The Compendium of Actuation | Actuator Engineering Reference — Firgelli

The Compendium of Actuation

Version 1.0.0 | Living Engineering Reference

0. Authority & Scope

0.1 Scope of Definition

This compendium defines the physics, classification, design, control, and application of actuators across industrial, robotic, and consumer domains. It serves as a canonical engineering reference for actuation systems, establishing standardized nomenclature, classifications, and physical principles governing the conversion of energy into controlled mechanical motion.

How to Cite This Reference:

APA Style: Firgelli Automations. (2025). The Compendium of Actuation: Taxonomy and Physics. Retrieved from https://www.firgelli.com/pages/actuation IEEE Style: "The Compendium of Actuation: Taxonomy and Physics," Firgelli Automations, 2025. [Online]. Available: https://www.firgelli.com/pages/actuation. Chicago Style: Firgelli Automations. "The Compendium of Actuation: Taxonomy and Physics." 2025. https://www.firgelli.com/pages/actuation.

0.2 Standards Alignment

The definitions, terminology, and classifications within this reference align with, and are informed by, the following international standards and conventions:

  • ISO 8373:2012 — Robotics and robotic devices — Vocabulary
  • IEC 60034-1 — Rating and performance of rotating electrical machines
  • IEC 60529 — Degrees of protection provided by enclosures (IP Code)
  • NEMA MG 1 — Motors and Generators (North American Standards)
  • UL 1004 — Standard for Safety regarding Electric Motors

I. The Core Ontology of Actuation

I.1 The Universal Definition of Actuation

Actuation is the controlled process by which an energy source is converted into mechanical motion in order to perform physical work within a system. It is the fundamental mechanism by which control signals (information) are translated into mechanical displacement, force, or torque (action).

In formal terms, actuation represents a transformation process in which input energy is converted into useful mechanical work, with unavoidable thermal and electrical losses:

A(Ein, Sc) → Wmech + Qloss

  • Ein = Input energy (electrical, hydraulic, pneumatic, thermal, chemical)
  • Sc = Control signal (commanded input or control variable)
  • Wmech = Mechanical work output
  • Qloss = Thermal and system losses

I.2 Formal Actuator Taxonomy

To provide a complete engineering definition, actuators are classified by four distinct vectors: Energy Domain, Motion Profile, Mechanical Transmission, and Control Topology.

1. Classification by Energy Domain

The primary source of potential energy used to drive the system.

  • Electrical: Utilization of electromagnetic fields (Lorentz force) or piezoelectric effects.
  • Fluid Power: Utilization of pressure differentials in liquids (Hydraulic) or gases (Pneumatic).
  • Thermal/Chemical: Utilization of phase changes (Wax Motors) or crystalline deformation (Shape Memory Alloys).

2. Classification by Motion Profile

The geometric path of the output vector.

  • Linear: Displacement along a single axis (Push/Pull).
  • Rotary: Angular displacement around a fixed axis (Torque/Spin).
  • Oscillatory: Repetitive periodic motion (Vibration).
  • Curvilinear: Complex non-linear paths (Soft Robotics).

3. Classification by Mechanical Transmission

The mechanism used to convert the prime mover's energy into the final motion profile.

  • Screw-Driven: Lead Screw, Ball Screw, Planetary Roller Screw.
  • Gear-Driven: Rack & Pinion, Spur Gear, Worm Drive, Harmonic Drive.
  • Direct Drive: Linear Motors (Voice Coil), Direct Drive Rotary (DDR).
  • Belt/Chain: Timing belt drives for high-speed transport.

4. Classification by Control Topology

The method by which the actuator's state is regulated.

  • Open-Loop: Motion is commanded without verification (e.g., standard Stepper Motors, Solenoids).
  • Closed-Loop: Output state is measured via sensors (Encoders, Hall Effect) and corrected in real-time.
  • Impedance Controlled: Force and stiffness are modulated dynamically (Robotics).

II. The Physics of Actuation

The performance of all actuators is governed by fundamental mechanical, electrical, and thermodynamic laws. This section defines the canonical physical relationships that describe how actuators generate force, torque, motion, and power, and how system losses and thermal limits constrain real-world operation.

II.1 Work, Energy, and Mechanical Output

Mechanical work is the scalar quantification of energy transfer, defined as the product of force and displacement. In actuation systems, this represents the useful energy delivered to the load.

Linear Systems

W = F · d

  • W = Mechanical work (joules, J)
  • F = Linear force vector (newtons, N)
  • d = Linear displacement vector (meters, m)

Rotary Systems

W = τ · θ

  • τ = Torque (newton-meters, N·m)
  • θ = Angular displacement (radians)

II.2 Power & Mechanical Advantage

Power is the time-rate of doing work. It establishes the upper limit of actuator performance: for a source of fixed power (e.g., a specific motor wattage), force and velocity share an inverse relationship.

The Power Equations

Plinear = F · v
Protary = τ · ω

Mechanical Advantage: By using transmission elements (gears, screws), speed (ω) can be traded for torque (τ). This is defined by the gear ratio (G) or screw lead (L), allowing a small motor to move massive loads at reduced speeds.

II.3 Force–Torque Conversion (The Screw Equation)

Electromechanical actuators typically convert high-speed, low-torque rotary motor output into low-speed, high-force linear motion via a screw transmission.

F = (2π · τ · η) / L

  • F = Linear output force (N)
  • τ = Input torque (N·m)
  • η = Mechanical efficiency (decimal, 0–1.0)
  • L = Screw Lead (meters per revolution)

Note on Lead vs. Pitch: Pitch is the distance between adjacent threads. Lead is the linear distance traveled in one full revolution. For single-start screws, Lead = Pitch. For multi-start screws, Lead = Pitch × Starts.

II.4 Motor Physics: The Electro-Mechanical Coupling

For DC and Brushless DC (BLDC) motors, performance is dictated by two fundamental motor constants: the Torque Constant (Kt) and the Back-EMF Constant (Ke).

1. The Torque-Current Relationship

Torque is directly proportional to the current flowing through the motor windings. This is the most critical relationship for actuator control: Current = Force.

τ = Kt · I

2. The Torque-Speed Curve

As a motor spins, it generates a Back-EMF voltage that opposes the supply voltage, reducing the current and thus the torque. This creates a linear torque-speed curve spanning from Stall Torque (zero speed, max current) to No-Load Speed (max speed, zero torque).

ω = (V - I·R) / Ke

II.5 Efficiency, Losses, and Thermodynamics

No actuator is 100% efficient. Energy not converted into mechanical work is dissipated as heat, governed by two primary loss mechanisms.

1. Copper Loss (I2R)

Resistive heating in the motor windings is the dominant source of heat in high-force applications. It scales with the square of the current.

Pheat = I2 · R

2. Core Losses (Iron Loss)

Heat generated by Hysteresis (constant magnetization reversal) and Eddy Currents in the motor's iron core. These losses increase with motor speed (frequency), whereas copper losses increase with load (torque).

II.6 Thermal Limits and Duty Cycle

Duty Cycle is the temporal constraint ensuring the actuator's average power dissipation does not exceed its Thermal Resistance (Rth) limit.

Duty Cycle (%) = [On Time / (On Time + Off Time)] × 100

Why Duty Cycle Matters: If Pheat exceeds the rate at which the housing can shed heat to the environment (1/Rth), the internal temperature will rise until the insulation melts. High-performance actuators use cooling fins or oil filling to lower thermal resistance and increase duty cycle.

II.7 Power & Force Density

A critical metric for engineering selection is the actuator's output relative to its physical mass.

  • Force Density (N/kg): Hydraulic actuators dominate here due to high operating pressures (3000+ psi). Electric actuators are limited by magnetic saturation of iron.
  • Power Density (W/kg): Pneumatic actuators excel in power density due to high speeds, but lack the force density of hydraulics or the precision of electrics.

III. Technology Profiles: The Canonical Monographs

This section provides formal, technology-specific monographs for the principal classes of actuators. Each profile defines the complete energy conversion chain, governing physics, performance characteristics, dominant failure mechanisms, and practical engineering implications.

III.1 Electric Linear Actuators

Technical cutaway of an Electric Linear Actuator

Definition: An electromechanical device that converts rotational energy from an electric motor into linear displacement via a mechanical transmission system.

1. The Energy Conversion Chain

Electric actuation represents a multi-stage transduction process. Efficiency losses occur at every stage of this chain:

Electrical Energy (V·I) → Magnetic Flux (Φ) → Rotary Torque (τ) → Linear Force (F)

  • Electrical Stage: Current flows through stator windings (copper loss).
  • Magnetic Stage: Lorentz force generates torque on the rotor (iron loss).
  • Mechanical Stage: Gears reduce speed/increase torque (friction loss).
  • Transmission Stage: Screw mechanism converts rotation to translation (contact friction).

2. Screw Mechanics & Force Generation

The core of the linear actuator is the screw transmission. The output force is a function of input torque and the geometric mechanical advantage of the screw threads.

F = (2π · τ · η) / L

  • F = Linear output force (N)
  • τ = Applied motor torque (N·m)
  • η = Screw efficiency (Acme: 20-40%, Ball Screw: 85-95%)
  • L = Screw lead (linear travel per revolution, meters)

3. Self-Locking vs. Backdrivable Regimes

The ability of an actuator to hold a static load without power depends on the friction angle relative to the lead angle.

  • Self-Locking (Static Holding): Common in Acme/Lead screws. Occurs when the tangent of the lead angle is less than the coefficient of friction (tan(λ) < μ). The actuator resists back-driving forces naturally.
  • Backdrivable (Dynamic Efficiency): Common in Ball and Roller screws. Due to low rolling friction, external loads can force the screw to rotate backwards. Requires an electromechanical brake for holding loads.

4. Dominant Failure Mechanisms

  • Nut Wear: In sliding-contact screws (Acme), the nut material (bronze/polymer) is the sacrificial element. Wear rate is proportional to P · V (Pressure × Velocity).
  • Bearing Fatigue (L10 Life): In rolling-contact screws (Ball/Roller), failure is defined by subsurface fatigue spalling. Lifespan is statistically calculated as L10 life (millions of revolutions).
  • Motor Commutation: In brushed motors, brush/commutator interface erosion limits total service hours.

III.2 Hydraulic Actuators

[Image of hydraulic actuator] Cross-section diagram of a hydraulic cylinder illustrating Pascal's Law

Definition: A fluid power device utilizing the incompressibility of liquids (typically oil) to generate high force density via pressure differentials.

1. Pascal’s Law & Force Generation

Hydraulics operate on Pascal’s Principle: pressure applied to a confined fluid is transmitted undiminished in all directions.

F = P · A

Because hydraulic fluid has a high Bulk Modulus (β) (resistance to compression), hydraulic actuators are mechanically "stiff," allowing for precise control of high-inertia loads without the "springiness" of pneumatics.

2. Force Density Dominance

Hydraulics offer the highest force-to-weight ratio of any standard actuator class. While electric motors are limited by magnetic saturation (~1.5 Tesla), hydraulic systems are limited only by the burst pressure of the cylinder (often >3000 PSI / 20 MPa).

3. Failure Modes: Leakage & Cavitation

  • Seal Wear & Leakage: Internal bypass leakage reduces volumetric efficiency (ηvol), causing drift. External leakage poses environmental hazards.
  • Cavitation: If local pressure drops below the fluid's vapor pressure, bubbles form and collapse violently. This causes pitting erosion on metal surfaces and distinct "gravel" noise.

III.3 Pneumatic Actuators

[Image of pneumatic actuator] Cross-section diagram of a pneumatic actuator

Definition: A fluid power device utilizing the compressibility of gases (typically air) to generate high-speed motion.

1. Compressibility & The Gas Laws

Unlike hydraulics, the working medium in pneumatics is compressible. This behavior is governed by the Ideal Gas Law (PV = nRT). This compressibility introduces Mechanical Compliance (elasticity) into the system.

2. The "Air Spring" Effect

Pneumatic actuators behave as non-linear springs.

  • Pros: Excellent shock absorption and compliance; safe for "bang-bang" (end-to-end) actuation.
  • Cons (Positioning): Extremely difficult to achieve precise intermediate positioning. Changes in load cause changes in gas compression, leading to "spongy" position control compared to the hydraulic "liquid steel" effect.

III.4 Piezoelectric Actuators

Piezoelectric crystal lattice deformation

Definition: Solid-state ceramic devices that utilize the inverse piezoelectric effect to convert electrical potential directly into atomic lattice deformation.

1. Crystal Lattice Physics

When an electric field (E) is applied across a piezo-ceramic material (like PZT), the asymmetry in the unit cell structure causes mechanical strain (S).

S = d33 · E

  • S = Strain (dimensionless change in length)
  • d33 = Piezoelectric charge constant (m/V)
  • E = Electric field strength (V/m)

2. Nanometer Precision vs. Hysteresis

Piezo actuators offer sub-nanometer resolution (infinite theoretical resolution, limited only by electronic noise). However, they suffer from Hysteresis (position depends on previous history) and Creep (drift over time under constant voltage), requiring closed-loop feedback for absolute accuracy.

III.5 Soft Actuators & Artificial Muscles

Definition: Compliant materials that deform under stimuli, mimicking biological muscle mechanics for robotics and prosthetics.

1. Shape Memory Alloys (SMA)

Alloys (e.g., Nitinol) that undergo a solid-state phase transformation (Martensite ↔ Austenite) when heated electrically.

  • Energy Density: Extremely high work-per-volume.
  • Bandwidth: Limited by the thermal cooling rate (slow relaxation).

2. Pneumatic Artificial Muscles (PAMs)

Flexible bladders encased in a braided mesh (McKibben muscles). When pressurized, the bladder expands radially and contracts axially. These provide high force and inherent safety for human-robot interaction due to their soft structure.

IV. Control & Intelligence: The Nervous System

An actuator without control is merely a force generator. Intelligence is defined by the system's ability to regulate that force in space and time. This section defines the canonical control architectures, feedback metrology, and fault-tolerance protocols that govern precision actuation.

IV.1 Control Architectures

1. Open-Loop vs. Closed-Loop Topology

The fundamental distinction in control theory is the presence of an error-correction mechanism.

  • Open-Loop (Blind): The controller issues a command (e.g., "Step 500 times") and assumes the actuator complies. Common in Stepper Motors. Failure Mode: If the motor stalls or misses a step, the controller has no knowledge of the positional error.
  • Closed-Loop (Servo): The controller compares the Commanded State (r) against the Measured State (y) to calculate an Error Signal (e = r - y). The controller drives the actuator to minimize e to zero.

2. PID Control Fundamentals

The Proportional-Integral-Derivative (PID) algorithm is the mathematical standard for linear servo control. It continuously calculates an error value and applies a correction based on three terms:

u(t) = Kpe(t) + Ki∫e(t)dt + Kd(de/dt)

  • P (Present): Proportional gain (Kp). Reacts to the current error. High Kp improves speed but causes oscillation.
  • I (Past): Integral gain (Ki). Sums past errors to eliminate steady-state offset (e.g., friction holding the actuator back).
  • D (Future): Derivative gain (Kd). Predicts future error based on rate of change, adding damping to prevent overshoot.

3. Feedforward vs. Feedback

While Feedback is reactive (correcting errors after they happen), Feedforward is predictive. In high-performance actuation, a feedforward model predicts the force required to accelerate the mass (F=ma) and injects that current immediately, reducing the lag inherent in pure feedback systems.

IV.2 Sensors & Metrology

Precision is limited by the system's ability to measure itself. The resolution of a linear actuator is a function of its sensor density and mechanical transmission.

1. The Linear Resolution Equation

For a screw-driven actuator with a rotary encoder, the smallest detectable linear increment (Δx) is derived from the screw lead, the gear reduction ratio, and the sensor pulses.

Resolution = Screw Lead / (Gear Ratio × Encoder CPR)

  • Screw Lead (L): Linear travel per revolution (mm).
  • Gear Ratio (G): The reduction factor (e.g., 20:1 reduction = 20).
  • Encoder CPR: Counts Per Revolution of the motor shaft.

Engineering Insight: Placing the encoder on the motor (before the gearbox) increases effective resolution by a factor of G, but introduces backlash error into the measurement. Placing it on the output shaft measures true position but requires higher sensor precision.

2. Quantization Error

Digital sensors divide continuous reality into discrete steps. An actuator cannot position itself more accurately than ± 0.5 counts. This Quantization Error manifests as high-frequency noise in the Derivative (D) term of a control loop.

3. Absolute vs. Incremental Positioning

  • Incremental (Relative): Counts pulses from an arbitrary starting point. Requires a "Homing Sequence" (driving to a physical limit switch) upon power-up to establish zero.
  • Absolute: Uses a unique binary code (Gray Code) or potentiometer voltage for every position. Retains position data even after total power loss. Essential for safety-critical applications.

IV.3 Safety & Fault Tolerance Protocols

Robust actuation systems must account for mechanical and electrical failure modes.

1. End-of-Stroke Limits (Hard vs. Soft)

  • Hard Limits: Physical micro-switches that mechanically break the circuit to the motor when travel limits are reached. This is the ultimate fail-safe.
  • Soft Limits: Virtual limits programmed into the controller firmware based on encoder counts. These prevent the actuator from ever hitting the physical hard stops, reducing mechanical wear.

2. Overcurrent (Stall) Protection

If an actuator jams, Back-EMF drops to zero and current spikes to V/R (Stall Current). This rapid heating will destroy the motor.

  • Trip Point: Controllers must be set to cut power if current exceeds nominal limits for a specific duration (e.g., >150% load for >500ms).

3. Redundancy

In critical avionics or medical systems, actuators employ Dual-Channel Architecture: two motors driving a single shaft, or two potentiometers comparing position data. If the two channels disagree, the system enters a Safe Mode.

V. Application Engineering: Failure Physics & Implementation

An actuator is only as reliable as its integration. While laboratory specs define theoretical performance, application engineering determines real-world survival. This section defines the geometric, structural, and environmental constraints that govern system longevity.

V.1 Mounting Geometry & Force Vectors

1. Vector Force Decomposition

Actuators are designed to push/pull axially. When mounted at an angle (θ) relative to the direction of motion, the useful force vector (Fuseful) is reduced by the cosine of that deviation angle.

Fuseful = Faxial · cos(θ)

Engineering Reality: In hinged applications (e.g., a hatch lift), the Triangle of Death occurs when the actuator is nearly parallel to the hinge (high θ). As θ approaches 90° (perpendicular), mechanical advantage is zero (cos(90) = 0). Systems should be designed to minimize θ at the point of highest load.

2. Euler Buckling (The Push Limit)

In compression (pushing), the actuator rod acts as a slender column. It will fail via **Buckling** long before it yields via compression. The Critical Buckling Load (Pcr) is calculated via the Euler Column Formula:

Pcr = (π2 · E · I) / (K · L)2

  • E: Young's Modulus (Steel ≈ 200 GPa)
  • I: Area Moment of Inertia (function of rod diameter)
  • L: Unsupported Length (Stroke)
  • K: Column Effective Length Factor (Crucial for mounting selection):
Mounting Condition K Value Buckling Risk
Pinned-Pinned (Clevis) 1.0 Standard Baseline (Idealized)
Fixed-Free (Cantilever) 2.0 Highest Risk (4x reduction in load)
Fixed-Fixed (Rigid) 0.5 Lowest Risk (4x increase in load)

V.2 Structural Interfaces

1. Side-Loading: The Primary Failure Mode

Linear actuators are strictly axial devices. Any force applied perpendicular to the travel axis is a Side Load (Radial Load).

  • Effect: Side loads create a bending moment on the lead screw and rod. This deforms the rod seal (allowing water ingress) and increases internal friction, robbing the system of force.
  • Solution: Use **Linear Slide Rails** to carry the radial load, isolating the actuator to handle only axial push/pull forces.

2. Mounting Topologies

  • Clevis Mounts (Spherical Rod Ends): Allow for angular misalignment in two planes. Essential for systems where the geometry changes throughout the stroke (e.g., solar trackers).
  • Trunnion Mounts: Mounts on the body of the actuator. Reduces the unsupported length (L) in buckling calculations, allowing for higher push forces.

V.3 Environmental Engineering

1. The Reality of IP Ratings

Ingress Protection (IP) ratings are static lab tests. Dynamic operation changes the physics of ingress.

  • The "Breathing" Effect: As an actuator extends, internal volume increases, drawing air in. As it retracts, air is expelled. If the seal is wet during extension, moisture is vacuumed inside the housing.
  • IP66 vs IP69K: IP66 protects against high-pressure jets. IP69K protects against high-pressure, high-temperature steam cleaning, essential for food & beverage compliance.

2. Temperature Derating

Actuator performance curves are typically rated at 25°C.

  • Low Temp (< 0°C): Lubricant viscosity increases, increasing the "No-Load Current" draw and reducing available force.
  • High Temp (> 50°C): Copper resistance increases (0.39% per °C), increasing I2R losses. The Duty Cycle must be linearly derated to prevent thermal runaway.

VI. Reliability, Lifespan & Failure Physics

Actuator lifespan is not random; it is a deterministic function of mechanical wear, thermal stress, and fatigue cycles. This section defines the canonical physics governing service life (L10) and the dominant failure modes in electromechanical systems.

VI.1 Wear Mechanisms

1. Screw & Nut Wear (The PV Limit)

For sliding-contact lead screws (Acme), life is limited by the wear of the softer nut material (bronze or polymer) against the harder steel screw. The wear rate is governed by the Pressure-Velocity (PV) value.

PV = Pressure (Load/Area) × Surface Velocity

Exceeding the material's critical PV rating causes rapid thermal deformation and catastrophic wear, even if the load is within the static rating.

2. Bearing Fatigue (L10 Life)

For rolling elements (Ball Screws & Bearings), failure is defined by subsurface fatigue spalling. The industry standard metric is L10 life: the number of revolutions at which 90% of a population will survive.

L10 = (C / P)p × 106 Revs

  • C: Dynamic Load Rating (from manufacturer).
  • P: Applied Equivalent Load.
  • p: Life Exponent (3 for Ball Bearings, 10/3 for Roller Bearings).

3. Brushed Motor Wear

In DC motors, the carbon brushes physically slide against the commutator. Life is limited by Electrical Erosion caused by arcing during commutation. High current density increases arcing, exponentially reducing brush life.

VI.2 Life Estimation Physics

1. The Load-Life Inverse Power Law

Reducing load dramatically extends life. For ball screws, halving the load increases life by a factor of 8 (23).

Lifenew = Liferated × (Loadrated / Loadactual)3

2. Thermal Aging (Arrhenius Equation)

Heat kills electronics and insulation. The Arrhenius Law states that for every 10°C rise in operating temperature, the chemical degradation rate doubles (halving the component life).

Reaction Rate (k) = A · e(-Ea / RT)

Practical Rule: Running a motor at 80°C instead of 60°C reduces its insulation life by approximately 75%.

VI.3 Dominant Failure Modes

1. Back-Driving & Regenerative Voltage

When a load forces an actuator to retract (gravity drop), the motor turns into a generator. This generates Back-EMF that can exceed the supply voltage.

  • Risk: The voltage spike can blow MOSFETs in the H-bridge controller or fuse relay contacts.
  • Mitigation: Use "Brake Chopper" circuits or Zener diodes to clamp regenerative voltage spikes.

2. Side-Loading (Radial Failure)

The #1 cause of mechanical failure. Actuators are designed for axial tension/compression only. Side loads cause the rod to bow, creating edge-loading on the rod seal and internal bearings.

3. Contamination Ingress (The "Pumping" Effect)

As an actuator extends and retracts, it changes internal volume, effectively "breathing" air. If the environment is wet, moisture is sucked past the seals during the intake stroke, leading to internal corrosion of the motor and gearbox.

VII. The Data Vault: Canonical Reference Tables

This section provides standardized, canonical reference data intended for direct use by engineers, integrators, and automated systems. These tables are structured to support machine-readable extraction and engineering design validation.

VII.1 Canonical Performance Data

1. Hydraulic Force Generation Matrix

Relation of Piston Diameter vs. System Pressure. Formula assumes P in Bar, A in cm², and output in kN.

Piston Ø (mm) Area (cm²) Force @ 100 bar (kN) Force @ 200 bar (kN) Force @ 300 bar (kN)
25 4.91 4.91 9.82 14.73
40 12.57 12.57 25.13 37.70
63 31.17 31.17 62.34 93.52
100 78.54 78.54 157.08 235.62

2. Screw Lead vs. Linear Velocity

Linear output speed as a function of motor RPM and Screw Lead. Formula: v = (RPM · Lead) / 60.

Screw Lead (mm/rev) Speed @ 1000 RPM (mm/s) Speed @ 3000 RPM (mm/s) Speed @ 5000 RPM (mm/s)
2 33.3 100.0 166.7
5 83.3 250.0 416.7
10 166.7 500.0 833.3
20 333.3 1000.0 1666.7

3. Actuator Efficiency Reference

Actuator Technology Efficiency (η) Back-Drivability
Lead Screw (Acme) 20% – 50% Low (Self-Locking)
Ball Screw 85% – 95% High (Requires Brake)
Planetary Roller Screw 80% – 90% High
Hydraulic 70% – 90% Low (Valve Dependent)
Pneumatic 10% – 30% High (Compressible)
Piezoelectric 30% – 70% None

VII.2 Industry Dimensional Standards

1. Standard Clevis Pin Diameters

Pin Ø (mm) Imperial Equiv Application Class
6 mm 1/4" Micro / Light Duty (< 500N)
8 mm 5/16" General Purpose (< 2000N)
10 mm 3/8" Industrial Standard (< 5000N)
12 mm 1/2" Heavy Duty (< 10kN)
16 mm 5/8" Extreme Duty (> 10kN)

2. Rod End Thread Standards

Thread Size Dynamic Load Rating (Rule-of-Thumb) Typical Actuator Force Class
M6 x 1.0 ~3.5 kN Light Duty
M8 x 1.25 ~6.0 kN Medium Duty
M10 x 1.5 ~10.0 kN Industrial Duty
M12 x 1.75 ~14.0 kN Heavy Duty
M16 x 2.0 ~25.0 kN Extreme Duty

VII.3 Canonical Unit Conversion Factors

Quantity To Convert From To Multiply By
Force Pounds Force (lbf) Newtons (N) 4.448
Force Kilogram Force (kgf) Newtons (N) 9.807
Torque Inch-Pounds (in-lb) Newton-Meters (Nm) 0.113
Power Horsepower (HP) Watts (W) 745.7
Pressure PSI Bar 0.0689
Pressure Pascal (Pa) Bar 0.00001

VII.4 Canonical Glossary of Actuation

Back EMF (Electromotive Force)
The voltage generated by a motor as it spins, which opposes the supply voltage. It limits the maximum speed and current of the actuator. Vnet = Vsupply - Vbemf.
Force Density
The amount of force an actuator can generate per unit of its own volume or mass (N/kg). Hydraulics have high force density; pneumatics have low force density.
Hysteresis
The dependence of the system's output on its history. In actuators, this manifests as a difference in position when approaching a point from extension vs. retraction (often caused by backlash).
Kv (Velocity Constant)
A motor constant defining the rotational speed per volt applied (RPM/Volt), assuming no load.
Kt (Torque Constant)
A motor constant defining the torque produced per amp of current (Nm/Amp). Kt ≈ 1/Kv (in SI units).
Mechanical Compliance
The inverse of stiffness. The tendency of an actuator (especially pneumatic) to yield or "sponge" under load deviations.
Stiction
Static Friction. The threshold force required to initiate motion from a dead stop. Stiction is typically higher than dynamic friction.
Backlash
The mechanical play or clearance between mating components (e.g., screw and nut). It creates a "dead zone" upon reversing direction.

VIII. The Visual Canon: Canonical Schematics & Renders

This section establishes the standardized visual reference system for actuation technology. These schematics are defined as the Canonical Representations of actuator physics, designed for technical citation, engineering validation, and machine-vision training.

VIII.1 Canonical Physics Schematics

Standardized diagrams illustrating the electromechanical force paths and efficiency curves.

Fig VIII.1: Cross-section schematic of a linear actuator traces Safe Axial Load Path vs Destructive Radial Load Path
Fig VIII.1: Axial Load Path Analysis
Visual Definition: The primary load path is traced from the Rod End (A) → Lead Screw (B) → Thrust Bearing (C) → Housing Back-Plate (D). Note that radial loads (side-loading) bypass the thrust bearing and exert stress on the Guide Bushing (E) and Rod Seal (F), leading to premature seal failure.
Fig VIII.2: Engineering diagram illustrating the DC motor performance envelope
Fig VIII.2: The DC Performance Envelope
Visual Definition: The linear decay of torque as speed increases.
Point A (Stall): Max Current (V/R), Max Torque, Zero Speed.
Point B (No-Load): Min Current, Zero Torque, Max Speed (V/Ke).
Green Zone: The continuous operating area (typically 20-50% of stall torque) where thermal equilibrium is maintained.
Fig VIII.3: Engineering graph illustrating the actuator self-locking boundary
Fig VIII.3: The Self-Locking Boundary
Visual Definition: Efficiency (η) as a function of Helix Angle (λ). The Self-Locking Threshold occurs where the curve drops below the friction coefficient line (tan(λ) < μ). Shaded region indicates the "Back-Driving Danger Zone" where external loads can reverse the mechanism.
Force Vector Diagram: Linear actuator pushing a hinged load
Fig VIII.4: Geometric Force Decomposition
Visual Definition: Illustrating the cosine loss in hinged applications.
Vector F_axial: The force generated by the actuator.
Vector F_useful: The effective vertical component (F_axial · cos(θ)).
As θ approaches 90° (deviation from lift vector), F_useful → 0, forcing the actuator to stall despite operating at full power.

VIII.2 Reference Component Hierarchy

High-fidelity exploded views defining the canonical architecture of electromechanical actuators.

Exploded View of Actuator Assembly
Fig VIII.5: The Assembly Stack
1. Stator/Rotor: Prime mover.
2. Planetary Gearbox: Torque multiplication (10:1 to 100:1).
3. Lead Screw: Rotary-to-Linear interface.
4. Drive Nut: The sacrificial wear component (Bronze/Polymer).
5. Extension Tube: Structural interface.
Planetary Gearbox Detail
Fig VIII.6: Planetary Reduction Stage
Details the Sun Gear (Input), Planet Carrier (Output), and Ring Gear (Fixed). Shows the load distribution across multiple teeth, explaining why planetary systems offer higher torque density than spur gears.

VIII.3 Standardized Engineering Nomenclature

To ensure interoperability with automated systems and engineering documentation, the following standardized labeling conventions are established for this compendium.

Component Standard Label Code Definition
Motor Winding MOT-W Copper stator coils subject to I2R heating.
Commutator COM-X Rotary electrical switch in brushed motors.
Thrust Bearing BRG-T Axial load support element (Ball or Tapered Roller).
Lead Screw SCR-L Trapezoidal thread profile (ACME).
Wiper Seal SEAL-W Elastomeric barrier preventing particulate ingress.

IX. The Machine-Readable Layer: Semantic Architecture

To function as a true 21st-century reference, this Compendium is structured for dual consumption: Human-Readable (text/visuals) and Machine-Readable (structured data). This section defines the Ontology, Schema, and Equation Registry that allow Artificial Intelligence and Knowledge Engines to parse this document as an authoritative reference.

IX.1 Canonical Entity Definitions (JSON-LD)

Core concepts are defined using the Schema.org vocabulary, extended with engineering-specific properties. Below is a representation of the canonical definition structure used within the site's knowledge graph.

{
  "@context": "https://schema.org",
  "@type": "TechArticle",
  "mainEntity": {
    "@type": "DefinedTerm",
    "termCode": "ACT-001",
    "name": "Linear Actuator",
    "description": "A mechanical device that converts energy (electrical, hydraulic, pneumatic) into linear motion.",
    "inDefinedTermSet": "https://www.firgelli.com/pages/actuation",
    "sameAs": [
      "https://en.wikipedia.org/wiki/Linear_actuator",
      "http://www.wikidata.org/entity/Q1128563"
    ]
  }
}

Fig IX.1: Sample JSON-LD node establishing semantic identity for AI parsers.

IX.2 The Canonical Equation Registry

Mathematical relationships are assigned immutable **Equation IDs**. This allows external engineering tools to reference specific physics models without ambiguity.

ID Name Canonical Form Domain
EQ-MECH-001 Linear Work W = F · d General Physics
EQ-MECH-002 Screw Force F = (2π · τ · η) / L Transmission
EQ-ELEC-001 Motor Torque τ = Kt · I Electromagnetic
EQ-THERM-001 Duty Cycle DC% = [On / (On + Off)] · 100 Thermodynamics
EQ-LIFE-001 L10 Bearing Life L10 = (C / P)3 · 106 Tribology

IX.3 Stable Semantic Anchors

To support long-term citation, the following stable URL anchors are established. These anchors are intended to remain stable across future version updates of the Compendium.

  • Definition of Force: #def-force
  • Definition of Backlash: #def-backlash
  • The Triangle of Death: #app-geometry-mounting
  • Ingress Protection Table: #ref-ip-ratings

IX.4 Document Versioning

Current Version: 1.0.0 (Canonical Release)
Last Updated: January 2025
Maintainer: Firgelli Automations Engineering Group
This document is a living standard. Revisions are tracked via semantic versioning (Major.Minor.Patch) to ensure citation integrity.


About the Author

Robbie Dickson is the Chief Engineer and Founder of Firgelli Automations. With a background in aeronautical and mechanical engineering (Rolls-Royce, BMW, Ford), he has spent over two decades pioneering precision motion control systems, from linear actuators for robotics to active aerodynamic braking systems for supercars.