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:
- Pitot capsule expands as total pressure increases → pushes the pointer toward higher Mach.
- Static capsule also expands as altitude increases (pressure decreases) → adjusts the pitot effect.
- 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.