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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
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gptkb:military_aircraft
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gptkbp:certification
|
military certification
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|
gptkbp:compression_ratio
|
6.5:1
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|
gptkbp:configuration
|
gptkb:V12
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gptkbp:cooling_system
|
gptkb:Cooler
gptkb:water
liquid cooling
liquid-cooled
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gptkbp:displacement
|
1,200 cc
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gptkbp:engine
|
gptkb:BMW_aircraft_engines
lightweight materials
modular design
every 500 hours
developed during interwar period
influenced future aircraft engines
aviation market
400 hp at 2,000 rpm
advanced metallurgy used
included supercharger
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|
gptkbp:engine_configuration
|
V engine
air-cooled
132-001
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|
gptkbp:engine_power
|
high reliability
1,500 hours
high altitude performance
2,000 rpm
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|
gptkbp:engine_production_method
|
mass production
|
|
gptkbp:engine_type
|
gptkb:BMW_132_K
reciprocating engine
|
|
gptkbp:first_flight
|
1926
|
|
gptkbp:first_introduced
|
1920s
|
|
gptkbp:fuel_capacity
|
300 kg without accessories
|
|
gptkbp:fuel_economy
|
50 L/h
|
|
gptkbp:fuel_type
|
gptkb:carburetor
aviation gasoline
|
|
gptkbp:historical_significance
|
used in WWII aircraft
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
BMW 132
|
|
gptkbp:ignition_system
|
magneto
|
|
gptkbp:is_tested_for
|
bench testing
|
|
gptkbp:maintenance
|
routine maintenance required
|
|
gptkbp:manufacturer
|
gptkb:BMW
|
|
gptkbp:notable_users
|
gptkb:Luftwaffe
|
|
gptkbp:number_of_engines
|
gptkb:12
|
|
gptkbp:power_output
|
400 hp
|
|
gptkbp:production_location
|
gptkb:Germany
|
|
gptkbp:production_years
|
1926-1945
|
|
gptkbp:propulsion
|
1.33 hp/kg
|
|
gptkbp:replaced_by
|
gptkb:BMW_801
|
|
gptkbp:successor
|
gptkb:BMW_801
|
|
gptkbp:torque
|
1,200 Nm
1,200 Nm at 1,500 rpm
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|
gptkbp:type
|
inline engine
|
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gptkbp:used_in
|
Bavarian aircraft
|
|
gptkbp:valve_configuration
|
overhead valves
|
|
gptkbp:weight
|
300 kg
|
|
gptkbp:bfsParent
|
gptkb:Focke-Wulf_Fw_200_Condor
gptkb:Arado_Ar_196
gptkb:Junkers_Ju_52
|
|
gptkbp:bfsLayer
|
6
|