why does carrier accuracy matter so much?

A planetary set earns its torque density by dividing load across several planets, and the carrier decides where each pin sits. A severely mispositioned pin can cause its planet to enter load earlier and carry a disproportionate share, and can become one factor limiting fatigue life or load capacity.

What pin-bore tolerance does a carrier need?

It depends on ratio, module and duty. Gear literature commonly cites pin spacing in the region of a few hundredths of a millimetre with the bores matched to each other within single-digit micrometres where load sharing is critical. The right number for your gearbox comes from your own load-sharing analysis; we machine and verify to the print.

Why bore both flanges in one setup?

Every re-fixturing makes the relationship between the flanges depend on how well two setups agreed rather than on the machine's positioning. Clamping the flanges together and boring through both at once makes the holes coaxial by construction instead of by tolerance arithmetic.

Do you machine steel carriers as well as aluminium?

Yes. Aluminium where inertia and weight dominate, structural or case-hardening steels where pin seating and torque capacity dominate. Note that bare carbon steel can develop surface rust during storage or transport unless a coating or protective oil is specified.

Does anodizing affect the pin bores?

Yes, on aluminium carriers with toleranced bores. Part of the coating builds up outward from the bore surface — nominally about a third of its thickness for Type II, about half for Type III — so the bore closes. On hardcoat that can take up much of an H7 band, so the bores are normally masked, machined oversize, or finish-machined after coating.

Request a quote Robotics CNC machining

行星减速器之所以能做到高扭矩密度,是因为把载荷分摊到多个行星轮上,而不是只靠一对齿轮。这个分摊能否真正实现,取决于一个关键零件:行星架。行星架销孔的位置精度是影响均载效果的重要因素之一:位置精度越高,各行星轮越能按设计目标均匀分担载荷;位置误差过大则可能导致部分行星轮承担更高载荷,降低疲劳寿命。

实际的均载还受齿轮误差、行星架变形、销轴刚度、轴承刚度以及浮动构件等因素影响。行星架是其中加工环节能直接控制的一项。

行星架到底控制什么

行星架既是承载件,也是决定各行星销空间位置的精密定位件。它把每根行星销固定在确定的半径和角度位置上,保证两片法兰与输出轴线垂直,并把合成扭矩传给输出轴。每一项功能都对应一个加工特征:

  • 销孔位置——半径与角度分度,会影响各行星轮进入承载的先后与载荷分配。
  • 销孔之间的位置和尺寸一致性——各销孔需相互一致,而不只是各自接近名义尺寸。
  • 两侧对应销孔的轴线一致性——若行星销轴线与减速器输出轴线的平行度偏差过大,行星轮会相对轴线倾斜。
  • 法兰端面对减速器基准轴线的垂直度,以及装配有要求时两端面之间的平行度
  • 输出接口——如花键或螺栓法兰,应相对于同一功能基准体系进行控制。
加工完成的铝合金行星架板,带销孔与销轴装配孔位

带销孔阵列的行星架板。这些销孔之间以及相对输出轴线的位置关系,会直接影响后续装配和载荷分配。

销孔位置是均载的关键杠杆

如果所有行星销都恰好落在正确的半径和分度上,各行星轮就会均匀分担载荷。实际上做不到——总有残余位置误差,销孔位置误差可能使某个行星轮更早进入承载,并承担高于设计目标的载荷份额。

公开文献中的示例通常将销孔间距误差分析在几十微米量级,各销孔之间的一致性在个位数微米,均载研究也常考察几微米的销孔位置标准差。这些是公开文献中的参考数值,不应直接用作图纸公差;具体要求取决于齿轮参数、结构形式、刚度和目标均载系数。可以可以普遍借鉴的是这一原则:对于均载而言,销孔轴线之间的位置一致性往往与单个销孔尺寸公差同样重要。

即使每个销孔的直径都满足很严的尺寸公差,如果销孔阵列的位置关系控制不足,仍可能造成载荷分配不均。因此需要同时控制孔径和销孔轴线之间的相对位置。

两片法兰为什么要合起来镗

许多行星架采用两片式结构——带法兰的本体加端盖,或两片法兰由筋板连接——每根行星销同时穿过两片。如果两片分开加工,销轴与输出轴线的平行度就取决于两次装夹之间的一致性。检验可以发现这种累积误差,但无法消除由多次装夹产生的误差源。

常见做法是把两片按装配关系夹在一起,在装配关系下对对应销孔进行一次装夹加工,使对应销孔的轴线关系在同一次加工中建立,可减少两次独立装夹带来的累积误差。代价是增加一套夹具和一道专门工序,换来的是减少导致销轴轴线偏差的一项主要工艺误差来源。对于销轴对中对均载影响较大的设计,将对应销孔在一次装夹内加工通常是更可取的工艺。

整体式行星架我们用另一种方式达到同样效果:销孔、输出接口和轴承位在一次五轴联动装夹内完成,各关键特征在同一坐标系和装夹状态下建立关系,可减少重复装夹带来的定位误差。

平行度、垂直度与端面关系

即使各单项尺寸均合格,如果关键几何关系超差,行星架仍可能无法满足装配和运行要求。法兰端面必须与孔轴线垂直、两端面相互平行,且平面度满足要求,装配拧紧后不会导致销轴歪斜。装配变形是实际存在的失效模式:自由状态下测量合格的行星架,拧紧后可能超差。

这也是行星架图纸上形位公差往往比尺寸公差还多的原因,以及为什么检测报告和尺寸本身同样重要。对于功能相关特征,建议使用适当的几何公差并明确基准体系。

材料选择及其对表面处理的影响

常见行星架材料及其加工影响。
材料适用场合加工 / 表面处理提示
6061-T6 铝合金适用于对重量和转动惯量较敏感、载荷水平中等的应用。切削性能较好,适合加工精密配合孔。若做阳极氧化,膜层会使孔径减小,见下文。
7075-T6 铝合金同等重量下需要更高强度。强度更高但耐蚀性较弱,阳极氧化表现与 6061 不同。
结构钢(如 S235JR / 1.0038)承载能力要求较高、且成本敏感的应用。裸露碳钢在运输和储存过程中容易产生表面锈蚀,潮湿环境下尤其明显——建议在图纸中明确防护方式,如镀层、防锈油或其他表面处理;如未指定,我们会在报价前确认。
渗碳钢销孔承受较高接触应力。热处理可能引起变形,关键孔通常在热处理后通过精磨或硬车完成最终尺寸控制。

行星架图纸上没有表面处理标注时,这是一个需要确认的问题,而不是可以按默认处理,因此我们会主动询问。这一点对钢制零件尤为重要:漏标表面处理可能导致零件在储存或运输过程中锈蚀。

铝合金行星架做阳极氧化时

氧化膜有一部分从孔壁向内生长,因此销孔孔径减小。向外增厚的比例因工艺而异:II 型约为膜厚的三分之一,III 型约为一半。因此 3–5 µm 的 II 型氧化通常仅使孔径减小数微米;而 8–25 µm 的硬质氧化可能占用 H7 公差带的较大比例,这还未计入加工波动。

当这一点影响装配时,销孔通常采用遮蔽、按膜厚预留尺寸补偿量加工,或在表面处理后精加工。

行星架也常需要为接地回路或传感器基准保留导电面。完整做法见阳极氧化件的导电接触面

回差究竟来自哪里

回差属于整机系统性能,受齿轮精度、轴承布置、预紧、配合、公差链和装配状态等多项因素影响。行星架是其中一个贡献项,而不是唯一的决定性零件。

实际含义是:行星架精度无法弥补其他齿轮件本身的误差,但行星架误差会直接影响整套齿轮系的性能。

来自车间的建议:行星架图纸上最重要的信息之一,是明确的基准体系——哪个面是 A、哪个孔是 B、销孔阵列相对于哪个基准定位。在我们收到的行星架图纸中,一个比较常见的问题是位置度标注很严、却没有标注基准;这种情况通常需要进一步确认,或在报价中预留一定的解释风险。

我们如何加工与验证

行星架在五轴联动上加工,在几何条件允许时,销孔阵列、输出接口和轴承位尽量在同一装夹和坐标系内完成。五轴行程 2000 × 1200 × 800 mm,三轴 2500 × 1200 × 800 mm;与减速器配套的轴类和法兰件车削可至 Ø500 × 580 mm。

检测在恒温计量室的三坐标上完成——思瑞 CROMA-776,测量行程 700 × 700 × 600 mm,雷尼绍 PH10T 自动测头——销孔实测坐标与位置度、平行度、垂直度和端面关系作为一组关联特征出具报告,而不是孤立尺寸;其他尺寸根据特征选择相应量具。资质为 ISO 9001:2015、IATF 16949:2016 与 AS9100D / EN 9100:2018,材料按批次可追溯。

延伸阅读:机器人关节壳体加工公差与 ISO 2768,以及行业页机器人零件加工

常见问题

行星架的精度为什么这么关键?

行星传动靠把载荷分摊到多个行星轮上获得高扭矩密度,而分摊由行星架决定每根销的位置。位置误差较大的销孔可能使对应行星轮更早进入承载并承担过高载荷,并成为限制疲劳寿命或承载能力的因素之一。

行星架销孔要控到多少?

取决于速比、模数和工况。齿轮文献常见量级为销孔间距几十微米、孔与孔一致性个位数微米(用于均载要求高的机型)。具体数值应来自您自己的均载计算;我们按图加工并按图验证。

为什么两片法兰要一次装夹镗孔?

每重新装夹一次,两片之间的关系就取决于两次装夹是否一致,而不是机床定位精度。合起来一次镗穿,孔的同轴由工艺保证,而不是靠公差叠加。

钢制行星架也能做吗?

可以。对重量和转动惯量较敏感的应用用铝合金,对销轴承载能力和扭矩容量要求较高的应用用结构钢或渗碳钢。注意裸露碳钢在运输和储存过程中容易产生表面锈蚀,需指定镀层或防锈油。

阳极氧化会影响销孔吗?

铝合金行星架且销孔为公差配合时会有影响。氧化膜有一部分从孔壁向内生长(II 型约三分之一,III 型约一半),因此孔径减小。硬质氧化可能占用 H7 公差带的大部分,因此通常采用遮蔽、预留尺寸补偿量,或氧化后精加工。

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Five-axis milling cell at Fenva Precision

Reducer components

Planetary reducer components are regular work on our floor.

Carriers, output shafts, ring-gear housings and bearing flanges, single parts or the whole set, machined together and inspected together. CMM reports on pin position, parallelism and the face relationship. Quote in 48 hours, no minimum order.