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| MIL-E-7016F
Note:
Approval of the analysis cannot be construed to mean
approval of any specific electric component or circuitry.
5.
PACKAGING
This section is not applicable to this specification.
5.1
6.
NOTES
Intended use. This specification is intended for use in preparing
6.1
analyses of the electric load and power source capacity for aircraft.
Definitions. The following definitions are applicable to the
6.2
terminology used in this specification.
6. 2.1
Analyses.
6.2.1.1
Electric load and power source utilization analysis. An
electric load and power source utilization analysis for an aircraft consists of indivi-
dual analyses of each electric power system, which is used in line maintenance,
operation, or both, of the aircraft. Each of these individual analyses is called a
system analysis.
System analysis. A system analysis is an electric load and power
6.2.1.2
source utilization analysis for an individual electric power system. In this speci-
fication, the system analysis is divided into a load analysis and a power source
analysis.
Load analysis. A load analysis is essentially a summation of the
6.2.1.3
electric loads applied to the particular system during specified operating conditions
of the aircraft.
Power source analysis. A power source analysis Consists of
6.2.1.4
determining the capacity of the power source for the same operating conditions
specified for the load analysis. The power source analysis includes the calculation
of percent growth capacity (see 6.2. 6).
Electric system. An electric system consists of an electric
6.2.2
power source, its power distribution system, and the electric load connected thereto.
Electric sources.
6.2.3
6.2.3.1
Electric source. An electric source is the electric equipment
which produces, converts, or transforms electric power. Common ac sources are
ac generators inverters, transformers, and frequency changers. Common dc sources
are dc generators, converters and batteries. A source may consist of multiple unit
sources operating in parallel.
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