Current
Electrical current is the flow of electric charge through a conductor, measured in amperes (A). It is a fundamental concept in electricity and electronics, cruc...
The ampere (A) measures electric current—the amount of charge flowing per second. It is the SI base unit essential for electrical system design, safety, and compliance, especially in aviation and engineering.
The ampere (symbol: A) is the fundamental SI unit for measuring electric current. It quantifies the rate at which electric charge flows through a conductor:
1 ampere = 1 coulomb of charge passing a point per second.
The name honors André-Marie Ampère (1775–1836), a French physicist and mathematician who founded the science of classical electromagnetism (electrodynamics).
Since 2019, the ampere is defined by fixing the value of the elementary charge (e) at exactly 1.602176634 × 10⁻¹⁹ coulombs.
Thus, 1 ampere is the electric current corresponding to the flow of 1/(1.602176634 × 10⁻¹⁹) elementary charges per second.
Source: BIPM SI base unit ampere
Key Point:
Before 2019, the ampere was defined by the force between two parallel conductors:
The ampere is that constant current which, if maintained in two straight parallel conductors of infinite length, 1 meter apart in vacuum, would produce a force equal to 2 × 10⁻⁷ newtons per meter of length.
This definition highlights the link between electricity and magnetism, as described by Ampère’s Law.
In aviation, amperes are crucial for specifying battery capacity, alternator/generator output, circuit breaker settings, and wire sizing.
Current (I) = Charge (Q) / Time (t)
Example: A current of 5 A means 5 coulombs of charge flow each second.
| Quantity | Symbol | SI Unit | Formula / Example | What It Measures |
|---|---|---|---|---|
| Current | I | A | I = Q / t | Charge flow per second |
| Voltage | V | V | V = I × R | Electric potential difference |
| Resistance | R | Ω | R = V / I | Opposition to current |
| Power | P | W | P = V × I | Rate of energy transfer |
| Charge | Q | C | Q = I × t | Total charge transferred |
| Capacity | Ah | Ah | Ah = I × time (h) | Battery charge over time |
Aircraft electrical systems are rated in amperes for:
ICAO Annex 6, Part I:
Requires electrical load analysis in amperes, proper circuit protection, and minimum battery endurance in Ah (ICAO Annex 6
).
| Device/Scenario | Typical Current (A) | Aviation Relevance |
|---|---|---|
| Navigation light | 1–3 | Circuit/wire sizing, CB selection |
| Cockpit panel | 0.5–2 | Bus load calc, redundancy |
| Avionics system | 5–20 | Load shedding, backup, isolation |
| Starter motor | 100–800 | Surge rating, relay/cable selection |
| Cabin lighting | 10–30 | Emergency power, load estimation |
| Pitot heater | 5–15 | De-icing, monitoring |
| Ground power unit | up to 1,000 | Supply limits, external power |
All protection devices (fuses, breakers) are rated in amperes per ICAO/FAA.
Best Practice:
Always use calibrated, approved instruments per aviation maintenance standards.
Example 1:
A 140 W landing light on a 28 V bus:
I = P / V = 140 / 28 = 5 A
Example 2:
Emergency bus must supply 20 A for 15 minutes:
t = 15 min = 900 s
Q = I × t = 20 × 900 = 18,000 C
Example 3:
Pitot heater, R = 7 Ω, V = 28 V:
I = V / R = 28 / 7 = 4 A
| Wire Gauge (AWG) | Max Current (A) | Typical Use |
|---|---|---|
| 22 | 5 | Avionics, signals |
| 18 | 10 | Small lights, switches |
| 14 | 20 | Cabin lighting, loads |
| 10 | 30 | Main bus, relays |
| 6 | 55 | Power, batteries |
Always use official charts for your installation.
| Electrical Concept | Water Analogy |
|---|---|
| Voltage | Water pressure |
| Current (A) | Flow rate (L/sec) |
| Resistance (Ω) | Pipe restriction |
Just as water flows faster with higher pressure or wider pipes, more electric current (amperes) flows with higher voltage or lower resistance.
| From | To | Multiply By |
|---|---|---|
| Amperes (A) | Milliamperes | 1,000 |
| Milliamperes | Amperes | 0.001 |
| Amperes (A) | Coulombs/sec | 1 |
| Amperes (A) | Electrons/sec | 6.241×10¹⁸ |
The ampere is the SI base unit for electric current—central to all electrical calculations, system design, and safety. In aviation, every wire, breaker, and battery is specified by amperes to ensure reliability and compliance. Understanding amperes is essential for everyone involved in electrical systems, especially in regulated fields like aviation.
Since 2019, the ampere is defined by fixing the elementary charge (e) at 1.602176634 × 10⁻¹⁹ coulombs, so 1 ampere is the current that transports 1 coulomb per second. This links the unit directly to a fundamental constant of nature.
Amperes specify the maximum safe current for wires, circuit breakers, and loads. ICAO and FAA standards require all aircraft circuits to be rated and protected in amperes to prevent overheating, fire, and ensure safety-critical systems remain operational.
1 ampere (A) = 1,000 milliamperes (mA). 1 coulomb (C) = 1 ampere × 1 second. 1 ampere-hour (Ah) = 3,600 coulombs. For AC systems, use RMS values for accurate current measurements.
Amperes measure current (rate of charge flow), while ampere-hours measure total charge delivered over time (battery capacity). For example, a 10 Ah battery can supply 10 A for 1 hour, or 1 A for 10 hours.
Current is measured using ammeters (inserted in series), clamp meters (detecting magnetic fields), or multimeters. In aviation, only calibrated, approved instruments may be used for maintenance and system checks.
Understand ampere ratings to ensure safe, compliant, and efficient system design—essential for aviation, engineering, and electrical maintenance.
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