Questions
According to metal additive manufacturing, what are the variables impact the two quality issues below, explain...

According to metal additive manufacturing, what are the variables impact the two quality issues below, explain in details how and why pressure, force, temperature and time affect them. a. surface finish. b. dimensional accuracy.

In: Mechanical Engineering

In no more than 300 words, describe the differences between a typical elastomeric engine mount and...

In no more than 300 words, describe the differences between a typical elastomeric engine mount and a typical hydramount. You should use diagrams, theory and mathematical models where appropriate to highlight the key differences and positives and negatives of both.

In: Mechanical Engineering

A model of an air ship is to be studied. The prototype is envisaged to be...

A model of an air ship is to be studied. The prototype is envisaged to be 8 m long with a diameter of 750 mm and the model is to be 300 mm long. What should the diameter of the model be? What should the diameter velocity in a wind tunnel be to simulate actual conditions? If the drag on the full model is found to be x N, what would the drag on the prototype be?

In: Mechanical Engineering

(Using Matlab)We are given data about a charity organization in table 1 Days 10 20 30...

(Using Matlab)We are given data about a charity organization in table 1 Days 10 20 30 40 50 60 70 80 90 100 Donation 23 45 60 82 111 140 167 198 200 220 Table 1: Donation collection by the charity organization Assume that x corresponds to the independent variable. Compute linear, quadratic and cubic fit for the data using regression techniques and plot them on three different graphs, all on the same figure. Use an appropriate small interval to create your plots. Mark the original data with green circles. Give appropriate titles and labels for the graph. Explain in few sentences which model best represents the data and why? Now, use the best model to find the value of the donation collection for 25th day. Print this value.

In: Mechanical Engineering

According to the metal additive manufacturing process identify and explain the reason behind the key processing...

According to the metal additive manufacturing process identify and explain the reason behind the key processing limits below. a.limits of the equipment used. b.limits of the material being processed.

In: Mechanical Engineering

A vehicle which is equipped with a 6 cylinder, 2000 cc spark ignition engine is cruising...

A vehicle which is equipped with a 6 cylinder, 2000 cc spark ignition engine is cruising at an average speed of 150 km/h from Ankara to Istanbul on the highway. The mass of the vehicle with single driver is 1200 kg and its projected frontal area is 3 m2. The coefficient of rolling resistance is 0.015 and the discharge coefficient is 0.3. The distance between Istanbul and Ankara is approximately 450 km. Assuming an average brake specific fuel consumption of 250 g/hp-h, calculate how many liters of fuel will be used during this journey ( r fuel = 0.73 g/cc and ambient air density r a=1.2 kg/m3).

In: Mechanical Engineering

A certain crude oil shows the following ultimate analysis: C=87.1% and H2=12.9%. The volumetric analysis of...

A certain crude oil shows the following ultimate analysis: C=87.1% and H2=12.9%. The volumetric analysis of the dry flue gas resulting from the combustion of this oil shows CO2=12%, O2=4.6%, CO=0%, and N2=83.4%

a. Theoretical Air-Fuel Ratio

b. Actual Air Fuel Ratio

c. Excess air in Percent

In: Mechanical Engineering

We have created angles features on parts (ie chamfers, tapers) two different ways. Describe the difference...

We have created angles features on parts (ie chamfers, tapers) two different ways. Describe the difference between the two methods

In: Mechanical Engineering

1- Abrasive wear is most common in situations in which: a. Hard particles are caught between...

1- Abrasive wear is most common in situations in which:


a. Hard particles are caught between two contact surfaces
b. the hardness of one material is much higher than the other
c. Neither A or B
d. Both A and B

2- What material property is critical to predicting wear behavior?


a. buckling resistance
b. tensile strength
c. modulus
d. hardness

3-What is the general cause of corrosion of low carbon steel?

a. Stray electric currents (very small)
b. Using two-dissimilar metals together
c. Being in the presence of moisture or water
d. All the above

In: Mechanical Engineering

Specify 6 best practices for controller loop tuning. Outline the details for each of these practices....

Specify 6 best practices for controller loop tuning. Outline the details for each of these practices. Provide details for each.

In: Mechanical Engineering

what is the heat treatment procces for the aircraft turbine blade ?with steps

what is the heat treatment procces for the aircraft turbine blade ?with steps

In: Mechanical Engineering

Give AT LEAST 5 METHODS of priming pumps.. Show their illustrations and describe how each methods...

Give AT LEAST 5 METHODS of priming pumps.. Show their illustrations and describe how each methods are used in priming pumps.

In: Mechanical Engineering

Over the last 50 years, the United States labor economy has changed from a manufacturing to...

Over the last 50 years, the United States labor economy has changed from a manufacturing to service and technology focus. Other than the obvious changes, such as fewer mine tragedies and more carpal tunnel syndrome, what other trends in employment safety do you predict, and what is your evidence for that prediction? How should companies respond? How would you respond? Why?

In: Mechanical Engineering

Question 1 a) A cylindrical feedstock of length = 35.4 cm and diameter = 10 cm...

Question 1

a) A cylindrical feedstock of length = 35.4 cm and diameter = 10 cm is subjected to turning using a high speed steel tool. For this tool, n and C values in the Taylor tool life equation are 0.125 and 70 m/min, respectively. The cost for hiring an operator and using the machine tool are $82 per hour. The tooling cost per edge of cutting is $5. Loading and unloading the part on to the machine takes about 4 min, and it takes about 2.5 minutes to change the tool. At a feed rate of 0.25 cm/rev, calculate:

(i) cutting speed for maximum production rate,

(ii) tool life [minutes], and

(iii) cost per unit and total cycle time of a produced part.

b) On a rectangular stock of aluminium alloy [tensile strength = 305 N/mm² and yield strength = 215 N/mm²] with dimensions of length = 320 mm and width = 30 mm, peripheral milling is performed on the top surface. The diameter of the carbide milling tool is 60 mm, with 8 teeth. The milling tool is centred along the workpiece width. At cutting speed of 80 m/min, chip load of 0.17 mm/tooth, and a depth of cut of 5 mm, calculate the following:

(i) the time to complete one machining one pass across the surface, and

(ii) the rate of maximum material removal during this cut.

Question 2

a) List and describe the five processes that cause wear at the interface of the tool and chip and the interface of tool and work in machining. What are the two major factors which enhance tool wear mechanisms? Explain in detail.

b) List and describe the three main processes that cause grinding wheel wear. Define Grinding Ratio and explain in detail, the relationship between grinding ratio, surface finish, and wheel speed using a plot.

Question 3

a) In an Electrochemical Machining process, the feedstock is made of an aluminium alloy (Ultimate Tensile Strength=572 MPa, Tensile Yield Strength=503 MPa). The desired time to machine a hole (?=10 mm) through a 20 mm-thick part is 2.1 min at a feed rate of 0.18 mm/s. What are:

(i) the efficiency of the process in %, and

(ii) the current requirement in amps to achieve this machining time target?

b) Describe in detail the process of circular sawing with the aid of a freehand sketch. What are the two major mechanisms by which circular sawing is achieved and what materials are commonly used as circular saws of each type?

In: Mechanical Engineering

Title: Titanium Alloy Database Table: Table 5b. Creep and Stress Rupture Properties of Titanium Alloys -...

Title: Titanium Alloy Database
Table: Table 5b. Creep and Stress Rupture Properties of Titanium Alloys - Stress for Creep Extension & Rupture (Metric Units)
alloy type common alloy name alloy alias ASTM grade UNS no. condition product form product thickness (mm) test temperature (°C) rupture time (s) stress to produce 0.1% strain (MPa) stress to produce 0.2% strain (MPa) stress to produce 0.5% strain (MPa) stress to produce 1.0% strain (MPa) stress to produce 2.0% strain (MPa) stress to produce 5.0% strain (MPa) rupture stress (MPa) notes source
Unalloyed & Modified Titanium Unalloyed Gr. 1 CP Grade 1 1 R50250 A NR NR 93 10000 193 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 1 CP Grade 1 1 R50250 A NR NR 150 10000 166 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 1 CP Grade 1 1 R50250 A NR NR 205 10000 145 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 1 CP Grade 1 1 R50250 A NR NR 260 10000 138 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 1 CP Grade 1 1 R50250 A NR NR 315 10000 124 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 2 CP Grade 2 2 R50400 A NR NR 93 10000 262 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 2 CP Grade 2 2 R50400 A NR NR 150 10000 228 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 2 CP Grade 2 2 R50400 A NR NR 205 10000 200 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 2 CP Grade 2 2 R50400 A NR NR 260 10000 179 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 2 CP Grade 2 2 R50400 A NR NR 315 10000 159 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 3 CP Grade 3 3 R50550 A NR NR 27 10 275 331 400 448 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 3 CP Grade 3 3 R50550 A NR NR 27 100 214 241 290 310 366 428 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 3 CP Grade 3 3 R50550 A NR NR 27 1000 221 234 317 400 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 3 CP Grade 3 3 R50550 A NR NR 425 10 34 55 69 90 117 138 152 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 3 CP Grade 3 3 R50550 A NR NR 425 100 28 34 48 55 69 83 110 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 3 CP Grade 3 3 R50550 A NR NR 425 1000 28 31 34 62 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 3 CP Grade 3 3 R50550 A NR NR 540 10 17 21 26 48 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 3 CP Grade 3 3 R50550 A NR NR 540 100 7 10 17 33 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 3 CP Grade 3 3 R50550 A NR NR 540 1000 7 19 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 4 CP Grade 4 4 R50700 A NR NR 25 10 366 393 428 490 531 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 4 CP Grade 4 4 R50700 A NR NR 25 100 338 345 366 428 497 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 4 CP Grade 4 4 R50700 A NR NR 25 1000 255 283 310 359 462 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 4 CP Grade 4 4 R50700 A NR NR 370 1 186 207 228 234 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 4 CP Grade 4 4 R50700 A NR NR 370 10 152 186 214 221 228 228 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 4 CP Grade 4 4 R50700 A NR NR 370 100 124 145 172 193 214 228 221 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 4 CP Grade 4 4 R50700 A NR NR 370 1000 97 110 124 138 159 179 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 4 CP Grade 4 4 R50700 A NR NR 425 1 117 138 172 207 221 221 221 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 4 CP Grade 4 4 R50700 A NR NR 425 10 69 90 124 145 159 179 193 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 4 CP Grade 4 4 R50700 A NR NR 425 100 62 55 76 90 97 117 138 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 4 CP Grade 4 4 R50700 A NR NR 425 1000 41 48 55 69 90 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 4 CP Grade 4 4 R50700 A NR NR 540 10 7 22 28 33 38 48 69 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 4 CP Grade 4 4 R50700 A NR NR 540 100 21 26 35 52 ASM
Unalloyed & Modified Titanium Unalloyed Gr. 4 CP Grade 4 4 R50700 A NR NR 540 1000 16 36 ASM
Unalloyed & Modified Titanium Ti-Ni-Mo CP Grade 12 12 R53400 A NR NR 250 1000 221 297 ASM
Alpha & Near-Alpha Ti-3Al-2.5V Ti Grade 9 9 R56320 A NR NR 250 1000 400 421 ASM
Alpha-Beta Ti-4Al-4Mo-2Sn Ti-550, IMI NR bar NR 400 10 607 621 917 ASM
Alpha-Beta Ti-4Al-4Mo-2Sn Ti-550, IMI NR bar NR 400 100 517 572 910 ASM
Alpha-Beta Ti-4Al-4Mo-2Sn Ti-550, IMI NR bar NR 400 1000 414 483 876 ASM
Alpha-Beta Ti-4Al-4Mo-2Sn Ti-550, IMI NR bar NR 450 10 359 428 835 ASM
Alpha-Beta Ti-4Al-4Mo-2Sn Ti-550, IMI NR bar NR 450 100 248 310 821 ASM
Alpha-Beta Ti-4Al-4Mo-2Sn Ti-550, IMI NR bar NR 450 1000 138 193 655 ASM
Alpha-Beta Ti-4Al-4Mo-2Sn Ti-550, IMI NR bar NR 500 10 172 662 ASM
Alpha-Beta Ti-4Al-4Mo-2Sn Ti-550, IMI NR bar NR 500 100 90 517 ASM
Alpha-Beta Ti-4Al-4Mo-2Sn Ti-550, IMI NR bar NR 500 1000 28 241 ASM
Alpha-Beta Ti-6Al-4V Titanium Grade 5; Ti-6-4 5 R56400 A NR NR 400 100 276 331 483 524 635 662 ASM
Alpha-Beta Ti-6Al-4V Titanium Grade 5; Ti-6-4 5 R56400 A NR NR 400 1000 407 455 579 614 ASM
Alpha-Beta Ti-6Al-4V Titanium Grade 5; Ti-6-4 5 R56400 A NR NR 455 10 262 317 393 441 559 600 ASM
Alpha-Beta Ti-6Al-4V Titanium Grade 5; Ti-6-4 5 R56400 A NR NR 455 100 124 172 255 303 414 483 ASM
Alpha-Beta Ti-6Al-4V Titanium Grade 5; Ti-6-4 5 R56400 A NR NR 455 1000 124 166 276 366 ASM
Alpha-Beta Ti-6Al-4V Titanium Grade 5; Ti-6-4 5 R56400 STA NR NR 400 10 462 524 586 621 662 703 ASM

From the data you have just downloaded, try to predict the stress at which Ti-11.5Mo-6Zr-4.5Sn will fail at if it needs to last for 750hrs at 370°C. (Yes, you might need to draw a graph).

Draw the graph and explain your answer

In: Mechanical Engineering