Heating System & Cooling System Flashcards
BLEED AIR HEAT SYSTEM USES _______________ IN HELICOPTER CABINS TO COMBINE BLEED AIR WITH CABIN AIR.
MINI-EJECTORS
SOME TURBINE-POWERED AIRCRAFT NOT EQUIPPED WITH AIR CYCLE SYSTEMS STILL MAKE USE OF ______________________ TO HEAT THE CABIN.
ENGINE COMPRESSOR BLEED AIR
TEMPERATURES AT HIGH ALTITUDES IN WHICH AIRCRAFT OPERATE CAN BE WELL BELOW _____.
0 °F
______________________THAT USE AIR CYCLEAIR CONDITIONING SYSTEMSMIX BLEED AIR WITH COLD AIR PRODUCED BY THE ________________________________ TO OBTAIN WARM AIR FOR THE CABIN.
PRESSURIZED AIRCRAFT
AIR CYCLE MACHINE EXPANSION TURBINE
AIRCRAFT ___________ WITH AIR CYCLE AIR CONDITIONING MAY BE HEATED BY ONE OF A FEW POSSIBLE METHODS.
NOT EQUIPPED
THE BLEED AIR IS MIXED WITH AMBIENT AIR, OR CABIN RETURN AIR, AND DISTRIBUTED THROUGHOUT THE ______________________.
AIRCRAFT VIA DUCTING
THE MIXING OF AIR CAN BE DONE IN A VARIETY OF WAYS.
4 ways
- MIXING AIR VALVES
- FLOW CONTROL VALVES
- SHUTOFF VALVES
- VARIOUS CONTROL VALVES CONTROLLED BY SWITCHES IN THE COCKPIT
OCCASIONALLY, AN _____________________ IS USED TO HEAT THE AIRCRAFT.
ELECTRIC HEATING DEVICE
ELECTRICITY FLOWING THROUGH A _______________ MAKES THE ELEMENT WARM. A FAN TO BLOW AIR OVER THE ELEMENTS AND INTO THE CABIN IS USED TO TRANSFER THE HEAT.
HEATING ELEMENT
OTHER ___________________ SIMPLY RADIATE HEAT TO WARM THE CABIN.
FLOOR OR SIDEWALL ELEMENTS
_______________________________ REQUIRE A SIGNIFICANT AMOUNT OF THE AIRCRAFT’S GENERATOR OUTPUT, WHICH IS BETTER DEDICATED TO THE OPERATION OF OTHER ELECTRICAL DEVICES. FOR THIS REASON, THEY ARE NOT VERY COMMON. HOWEVER, THEIR USE ON THE GROUND WHEN POWERED BY A GROUND ELECTRICAL POWER SOURCE PREHEATS THE CABIN BEFORE PASSENGERS BOARD AND DOES NOT TAX THE ELECTRICAL SYSTEM.
ELECTRIC HEATING ELEMENT HEATERS
MOST ________________ LIGHT AIRCRAFT USE EXHAUST SHROUD HEATING SYSTEMS TO HEAT THE CABIN.
SINGLE-ENGINE
AMBIENT AIR IS DIRECTED INTO A METAL SHROUD, OR JACKET, THAT ENCASES PART OF THE ENGINE’S_________________. THE AIR IS WARMED BY THE EXHAUST AND DIRECTED THROUGH A FIREWALL HEATER VALVE INTO THE CABIN. THIS SIMPLE SOLUTION REQUIRES NO ELECTRICAL OR ENGINE POWER AND IT MAKES USE OF HEAT THAT WOULD OTHERWISE BE WASTED.
EXHAUST SYSTEM
MOST INVOLVE PRESSURIZING THE EXHAUST SYSTEM WITH AIR, WHILE INSPECTING FOR LEAKS WITH A _________________. SOME REQUIRE THE EXHAUST TO BE REMOVED AND PRESSURIZED WHILE SUBMERGED UNDER WATER TO DETECT ANY LEAKS.
SOAPY SOLUTION
FREQUENCY OF EXHAUST HEAT LEAK DETECTION CAN BE EVERY _____ HOURS.
100
_________________ ARE SIMILAR TO EXHAUST SHROUD HEATERS IN THAT AMBIENT AIR IS HEATED AND SENT TO THE CABIN. THE SOURCE OF HEAT IN THIS CASE IS AN INDEPENDENT COMBUSTION CHAMBER LOCATED INSIDE THE CYLINDRICAL OUTER SHROUD OF THE HEATER UNIT. THE CORRECT AMOUNT OF FUEL AND AIR ARE IGNITED IN THE AIR-TIGHT INNER CHAMBER. THE EXHAUST FROM COMBUSTION IS FUNNELED OVERBOARD.
COMBUSTION HEATERS
AMBIENT AIR IS DIRECTED BETWEEN THE COMBUSTION CHAMBER AND THE OUTER SHROUD. IT ABSORBS THE COMBUSTION HEAT BY _________ AND IS CHANNELED INTO THE CABIN.
CONVECTION
5 Types of aircraft heating system
Bleed air systems
electric heating systems
exhaust shroud haters
combustion heaters
ventilating air system
A major concern of exhaust shroud heat systems is the possibility that exhaust gases could __________ the cabin air
Contaminate
Occasionally, the exhaust system is slightly modified in a shroud heat configuration. For example, an exhaust muffler may have numerous ________ attached, which increase heat transfer to the cabin air
welded studs