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ورق بلا هدف

This document appears to be a midterm exam for a mechanical power engineering course. It contains 3 questions related to internal combustion engine design. Question 1 involves correcting statements about engine design and materials. Question 2 involves using performance map data to select engine parameters like displacement and cylinders to meet power requirements. Question 3 involves piston, connecting rod, and force analysis calculations to design these components for a specific engine.

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0% found this document useful (0 votes)
44 views37 pages

ورق بلا هدف

This document appears to be a midterm exam for a mechanical power engineering course. It contains 3 questions related to internal combustion engine design. Question 1 involves correcting statements about engine design and materials. Question 2 involves using performance map data to select engine parameters like displacement and cylinders to meet power requirements. Question 3 involves piston, connecting rod, and force analysis calculations to design these components for a specific engine.

Uploaded by

mosaadm
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
You are on page 1/ 37

Mechanical Power Engineering 4th year MPE

Mansoura
Department 1st semester
University
Faculty of Engineering Mid-Term 2020-2021

Course Title: Design of Mechanical


Total Marks 25
Power Engines No. of Pages: 3+Tables
Allowed Time 1.25 hours
Course Code: MPE4414
Name:…………………………………..……………………………………..Sec.( )
Assume reasonably any missing data – Give units of ALL deduced quantities

Question No. (1) : Correct the following expressions if there are mistakes: (8 Marks)
1. The over square engine has lower piston speed and higher heat transfer losses compared with
the under square engine.
1
(True)

2. Maximum brake torque occurs at engines speeds lower than the ones at which maximum
brake mean effective pressure occurs. 1
Maximum brake torque occurs at engines speeds equal to the ones at which maximum
brake mean effective pressure occurs.
3. Gas turbines are considered common examples of external combustion engines at which the
combustion occurs in a combustion chamber outside the turbine itself. 1
Gas turbines are considered common examples of internal combustion engines at which
the combustion occurs in a combustion chamber before the turbine itself.
4. Fiber reinforcement is used to decrease thermal conductivity of the aluminum alloys used for
piston fabrication and hence reduces heat losses from combustion chamber. 1
Fiber reinforcement is used to increase thermal and mechanical loads limits of the
aluminum alloys used for piston fabrication.
5. Advantages of sintered conrods include lower weight, higher velocity limit, and lower cost
compared to forged conrods which make sintered rods suitable for modern engines. 1
Advantages of sintered conrods include lower weight and higher velocity limit but higher
cost compared to forged conrods which make sintered rods suitable for modern engines.
6. Steel alloys are commonly used for the fabrication of crankshafts because of the lower weight
compared with cast iron crankshafts.
1
Steel alloys are commonly used for the fabrication of crankshafts because of the higher
strength compared with cast iron crankshafts.
7. The connecting rod connects the piston and the flywheel and is responsible for converting the
linear motion to a rotating motion. 1
The connecting rod connects the piston and the crankshaft and is responsible for
converting the linear motion to a rotating motion.
8. At least 3 journal bearings are used to hold an overhung crankshaft.
1
At least 3 journal bearings are used to hold a center crankshaft.

Page 1 of 4
Question No. (2) : (7 Marks)
The following figure represents a
performance map for a 4-stroke naturally
aspirated spark ignition engine. If the engine
provides a maximum power of 143 kW at a
speed of 5200 rpm, select proper values of
different operating parameters including
engine displacement, bore, stroke, and
number of cylinders that satisfy the engine
requirements. Use OPD parameter to verify
your result.

𝑷𝒃 = 𝑻. 𝝎
𝟐𝝅 × 𝟓𝟐𝟎𝟎
𝟏𝟒𝟑 × 𝟏𝟎𝟎𝟎 = 𝑻 × 1
𝟔𝟎
∴ 𝑻 = 𝟐𝟔𝟐. 𝟔 𝑵. 𝒎
From chart:
∴ 𝒃𝒎𝒆𝒑 = 𝟏𝟏 𝒃𝒂𝒓 1
Typical values from table:
let
𝑵𝒄 = 𝟔 𝒄𝒚𝒍𝒊𝒏𝒅𝒆𝒓𝒔 1
𝑺
=𝟏
𝑩
𝑵
𝑷𝒃 = 𝒃𝒎𝒆𝒑𝑽𝒅 𝑵𝒄 1
𝒏
𝝅 𝟐 𝟓𝟐𝟎𝟎
𝟏𝟒𝟑 = 𝟏𝟏 × 𝟏𝟎𝟎 × 𝑩 𝑺×𝟔×
𝟒 𝟔𝟎 × 𝟐
∴ 𝑩𝟐 𝑺 = 𝑩𝟑 = 𝟎. 𝟎𝟎𝟎𝟔𝟑𝟕 1
∴ 𝑩 = 𝑺 = 𝟖. 𝟔 𝒄𝒎
Engine displacement
𝝅 𝟐
𝑽𝒅,𝒕𝒐𝒕 = 𝑩 𝑺𝑵𝒄
𝟒
𝝅
= × 𝟖. 𝟔𝟑 × 𝟔 = 𝟐𝟗𝟗𝟕. 𝟑𝟒𝟑 𝒄𝒎𝟑 ≈ 𝟑 𝑳 1
𝟒
Check:
𝑷𝒃 𝟏𝟒𝟑
𝑶𝑷𝑫 = = = 𝟒𝟕. 𝟕 𝒌𝑾/𝑳 1
𝑽𝒅,𝒕𝒐𝒕 𝟑
Which verify the OPD span in tables (40:80 kW/L)

Page 2 of 4
Question No. (3) : (10 Marks)
It is required to design the piston and connecting rod of a 3L 4-stroke 6-cylinder SI engine. The engine
has a bore of 8.8 cm and connecting rod to crank offset ratio of 4. If the maximum allowable pressure
inside the combustion chamber is 5 MPa, find suitable dimensions for piston including its crown, barrel,
skirt, and its rings and pin. Give also proper dimensions of the conrod I-section and perform force
analysis to calculate the maximum stress upon the conrod at 5000 rpm when a right angle is created
1
between the conrod the crank arm. (Take the constant 𝛼 in Rankine-Gordon equation to be for steel
7500
conrod)
Piston crown thickness: 1 𝝈𝒃𝒓 = 𝟎. 𝟑 𝑴𝑷𝒂 for low speed engines
Let the piston be ∴ 𝒍𝟏 ≈ 𝟓𝟖 𝒎𝒎
made of aluminum
Let total piston length = 1.5 D= 132 mm
with a design stress
(𝑺𝒅 = 𝟒𝟎 𝑴𝑷𝒂) Clearance:
Grashoff’s formula For crown= 0.01 D= 0.88 mm
For skirt= 0.002 D= 0.18 mm
𝑷𝒎𝒂𝒙
𝒕 = 𝟎. 𝟒𝟑𝑫√
𝑺𝒅 Piston pin (made from steel) 1
𝑳𝒑𝒊𝒏 = 𝑫 − 𝟓 = 𝟖𝟑 𝒎𝒎
𝟓 Let 𝒅𝒐 = 𝟏. 𝟐𝒅𝒊
= 𝟎. 𝟒𝟑 × 𝟖𝟖√ ≈ 𝟏𝟒 𝒎𝒎
𝟒𝟎
𝑰 𝝅
𝒛= = (𝒅𝟒 − 𝒅𝟒𝒊 )
Piston rings (assuming CI rings) 1 𝒄 𝟑𝟐𝒅𝒐 𝒐
𝝅 𝒅𝟒𝟎
= (𝒅𝟒𝒐 − )
𝟑𝟐𝒅𝒐 𝟏. 𝟐𝟒
𝒃 ≈ 𝟎. 𝟎𝟑𝑫 ≈ 𝟑 𝒎𝒎
= 𝟎. 𝟎𝟓𝟎𝟖𝟑𝒅𝟑𝒐
Let: 𝒉 = 𝒃 = 𝟑 𝒎𝒎
𝑭𝒑 𝑳𝒑𝒊𝒏 𝟎. 𝟎𝟖𝟑
Check for 4 rings 𝑴= = 𝟑𝟎𝟒𝟏𝟎 × = 𝟔𝟑𝟏 𝑵. 𝒎
𝟐 𝟐 𝟒
𝑫 𝟖𝟖 𝑴
𝒉𝒎𝒊𝒏 = = = 𝟐. 𝟐 𝒎𝒎 Bending stress: 𝝈𝒃 = = 𝟏𝟎𝟎 𝑴𝑷𝒂
𝟏𝟎𝒏 𝟏𝟎 × 𝟒 𝒛

Top land: ∴ 𝒅𝒐 ≈ 𝟓𝟎 𝒎𝒎, 𝒅𝒊 ≈ 𝟒𝟐 𝒎𝒎


𝒉𝟏 = 𝒕 = 𝟏𝟒 𝒎𝒎 𝑭𝒑 ⁄𝟐
𝝈𝒔 = 𝝅 = 𝟐𝟔. 𝟑 𝑴𝑷𝒂 < 𝟒𝟎𝑴𝑷𝒂
Width of ring grooves: (𝒅𝟐𝒐 − 𝒅𝟐𝒊 )
𝟒
𝒉𝟐 = 𝒉 = 𝟑 𝒎𝒎 𝑭𝒑
𝝈𝒃𝒓 = = 𝟏𝟎 𝑴𝑷𝒂, ∴ 𝒍𝒆𝒏𝒅 ≈ 𝟔𝟏 𝒎𝒎
𝒅𝒐 𝑳𝒆𝒏𝒅
Barrel and skirt 2
For conrod
𝒕𝟏 = 𝒃 + 𝟎. 𝟎𝟑𝑫 + 𝟎. 𝟒𝟔
𝝅
= 𝟑 + 𝟎. 𝟎𝟑 × 𝟖𝟖 + 𝟎. 𝟒𝟔 𝑽𝒅,𝒕𝒐𝒕 = 𝑩𝟐 𝑺𝑵𝒄
𝟒
𝝅
≈ 𝟕 𝒎𝒎 𝟑𝟎𝟎𝟎 = 𝟖. 𝟖𝟐 𝑺 × 𝟔, ∴ 𝑺 = 𝟖. 𝟑 𝒄𝒎
𝟒
𝑹𝒍,𝒎𝒂𝒙 𝑺
𝒍𝟏 = ∴ 𝒂 = = 𝟒. 𝟏𝟓 𝒄𝒎
𝑫𝝈𝒃𝒓 𝟐
1
𝑹𝒍,𝒎𝒂𝒙 = 𝟎. 𝟎𝟓𝑭𝒑 , 𝑭𝒑 = 𝑷𝒎𝒂𝒙 𝑨𝒑 ∴ 𝒓 = 𝟒𝒂 = 𝟏𝟔. 𝟔 𝒄𝒎
𝝅 𝟖.𝟖 𝟐
𝑭𝒑 = 𝟓𝟎𝟎𝟎 × ( ) = 𝟑𝟎. 𝟒𝟏 𝒌𝑵
𝟒 𝟏𝟎𝟎

∴ 𝑹𝒍,𝒎𝒂𝒙 = 𝟏𝟓𝟐𝟎. 𝟓𝟑𝟏 𝑵 Best Wishes


Dr. Waleed M. Shaaban
Dr. Mahmoud A. Shouman

Page 3 of 4
For I-section 1
Let 𝑯 = 𝟓𝒕, 𝑩 = 𝟒𝒕 𝑰𝒙𝒙 = 𝟖. 𝟑𝟖 × 𝟏𝟎−𝟖 𝒎𝟒
𝑨 = 𝟏𝟏𝒕𝟐 , 𝑴
𝟒𝟏𝟗 𝟒 𝑴′ = = 𝟑𝟑𝟗. 𝟏𝟓 𝑵. 𝒎
𝟏 − 𝝃𝑭𝒂
𝑰𝒙𝒙 = 𝒕
𝟏𝟐 𝑯
𝒌𝒙𝒙 = 𝟏. 𝟕𝟖𝟐𝒕 𝒄= = 𝟏𝟕. 𝟓 𝒎𝒎
𝟐
𝝈𝒄 = 𝟑𝟑𝟎 𝑴𝑷𝒂 𝒇𝒐𝒓 𝒔𝒕𝒆𝒆𝒍 Combined stress 1
𝝈𝒄 𝑨 ′
𝑭𝒂 𝒄𝑴
𝑭𝒄 = = 𝟓𝑭𝒑 𝝈= + = 𝟏𝟐𝟕. 𝟐𝟐 𝑴𝑷𝒂
𝒓 𝑨 𝑰𝒙𝒙
𝟏+ 𝜶( )
𝒌𝒙𝒙 < 𝟑𝟑𝟎 𝑴𝑷𝒂 𝒇𝒐𝒓 𝒔𝒕𝒆𝒆𝒍
𝟑𝟑𝟎 × 𝟏𝟎𝟔 × 𝟏𝟏𝒕𝟐
= 𝟓 × 𝟑𝟎𝟒𝟏𝟎
𝟏 𝟎. 𝟏𝟔𝟔
𝟏+ ( )
𝟕𝟓𝟎𝟎 𝟏. 𝟕𝟖𝟐𝒕
∴ 𝒕 = 𝟕 𝒎𝒎, 𝑯 = 𝟑𝟓 𝒎𝒎, 𝑩 = 𝟐𝟎 𝒎𝒎
Big end depth= 1.1H= 39 mm
Small end depth= 0.8H= 28 mm
Force analysis 2
𝒂
∅ = 𝒕𝒂𝒏−𝟏 = 𝟏𝟒. 𝟎𝟑°
𝒓
𝜽 = 𝟗𝟎 − ∅ = 𝟕𝟓. 𝟗𝟔°
𝒂
𝒂𝒑 = 𝝎𝟐 𝒂(𝒄𝒐𝒔𝜽 + 𝒄𝒐𝒔𝟐𝜽)
𝒓
𝟐𝝅 × 𝟓𝟎𝟎𝟎 𝟐
=( )
𝟔𝟎
× 𝟎. 𝟎𝟒𝟏𝟓(𝒄𝒐𝒔𝟕𝟓. 𝟗𝟔
+ 𝟎. 𝟐𝟓𝒄𝒐𝒔𝟐 × 𝟕𝟓. 𝟗𝟔)
= 𝟐𝟒𝟗. 𝟕 𝒎⁄𝒔𝟐
Let weight of reciprocating parts= 2 kg
𝑾𝑹
𝑭𝑰𝑹 = 𝒂 = 𝟐 × 𝟐𝟒𝟗. 𝟕 = 𝟒𝟗𝟗. 𝟒 𝑵
𝒈 𝒑
𝑭𝒑 − 𝑭𝑰𝑹 𝟑𝟎𝟒𝟏𝟎 − 𝟒𝟗𝟗. 𝟒
𝑭𝒂 = =
𝒄𝒐𝒔∅ 𝒄𝒐𝒔𝟏𝟒. 𝟎𝟑
= 𝟑𝟎𝟖𝟑𝟏. 𝟕𝟕 𝑵
𝑴 = 𝟎. 𝟎𝟔𝟒𝒓𝟑 𝝆𝑨𝝎𝟐 𝐬𝐢 𝐧(𝜽 + ∅)
= 𝟎. 𝟎𝟔𝟒 × 𝟎. 𝟏𝟔𝟔𝟑 × 𝟕𝟖𝟎𝟎 × 𝟏𝟏
𝟐(
𝟐𝝅 × 𝟓𝟎𝟎𝟎 𝟐
× (𝟕/𝟏𝟎𝟎𝟎) ) 𝐬𝐢 𝐧(𝟗𝟎)
𝟔𝟎
= 𝟑𝟑𝟕. 𝟒𝟑 𝑵. 𝒎
Let E=200 GPa
𝟎. 𝟏𝒓𝟐 𝟎. 𝟏 × 𝟎. 𝟏𝟔𝟔𝟐
𝝃= =
𝑬𝑰𝒙𝒙 𝟒𝟏𝟗 𝟕 𝟒
𝟐𝟎𝟎 × 𝟏𝟎𝟗 × ( )
𝟏𝟐 𝟏𝟎𝟎𝟎
= 𝟏. 𝟔𝟒𝟑𝟒𝟕 × 𝟏𝟎−𝟕

Page 4 of 4
Mechanical Power Engineering 4th year MPE
Mansoura
Department 1st semester
University
Faculty of Engineering Mid-Term 2020-2021

Course Title: Design of Mechanical


Total Marks 25
Power Engines No. of Pages: 3+Tables
Allowed Time 1.25 hours
Course Code: MPE4414
Name:…………………………………..……………………………………..Sec.( )
Assume reasonably any missing data – Give units of ALL deduced quantities

Question No. (1) : Choose the correct answer: (8 Marks)


1. The process at which the exhaust is pushed out the combustion chamber during the intake
process in a 2-stroke ICE is called
a) Exhaust stroke b) Exhaust recycling
c) Exhaust blowdown d) Scavenging
2. The under square engine results in .... friction losses compared with an over square engine with
similar bore
a) Lower b) Higher
c) Equal d) Unknown
3. A common example of external combustion engines is
a) Steam turbine b) Gas Turbine
c) SI engine d) Electric motor
4. Fiber reinforcement of aluminum alloys used for piston fabrication gives.... thermal and
mechanical load limits
a) Lower b) Higher
c) Equal d) Unknown
5. Advantages of fabricating conrods using casting manufacturing include
a) Low weight b) Low cost
c) High strength d) Good quality
6. Piston functions include
a) Sealing off the working chamber b) Actuating the intake and exhaust valves
c) Exchanging power with the Flywheel d) All choices
7. The crankshaft is required to have high modulus of rigidity in order to withstand
a) Normal stresses b) Torsion
c) Vibrations d) Variable load
8. Sintered conrods results in....compared with forged conrods which make sintered rods suitable
for modern engines.
a) Higher weight b) Higher velocity limit
c) Lower cost d) All choices

Page 1 of 3
Question No. (2) : (7 Marks)
3
A V4 2500 cm , 4-stroke diesel engine equipped with a two-stage turbocharging system (see figure
below) and operates at 4000 rpm and a volumetric efficiency of 140% with an air to fuel ratio of 21:1.
Assuming that the air density equals 1.2 kg/m3 and the specific heat at constant pressure is constant and
equals 1.2 kJ/kg.K, determine;
1. The power that both high-pressure and low-pressure turbochargers must produce
2. The temperature at the intercooler exit.
3. If the engine operates with a brake thermal efficiency of 34%, determine the engine power output
(Assuming that the combustion efficiency to be equal 96% and the lower heating value of used fuel
is 42.5 MJ/kg).

Page 2 of 3
Question No. (3) : (10 Marks)
It is required to design the piston and connecting rod of a 2.4L 4-stroke 4-cylinder SI engine. The engine
has a bore of 9 cm and connecting rod to crank offset ratio of 4. If the maximum allowable pressure
inside the combustion chamber is 6 MPa, find suitable dimensions for piston including its crown, barrel,
skirt, and its rings and pin. Give also proper dimensions of the conrod I-section and perform force
analysis to calculate the maximum stress upon the conrod at 3200 rpm when a right angle is created
1
between the conrod the crank arm. (Take the constant 𝛼 in Rankine-Gordon equation to be for steel
7500
conrod)

Best Wishes
Page 3 of 3 Dr. Waleed M. Shaaban
Dr. Mahmoud A. Shouman
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If there is a change crank angel from 30, it
is always rounded up in the subsequent
calculations to the larger number

inverse cos

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