ATPL Theory

Machmeter

Everything about the Machmeter, including:

  • what it is,
  • how Mach is measured and calculated,
  • how a mechanical Machmeter works, and
  • how its linkage system operates — all in one clear explanation 👇

✈️ Machmeter — Principle, Measurement, and Mechanism


🧭 1️⃣ What Mach Means

The Mach number (M) is the ratio of the aircraft’s True Airspeed (TAS) to the local speed of sound:

$$ M = \frac{\text{TAS}}{\text{a}} $$

Where:

  • TAS = True Airspeed
  • a = speed of sound (depends on air temperature)

At sea level, the speed of sound ≈ 340 m/s (661 kt), but it decreases with altitude because air temperature drops.


⚙️ 2️⃣ How Mach Is Measured in Aircraft

Modern aircraft calculate Mach using pressures from the pitot-static system:

  • Total (pitot) pressure ( p_t )
  • Static pressure ( p_s )

The Machmeter (or Air Data Computer) determines Mach from their ratio:

$$ M = \sqrt{\frac{5}{2}\left[\left(\frac{p_t}{p_s}\right)^{2/7} - 1\right]} $$

This formula comes from compressible airflow laws (using γ = 1.4 for air).

✅ So — the Mach number depends only on total pressure and static pressure.


📟 3️⃣ What a Machmeter Does

The Machmeter shows the aircraft’s Mach number, not its airspeed. It’s crucial at high altitudes because the speed of sound changes with temperature — so IAS or TAS alone don’t show how close the aircraft is to its Mach limits (MMO).


⚙️ 4️⃣ Mechanical Machmeter — How It Works

Before digital systems, the Mach number was indicated mechanically using only pitot and static pressures.

🔹 Main Components

Component Measures Effect
Pitot capsule Total pressure ((p_t)) Expands with airspeed
Static capsule (aneroid) Static pressure ((p_s)) Expands with altitude (compensates for air density)
Linkage system Combines both capsule movements Moves the Mach pointer on the dial

The instrument compares total and static pressures to display Mach number directly.


🧩 5️⃣ Principle of the Linkage

Inside the Machmeter, a mechanical linkage (levers, gears, and a cam) combines the two pressure effects.

🔸 Step-by-step:

  1. Pitot capsule expands as total pressure increases → pushes the pointer toward higher Mach.
  2. Static capsule also expands as altitude increases (pressure decreases) → adjusts the pitot effect.
  3. The linkage blends these two movements so that the pointer shows the correct Mach ratio for any altitude.

👉 The linkage is shaped so that the movement matches the non-linear relationship between pressure ratio and Mach number.

🪀 Conceptual Diagram

Pitot (total pressure) capsule  → expands with speed
        │
        ▼
   Lever/Cam system ←── Static (altitude) capsule
        │
        ▼
    Mach pointer (dial)
  • More pitot pressure → higher Mach
  • Less static pressure (higher altitude) → higher Mach for the same speed

🧠 6️⃣ Why It’s Important

  • At high altitude, IAS decreases but Mach increases for the same TAS.
  • Aircraft must stay below a maximum Mach limit (MMO) to avoid compressibility effects and shock waves.
  • The Machmeter gives an accurate, altitude-compensated indication of this limit.

✅ 7️⃣ Summary

Feature Description
Purpose Show speed relative to the speed of sound
Measured by Comparing pitot and static pressures
Inputs Total (pitot) pressure, Static pressure
Main parts Pitot capsule, Static aneroid capsule, Mechanical linkage
Output Pointer showing Mach number (e.g. 0.78)
Compensation Automatically adjusts for altitude and air density
Modern version Air Data Computer calculates Mach digitally

✈️ In short:

The Machmeter measures how fast the aircraft is flying relative to the speed of sound. In a mechanical Machmeter, pitot and static pressures move two capsules connected by a linkage system that combines their effects — showing Mach number directly, automatically compensating for altitude and temperature.