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Landing Gear Ups and Downs: the Eccentric Arc Surface in a Deep Hole

A landing gear leg carries the airframe on an eccentric arc surface that sits inside a deep bore. This page explains how that surface is generated, why hardness above 53 HRC changes the cutting mechanics, and which process window holds the arc profile without chatter.

±0.005 mmRa 0.2–0.8 μmUp to 53+ HRC5-axis capable
Aerospace CNC machining of a landing gear eccentric arc surface
Short version

Key takeaways

Eccentric, not roundThe contact surface is an offset arc, so wall thickness changes around the axis.
Hardness sets the toolAbove 53 HRC the cut belongs to CBN or ceramic, not coated carbide.
Depth drives chatterA long boring bar is the weak link; stiffness matters more than spindle speed.
Measure the arc, not the boreCMM or air gauge must reference the eccentric axis, not the outer diameter.
Geometry

Why the landing gear eccentric arc surface sits inside a deep hole

A landing gear leg is not a straight column with a round bore. The upper and lower ends of the frame are offset, and the pin that carries the wheel or the drag brace has to swing about an axis that is not the bore center. That offset is what makes the bore surface eccentric. The arc radius is larger than the bore radius on one side and smaller on the other, so the wall thickness changes as you rotate around the axis.

In service the landing gear takes two loads at once. The leg bends from the ground reaction, and the eccentric surface takes a rotating contact load from the pin. The arc, not the round bore, is the surface that sets contact stress and wear. If the arc is off by a few hundredths of a millimeter, the pin contact moves to one edge and the load path is no longer what the stress analysis assumed.

That is why the eccentric arc usually carries a tolerance near ±0.005 mm and a finish in the Ra 0.8–1.6 μm band, with critical bands down to Ra 0.2–0.8 μm. The bore depth often runs several times the arc diameter, so the cutting tool reaches far from the spindle nose. Deep-hole geometry and a hard material together are the two constraints that decide the whole process.

Mechanics

What hardness above 53 HRC does to the cut

Many landing gear pins and sleeves run at 53 HRC or harder, and some tool steel grades sit higher than that after heat treatment. At this hardness the material no longer forms a clean shear plane ahead of the edge. The chip comes off in segments, cutting pressure spikes, and most of the heat goes into the tool tip instead of the chip.

Coated carbide still works below roughly 45 HRC. Above 50 HRC the edge breaks down fast, and the failure is not gradual. The flank wears, the cutting force climbs, and then the edge chips. In a deep hole you may not see that until the arc profile has already drifted out of tolerance.

The practical answer is polycrystalline cubic boron nitride (PCBN) or a ceramic grade, run dry or with minimal lubrication, at surface speeds far higher than carbide would tolerate. A 60–120 m/min band is a normal starting range for PCBN in hardened steel, with depth of cut kept light. The trade is clear: the tool costs more, but it holds size across a long boring pass.

Chatter

Chatter is the real limit, not the material

A boring bar that reaches 4× its diameter or more is a spring. When the cutting force varies, the bar deflects, the depth of cut changes, and the force varies again. That loop is regenerative chatter, and it shows up as a wavy arc surface with a pitch equal to the chatter frequency. In a deep eccentric bore the bar is also unsupported on one side, because the arc is offset.

Three knobs control it. Shorten the overhang if the part can be turned around. Increase the bar diameter until it nearly touches the bore wall, which also raises the bar's static stiffness. Then tune the spindle speed: a stability lobe diagram for the specific bar and holder will show a sweet spot where the same depth of cut becomes stable.

If chatter persists, reduce the radial engagement and take more passes. On a 5-axis machine with a Ø400 mm rotary table, the part can be indexed so the eccentric arc is cut with the shortest possible tool. That single setup change often removes more vibration than any speed adjustment.

Setup

How to hold the work and reference the eccentric axis

Everything depends on the datum. If the part is clamped on the outer diameter and the eccentric axis is assumed to be concentric, the arc will be right on the machine and wrong on the CMM. The correct reference is the eccentric axis itself, established from the pin bore or from a machined face that the design already ties to that axis.

For hard, thin-walled gear legs, clamping pressure is a real risk. A three-jaw chuck closed hard will ovalize the bore, and the part springs back after unclamping. Soft jaws bored to the actual part diameter, plus a light clamp force, keep roundness inside the tolerance band.

A mill-turn center or a 5-axis machine with a rotary table lets the bore and the opposite face be machined in one setup. One setup removes the stack-up error that comes from re-chucking, and it is usually worth more than a tighter machine spec. We run this kind of work on 16 simultaneous 5-axis centers and 16 mill-turn centers, with a maximum processing size of 4,000 mm.

Process window

Parameters that hold the landing gear bore in tolerance

A workable starting point for a hardened steel landing gear bore: PCBN or ceramic insert, surface speed 60–120 m/min, feed 0.05–0.15 mm/rev, depth of cut 0.10–0.30 mm per side. Keep depth of cut below the bar's stability limit rather than pushing feed. Feed changes the finish; depth of cut changes the vibration.

Cooling matters more than it looks. PCBN generally runs dry or with air blast, because thermal shock from flood coolant can crack the edge. Ceramic grades behave the same way. If the setup needs lubrication for chip evacuation, use a directed minimum-quantity stream and keep it steady.

Then verify. Rough the bore, leave 0.2–0.3 mm, stress-relieve if the drawing allows it, and finish in a separate pass with a freshly indexed edge. Measure the arc on a CMM or with an air gauge set to the eccentric axis. One pass of roughing without a finish allowance is the most common way a good setup still produces an out-of-tolerance arc.

Selection

Which tool and setup for which bore condition

Match the process to hardness, depth and volume.

Bore conditionTool choiceSetupWhen it stops working
Below 45 HRC, depth under 3×DCoated carbide boring bar3-axis or mill-turnBar overhang passes 4×D
45–55 HRC, depth 3–6×DPCBN insert, light depth of cut4-axis with tailstock supportFlood coolant on the PCBN edge
Above 55 HRC, depth over 6×DCeramic or PCBN, dry cutting5-axis, single setupThin wall distorts under clamp load
Eccentric arc, tight profilePCBN, reduced radial engagementRotary table, part indexedDatum taken from outer diameter
One-off prototype, soft stockCarbide, then heat treat3-axis plus finish grindHeat treat moves the arc off size

What we would choose

For a hardened landing gear bore with an eccentric arc, run PCBN or ceramic dry in one 5-axis setup and leave a real finishing allowance. If the part is still soft and the volume is low, cut it with carbide before heat treatment and grind the arc afterward.

FAQs

Landing gear bore questions

Can the eccentric arc be cut on a 3-axis machine?

Yes, if the part can be positioned so the eccentric axis lines up with the spindle. That usually needs a fixture with an offset pilot, or the part turned in a second setup.

The risk is the second setup. Re-chucking adds stack-up error, and on a deep bore that error shows up directly in the arc profile. A 4-axis or 5-axis setup removes it.

Why does the bore go out of round after unclamping?

The wall is thin and the clamp load is high. The bore is round while the jaws hold it and springs back oval once they open.

Use soft jaws bored to the part diameter, reduce clamp force, and check roundness with the part free. A ±0.005 mm arc tolerance leaves little room for springback.

What surface finish should we ask for?

Ra 0.8–1.6 μm covers most landing gear bore surfaces and is reachable with PCBN at moderate feed.

Where the pin contact pressure is high, Ra 0.2–0.8 μm is reasonable. That usually means a lighter finishing pass or a fine boring head, and it adds time.

How do we know the arc is right before shipment?

Measure it on a CMM or an air gauge referenced to the eccentric axis, not the outer diameter. Report the arc radius and the profile along the bore length.

We inspect 100% of parts before shipment, covering raw material check, in-process monitoring and final inspection, with reports on request.

Does heat treatment come before or after machining?

For steel above 53 HRC, heat treat first, then bore with PCBN or ceramic. Cutting soft and hardening afterward lets the arc move during quench.

If the drawing allows, a stress-relief step between roughing and finishing keeps the bore stable.

What if the boring bar chatters no matter the speed?

Shorten the overhang, increase bar diameter, or index the part so the arc is reached with a shorter tool. Reducing radial engagement and adding passes is the fallback.

Chasing the speed alone rarely fixes a bar that is simply too long for the bore.

Send us the landing gear drawing

Upload the part and we return a quotation with free DFM analysis within 12 hours.

12-hour quote±0.005 mm100% inspectionNDA on request

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