Electrical system(民航飞机电气系统1)
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Chapter 1 Aircraft Electrical System
1
Chapter 1 Aircraft Electrical system
• Electrical component • Storage Battery • DC & AC Generator • Control and Protection in DC Electrical System
20
Secondary source.
• A secondary source is equipment that transforms and/or converts primary source power to supply electrical power
to either AC or DC powered equipment.
10
• Jet
airliners
have
extremely complex
electrical systems and use alternating current as the primary source of electricity. • Batteries are used for emergency and backup operations and for some special
19
Secondary Source
• A secondary source is equipment that transforms and/or converts primary source power to supply electrical power to either AC or DC powered equipment .
Flyer. In those days the role of
electricity was limited to the magneto which provides sufficient voltage to spark the fuel/air mixture.
6
Magnetos still supplied the spark to the
13
A
typical
aircraft
power and
electrical
source,
system
consists of a primary (main) power source, emergency power control secondary system devices, conversion equipment, protection
interconnection
network,
and
power
distribution system.
14
Electrical Source
The electrical equipment which produces, converts or transforms electrical power.
Minimum
Transformer
Equipment
Rectifier
List
Units,
(MMEL)
Inverters,
limitations (e.g. AC and/or DC Generators, Main Batteries, APU etc.).
28
Abnormal electrical power operation
operate the electric motor used to start the
engines.
7
8
• The years between the two world wars is
the golden age of aviation, improved in importance and complexity. • As the twentieth century ended, electrical systems have become just about equal in
applications.
11
DEFINITIONS OF AIRCRAFT ELECTRICAL SYSTEM
12
Electrical System
An electrical system consists
its
of
an
electrical
power
source,
power
distribution system and the electrical load connected to that system.
powered independently of aircraft battery
or generating systems. The source can be either a motorised generating unit or a battery unit.
25
Nominal rating
This rating is usually a continuous duty rating for specified operating conditions.
26
Condition of Power Sources
• Normal electrical power operation • Abnormal electrical power operation • Emergency electrical power operation
Emergency operation is a condition that occurs following a loss of all normal electrical generating power sources or
other malfunction that results in operation
importance with the engines.
9
• For many years, light planes exclusively used the 14-volt electrical system. Starting approximately in the early 1980s, the 28volt system began to take over light aircraft.
engines, but 14- or 28-volt direct-current generator supplied current to operate the navigation and landing lights, the radios. Generators kept the batteries charged to
In the event of a primary power source failure, provided emergency from or power is usually auxiliary independent
power
ram
unit
air
(APU)-driven
generator(s),
• A secondary source is entirely dependent
upon
source.
the
primary
source
and
is
considered part of the load of the primary
21
Emergency Power Source
22
Emergency power
来自百度文库
mechanical, chemical energy etc.
• Easily and economically transportable by
means of running cables.
4
5
• Electrical systems have been an
onboard fixture since the Wright
Some common DC sources are
• DC generators • converters
• batteries.
17
Primary (Main) Power Source
18
Primary Power Source
A primary source is equipment that generates electrical power from energy other than electrical, and is independent of any other electrical source.
15
Electrical Source
Some common AC sources are identified as follows:
• AC alternators
• inverters
• transformers • frequency changers.
16
Electrical Source
on standby power (batteries and or other emergency generating source such as an APU or Ram Air Turbine (RAT) only.
30
Classification of electrical load
remove the malfunction or the failure from the remainder of the system before the limits of abnormal operation are exceeded.
29
Emergency electrical power operation
27
Normal electrical power operation
Normal operating conditions assumes that all of the available electrical power system is functioning correctly within Master
hydraulically-driven
generator(s), or batteries.
23
Ground power
24
ground power source
A ground power source can be connected to the bus bar distribution system thus allowing all electrical systems to be
• Electrical Machine and control
• Lighting
2
When, Why Electric Energy was used in an aircraft?
3
Electrical energy is being widely used
• Clean form of energy – absence of smoke, ashes, dust, etc. • Easily convertible to light, heat,
• Vital (critical, emergency) • Essential • Non-essential
31
32
Typical Aircraft Electrical System
• Primary (main) power source • Emergency power source • Secondary power conversion equipment • System control and protection devices
Abnormal operation occurs when a
malfunction or failure in the electric system has taken place and the protective
devices of the system are operating to
• The primary purpose of fuel/air mixture is still the magneto. However, the electrical energy in the increased tremendously. igniting the domain of the demand for airplane has
1
Chapter 1 Aircraft Electrical system
• Electrical component • Storage Battery • DC & AC Generator • Control and Protection in DC Electrical System
20
Secondary source.
• A secondary source is equipment that transforms and/or converts primary source power to supply electrical power
to either AC or DC powered equipment.
10
• Jet
airliners
have
extremely complex
electrical systems and use alternating current as the primary source of electricity. • Batteries are used for emergency and backup operations and for some special
19
Secondary Source
• A secondary source is equipment that transforms and/or converts primary source power to supply electrical power to either AC or DC powered equipment .
Flyer. In those days the role of
electricity was limited to the magneto which provides sufficient voltage to spark the fuel/air mixture.
6
Magnetos still supplied the spark to the
13
A
typical
aircraft
power and
electrical
source,
system
consists of a primary (main) power source, emergency power control secondary system devices, conversion equipment, protection
interconnection
network,
and
power
distribution system.
14
Electrical Source
The electrical equipment which produces, converts or transforms electrical power.
Minimum
Transformer
Equipment
Rectifier
List
Units,
(MMEL)
Inverters,
limitations (e.g. AC and/or DC Generators, Main Batteries, APU etc.).
28
Abnormal electrical power operation
operate the electric motor used to start the
engines.
7
8
• The years between the two world wars is
the golden age of aviation, improved in importance and complexity. • As the twentieth century ended, electrical systems have become just about equal in
applications.
11
DEFINITIONS OF AIRCRAFT ELECTRICAL SYSTEM
12
Electrical System
An electrical system consists
its
of
an
electrical
power
source,
power
distribution system and the electrical load connected to that system.
powered independently of aircraft battery
or generating systems. The source can be either a motorised generating unit or a battery unit.
25
Nominal rating
This rating is usually a continuous duty rating for specified operating conditions.
26
Condition of Power Sources
• Normal electrical power operation • Abnormal electrical power operation • Emergency electrical power operation
Emergency operation is a condition that occurs following a loss of all normal electrical generating power sources or
other malfunction that results in operation
importance with the engines.
9
• For many years, light planes exclusively used the 14-volt electrical system. Starting approximately in the early 1980s, the 28volt system began to take over light aircraft.
engines, but 14- or 28-volt direct-current generator supplied current to operate the navigation and landing lights, the radios. Generators kept the batteries charged to
In the event of a primary power source failure, provided emergency from or power is usually auxiliary independent
power
ram
unit
air
(APU)-driven
generator(s),
• A secondary source is entirely dependent
upon
source.
the
primary
source
and
is
considered part of the load of the primary
21
Emergency Power Source
22
Emergency power
来自百度文库
mechanical, chemical energy etc.
• Easily and economically transportable by
means of running cables.
4
5
• Electrical systems have been an
onboard fixture since the Wright
Some common DC sources are
• DC generators • converters
• batteries.
17
Primary (Main) Power Source
18
Primary Power Source
A primary source is equipment that generates electrical power from energy other than electrical, and is independent of any other electrical source.
15
Electrical Source
Some common AC sources are identified as follows:
• AC alternators
• inverters
• transformers • frequency changers.
16
Electrical Source
on standby power (batteries and or other emergency generating source such as an APU or Ram Air Turbine (RAT) only.
30
Classification of electrical load
remove the malfunction or the failure from the remainder of the system before the limits of abnormal operation are exceeded.
29
Emergency electrical power operation
27
Normal electrical power operation
Normal operating conditions assumes that all of the available electrical power system is functioning correctly within Master
hydraulically-driven
generator(s), or batteries.
23
Ground power
24
ground power source
A ground power source can be connected to the bus bar distribution system thus allowing all electrical systems to be
• Electrical Machine and control
• Lighting
2
When, Why Electric Energy was used in an aircraft?
3
Electrical energy is being widely used
• Clean form of energy – absence of smoke, ashes, dust, etc. • Easily convertible to light, heat,
• Vital (critical, emergency) • Essential • Non-essential
31
32
Typical Aircraft Electrical System
• Primary (main) power source • Emergency power source • Secondary power conversion equipment • System control and protection devices
Abnormal operation occurs when a
malfunction or failure in the electric system has taken place and the protective
devices of the system are operating to
• The primary purpose of fuel/air mixture is still the magneto. However, the electrical energy in the increased tremendously. igniting the domain of the demand for airplane has