Lab 1 Recip Engines HW (1)

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Western Michigan University *

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1235

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Mechanical Engineering

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Feb 20, 2024

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AVS 1235 Project Home Work #1 Engine Research Reciprocating Engines – WMU Fleet Purpose: Research several aircraft to determine the powerplant installed. Research the reciprocating engines used on the WMU fleet of aircraft. Become familiar with model designation and specifications of various aircraft reciprocating engines. Reference: Cirrus POH Seminole POH Arrow POH Aircraft specific websites ELearning Material Internet Procedure: Using College of Aviation Electronic Flight Bag on ELearning and the internet, find the following information about the powerplants installed on the aircraft listed below. Aircraft #1: Cirrus SR20 Manufacturer: _The cirrus design company______________________ Model: __IO-360-ES_____________________ Horsepower: __200 HP at 2700 RPM_____________________ Aircraft #2 Piper PA-44-180 Seminole Left Engine – Manufacturer: __Lycoming_____________________ Model: _180______________________
Horsepower: _0-360-A1H6______________________ Right Engine – Manufacturer: _Lycoming______________________ Model: _LO-360-A1H6______________________ Horsepower: _180 HP 2 2700 rpm______________________ Aircraft #3 – Piper PA-28R-201 Arrow IV Manufacturer: _Lycoming______________________ Model: _IO-360-C1C6______________________ Horsepower: _200 HP @2700 rpm______________________ Aircraft #4 – Airbus A380 Option 1 – Manufacturer: __Airbus_____________________ Model: _____A380__________________ Thrust: ___332.44-356.81kN____________________ Option 2 – Manufacturer: _Rolls-Royce____________________ Model: _______________________ Thrust: __70,000 dbf or 7,000 dbf (Capable of 81,000 lbf)___ Aircraft #5 – Beechcraft B90 King Air Manufacturer: Pratt and Whitney Canada___ Model: PT5A-27___ Horsepower: _680 she (715 esop)___
Aircraft #6 – Piper PA-32R-301T Saratoga TC Manufacturer: Lycoming___ Model: __TIO-540-AHIA_____ Horsepower: __300______ Aircraft #7 – Boeing 787 Dreamliner Option 1 – Manufacturer: ___General Electric Aviation________ Model: ___GEnx-1B_______ Thrust: ___66,500- 78,000 lbf_______ Option 2 – Manufacturer: __Rolls -Royce_____________________ Model: ___Trent 1000____________________ Thrust: ___53,000 - 78000 lbf____________________ Aircraft #8 – Boeing 777-300 Option 1 – Manufacturer: ___Pratt and whitney_____ Model: ___4000____________________ Thrust: __98,000 dbf (takeoff): 77,000 dbf (max continuous)____ Option 2 – Manufacturer: _Rolls Royce_____ Model: __Trent 800_______ Thrust: __94,000 lbf______
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Option 3 – Manufacturer: _General Electric Aviation______________________ Model: __GE90-92B/94B_____________________ Thrust: __94,000_____________________ Aircraft #9 – North American P-51D Mustang Manufacturer: _Packard Motor Car Company________ Model: ___V-1650-7____________________ Horsepower: __1,490 @ 3,000rpm (1,720 @ WEP______ Aircraft #10 – Piper PA-34-220T Seneca V Manufacturer: _Continental Motors____________ Model: __TISO-360-RB_____________________ Horsepower: __220_______________
Answer the following ques1ons 1. The engines on the Seminole are Lycoming (L)O-360-A1H6. Fill in the blanks with the meanings of engine model designators: O: ______Horizontally Opposed____________ 360: __360 Cubic square inches displacement_______________ L: _____LeC Engine________________________ A1H6: ___Accessory Horepower______________ Refer to Lycoming Service Instruc1on 1009AW to answer ques1ons 2-4. 2. What is the time between overhaul (TBO) for the Seminole engines? 2000 hours 3. Under what conditions could WMU extend the Seminole TBO by 200 hours? If the aircraft is flown over 40 hours per month since the engine was placed in service. 4. What is the TBO for the Arrow engine? 1400 hours 5. The engine on the Super Decathlon is a Lycoming AEIO-360-H1B. Fill in the blanks with the meanings of engine model designators: AE: __Aeroba1c Engine _________________________________
I: ____Fuel Injected _______________________________ O: ___Opposed Cylinders __________________________ 360: ___360 Cubic displacement __________________________ H1B:_____H indicates Horizontal Helicopter, 1 indicates the design of nose sec1on and B indicates Accessory Sec1on________________________ 6. The engine in the Cirrus is rated at 200 hp. What is the maximum rated horsepower for that engine model, according to the Maintenance and Operators Manual? 200 HP for 2700 RPM 7. Using the IO-360 Maintenance and Operators Guide, write the terms, not the definition, for the following engine acronyms. ABC ___ACer BoWom Center____________ ATC ____ACer Top Center_______________ BHP ____Brake Horsepower ______________ BSFC ____Brake Specific Fuel Consump1on____ BTC ___Before___Top______Center__________ CHT ____Cylinder Head Temperature EGT ____Exhaust gas temperature ______________
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GPM ___Gallons Per Minute__________________ MAP ___Manifold Pressure___________________ OAT _____Outside Air Temperature ________ PPH ____Pounds Per Hour___________________ RPM ____Revolu1ons Per Minute______________ TDC ___Top Dead Center_____________________
Fill in the blanks on the chart below. (Reference: Seminole POH, IO-360 Operators Guide and Arrow POH) WMU Fleet Engine Informa3on Cirrus SR20 Piper Arrow Piper Seminole Manufacturer Teledyne Con1nental Lycoming Lycoming Model IO-360-ES IO-360-C1C6 (L)O-360-A1H6 Horsepower 200(210 Max) 200 180 Displacement 360in^ 3 360in^3 361in^3 Cylinders 6 4 4 Bore 4.44 in 5.125 in 5.125 in Stroke 3.88 in 4.375 in 4.375 in Fuel Metering Type Fuel Injected Fuel Injected Carburetor TBO 1,500 hours 2,000 Hours 2,00 Hours