CTR K

Power-Screw and Lead-Screw Torque and Efficiency

A power screw converts rotational motion into linear force — lifting a load in a screw jack, advancing a tool in a press, or positioning a valve stem. The central design questions are: how much torque does the drive motor or handle need to raise (and lower) the load, and will the screw hold position when the drive is released, or will it back-drive? Both answers depend on the thread geometry and friction through the same two torque equations, and getting them wrong is the most common cause of under-powered actuators and runaway jacks.

This guide walks through the Shigley raise/lower torque model — the method used in ASME B1.5 (Acme threads) and DIN 103 / ISO 2901 (metric trapezoidal threads) — including the modified friction coefficient for flanked thread forms, the collar torque contribution, the mechanical efficiency expression, and the self-locking condition. A short worked example links every step to the formulas so you can reproduce it by hand or verify it against the MechanixCalc power screw calculator.

Thread geometry and the modified friction coefficient

Three geometric parameters drive the torque equations. The mean thread diameter d_m = d − h sets the effective friction radius r_m = d_m / 2. The lead l (distance advanced per revolution; l = n_starts × pitch) determines the helix angle λ. The thread flank angle α controls how much of the normal force between mating threads acts radially — creating an extra wedging component that raises the effective friction.

For a flat (square) thread, α = 0 and the thread flanks are perpendicular to the screw axis, so the full normal force opposes axial motion and no radial wedging occurs. For an Acme thread (ASME B1.5, α = 14.5°) or a metric trapezoidal thread (DIN 103, α = 15°), the flanks are inclined and the radial component increases the contact force. The engine corrects for this by replacing the measured friction coefficient μ with a modified value μ′ = μ / cos(α). Buttress threads (α ≈ 7° on the load flank) fall between the two extremes. The self-locking condition and both torque expressions use μ′ throughout.

Lead angle and modified friction coefficient
λ = arctan(l / (π·d_m)) μ′ = μ / cos(α)

where λ = helix (lead) angle (degrees); l = lead [mm/rev]; d_m = mean thread diameter = d − h [mm]; μ = measured thread friction coefficient; α = thread flank half-angle (°): 14.5° Acme, 15° DIN 103 trapezoidal, 0° square, ≈7° buttress; μ′ = modified (effective) friction coefficient used in all torque expressions

Raise and lower torque — the full expressions

The raise torque has two additive parts: the thread torque T_thread (which does the work of lifting the load against thread friction) and the collar torque T_c (which overcomes friction at the thrust bearing or flat collar that reacts the axial load). The thread torque follows from the equilibrium of forces on the thread helix, expressed at the mean radius r_m. The collar torque is simply the product of the collar friction coefficient, the load, and the mean collar radius.

The lower torque expression is similar but with the sense of the friction term reversed. When the load attempts to drive the screw backwards, friction now partially assists the motion. If the load can overcome friction — that is, if tan(λ) > μ′ — the screw overhauls (back-drives) and a separate brake or holding device is required. When tan(λ) ≤ μ′, friction is sufficient to prevent back-driving and the screw is self-locking: a negative T_lower_thread confirms the load cannot move the screw unaided. The collar torque is always added in the same (positive) direction for both raising and lowering because the collar must always be overcome by the drive.

Raise torque — thread plus collar
T_raise = W · r_m · (l + π·μ′·d_m) / (π·d_m − μ′·l) + μ_c · W · (d_c / 2)

where T_raise = total raising torque [N·mm]; W = axial load [N]; r_m = d_m / 2 = mean thread radius [mm]; l = lead [mm]; μ′ = modified thread friction coefficient; d_m = mean thread diameter [mm]; μ_c = collar friction coefficient; d_c = mean collar (thrust bearing) diameter [mm]

Lower torque and self-locking condition
T_lower = W · r_m · (π·μ′·d_m − l) / (π·d_m + μ′·l) + μ_c · W · (d_c / 2) Self-locking when: tan(λ) < μ′

where T_lower_thread < 0 means the thread alone is self-locking; T_lower < 0 means self-locking even after the collar adds its positive contribution; the screw overhauls (back-drives) when tan(λ) > μ′

Mechanical efficiency

Thread efficiency η compares the ideal (frictionless) work of raising the load over one revolution — which is simply W × l — to the actual thread-raising work 2π × T_raise_thread. It excludes collar losses because the collar is a separate mechanical component (thrust bearing, plain collar or washer) whose efficiency depends on its own design, not on the thread geometry. Collar losses are tracked separately in the total torque and in the mechanical-advantage panel.

Efficiency rises with increasing lead angle up to a peak near λ_opt ≈ 45° − α/2, then falls again because very steep leads require large normal forces for the same axial load. At the self-locking boundary, η → 0; at the optimal lead angle, η_max ≈ (1 − μ′) / (1 + μ′) for small α. In practice, most power screws operate between 10° and 20° lead angle, putting thread efficiency in the 20%–45% range for typical friction coefficients. The MechanixCalc power screw calculator plots η against λ for five standard friction levels so the designer can see the sensitivity.

Thread mechanical efficiency
η = (W · l) / (2·π · T_raise_thread) × 100 %

where η = thread efficiency [%]; T_raise_thread = thread-only raising torque component (excluding T_collar) [N·mm]; η = 0 at the self-locking boundary (tan λ = μ′) and peaks near λ_opt ≈ 45° − α/2

Thread stress and contact pressure

The screw minor (root) diameter d_r = d − 2h carries the combined compressive and torsional loads. Compressive stress σ_c acts on the cross-sectional area π·d_r²/4; torsional shear stress τ acts on the same section from the raising thread torque. Von Mises theory combines them into a single equivalent stress σ_vm for comparison against the material yield strength. This check is particularly important for long, slender screws where d_r is small relative to the applied load.

Thread contact (bearing) pressure p_c acts on the projected flank area of the engaged threads. For a nut of engagement length L_nut, the number of engaged threads is n_t = L_nut / l, and the bearing pressure is W spread over π·d_m·h per thread. The Shigley limit is 15 MPa for a general nut and 25 MPa for a bronze nut — values exceeded at low n_t or high load indicate a longer nut or coarser thread is needed to avoid galling and accelerated wear.

Von Mises combined stress at screw root
σ_c = W / (π·d_r² / 4) τ = 16·T_raise_thread / (π·d_r³) σ_vm = √(σ_c² + 3·τ²)

where d_r = d − 2h = minor (root) diameter [mm]; σ_c = compressive stress [MPa]; τ = torsional shear stress [MPa]; σ_vm = Von Mises equivalent stress [MPa]

Thread contact (bearing) pressure
p_c = W / (π · d_m · h · n_t) where n_t = round(L_nut / l)

where p_c = contact (bearing) pressure [MPa]; h = thread depth [mm]; n_t = number of engaged threads; L_nut = nut engagement length [mm]; p_c ≤ 15 MPa recommended, ≤ 25 MPa bronze-nut maximum (Shigley §8-2)

Worked example

Find the raising torque, collar torque, self-locking status and thread efficiency for an Acme-thread screw jack (α = 14.5°) lifting W = 10 000 N. Thread: d = 40 mm, lead l = 8 mm, depth h = 4 mm. Collar: d_c = 60 mm. Friction: μ = 0.12, μ_c = 0.10.

Given

  • Axial load W10 000 N
  • Thread typeAcme, α = 14.5°
  • Nominal diameter d40 mm
  • Lead l8 mm
  • Thread depth h4 mm → d_m = 36 mm, d_r = 32 mm, r_m = 18 mm
  • Collar mean diameter d_c60 mm
  • Thread friction μ0.12
  • Collar friction μ_c0.10

Result

  • Modified friction μ′0.124
  • Lead angle λ4.05°
  • Self-lockingYes — tan(λ) < μ′
  • Thread raise torque T_thread35.35 N·m
  • Collar torque T_collar30.00 N·m
  • Total raise torque T_raise65.35 N·m
  • Thread efficiency η36 %
  1. Mean diameter: d_m = d − h = 40 − 4 = 36 mm. Mean radius: r_m = 36 / 2 = 18 mm.
  2. Modified friction: μ′ = μ / cos(α) = 0.12 / cos(14.5°) = 0.12 / 0.96815 = 0.1239.
  3. Lead angle: λ = arctan(l / (π·d_m)) = arctan(8 / (π × 36)) = arctan(0.07074) = 4.05°.
  4. Self-locking check: tan(λ) = 0.0707 < μ′ = 0.1239 → SELF-LOCKING (no brake required).
  5. Thread raise numerator: l + π·μ′·d_m = 8 + π × 0.1239 × 36 = 8 + 14.02 = 22.02.
  6. Thread raise denominator: π·d_m − μ′·l = π × 36 − 0.1239 × 8 = 113.10 − 0.991 = 112.11.
  7. Thread raise torque: T_thread = W·r_m·(22.02 / 112.11) = 10 000 × 18 × 0.19641 = 35 354 N·mm = 35.35 N·m.
  8. Collar torque: T_collar = μ_c · W · (d_c / 2) = 0.10 × 10 000 × 30 = 30 000 N·mm = 30.00 N·m.
  9. Total raise torque: T_raise = 35.35 + 30.00 = 65.35 N·m.
  10. Thread efficiency: η = (W · l) / (2·π · T_thread) × 100 = (10 000 × 8) / (2π × 35 354) × 100 = 80 000 / 222 136 × 100 = 36.0 %.

Illustrative — verify against your actual thread geometry, surface finish, lubrication condition and material pair. The calculator runs the same formulas with your exact inputs, adds the Von Mises stress and contact-pressure checks, and generates a branded PDF engineering report.

Do it on your own numbers

Run the full raise/lower torque, efficiency, self-locking check, Von Mises stress and contact pressure for your lead screw — with a PDF engineering report. Free 30-minute preview, no sign-up.

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Frequently asked questions

What is the difference between the raise torque and the lower torque?

Raising torque must overcome both the thread friction and the gravity load simultaneously, so friction adds to the effort required. Lowering torque has gravity assisting, but the thread friction now opposes the downward travel — if friction is strong enough (tan λ < μ′), the screw is self-locking and a positive input torque is still needed to lower. If friction is weaker than the lead angle demands (tan λ > μ′), the screw overhauls: gravity can drive the screw backwards without any driving torque, and a brake is required.

What friction coefficient should I use?

Typical values for a well-lubricated steel/bronze thread are μ ≈ 0.10–0.12 and collar μ_c ≈ 0.10. Dry steel-on-steel can reach μ = 0.15–0.20, and PTFE-lined nuts drop to μ ≈ 0.05. Collar friction depends on the thrust-bearing type: a rolling-element thrust bearing reduces μ_c to 0.01–0.03, which substantially cuts the total torque and improves efficiency. Always state the assumed friction condition alongside any torque value — a 2× change in μ can shift torque by 30–50 % and flip a self-locking screw into an overhauling one.

When does a screw stop being self-locking?

A power screw is self-locking as long as tan(λ) < μ′ (the modified friction coefficient). Lead angle increases with coarser threads or more thread starts; friction drops with better lubrication. Multi-start threads and ball-screw leads (which are much coarser for the same diameter) routinely exceed the self-locking threshold. If you need a holding screw without a brake, keep a single start, use a relatively fine lead and confirm the inequality for your worst-case (most-lubricated) friction condition.

How does thread form (Acme vs square vs buttress) affect efficiency?

Square threads (α = 0°) give the highest efficiency because there is no radial wedging component — μ′ = μ. Acme and metric trapezoidal threads (α ≈ 14.5–15°) have μ′ ≈ 1.035·μ, a 3–4 % penalty, but their wider root makes them stronger and easier to manufacture with a lead screw tap. Buttress threads (α ≈ 7° on the load flank) fall between the two, combining good strength in one axial direction with moderate efficiency. The efficiency difference between square and Acme is rarely decisive — friction level and lead angle have a far larger effect.

Is the power screw calculator free?

You can run a full calculation during a free 30-minute preview with no sign-up required, and a free 14-day account trial (no credit card) unlocks every calculator on the platform. The branded PDF engineering report and saved / shareable calculations are part of a paid plan.

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