Single Cylinder Model Aircraft Engine Report

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PROJECT BRIEF You are provided with the design of a single cylinder model aircraft engine. The engine generates 50 Watts of power with a shaft speed of 11,500 rpm. The combined force (inertia and the force from combustion) generated at the crank pin is 360 N. You are tasked with undertaking the detailed design of the conceptual engine. Figure 1 The single cylinder model aircraft engine [supplied as an .stp file on Canvas for import to your chosen software] SUBMISSION DETAILS • The assignment will be submitted through Canvas. • Submission deadline is 3rd September 2021. • Any work submitted late will receive a penalty of 5% per working day. • If you are unclear about any aspect of electronic submission or submission in general, you should seek advice well in advance of the assignment deadline. • If you are unclear about any aspect of electronic submission or submission in general, you should seek advice well in advance of the assignment deadline. • The report should be word processed in Arial or Times New Roman, size 12, with a minimum line spacing of 1.5 times and written in English. This includes figure/table captions. The report has a maximum page limit of 18 pages (all sections). • Your report should have a cover page. The following is required in this specific order or 10% reduction in assignment mark will be applied. Module title, Department (of Mechanical Engineering), Group number, and ID number, Report title, Date of submission. • Appendices are not allowed. • Immediately following the cover page, a completed University of Birmingham Assessment and Student Template should be provided. • The quality of the presentation of the report will also be assessed so think carefully about the way you present your work to ensure the reader can follow each step. • The assignment should be completed individually. This means that each student should individually submit 1 report. • Additional advice on report writing is available through the University Academic Skills Centre. https://intranet.birmingham.ac.uk/as/libraryservices/library/skills/asc/index.aspx. ASSIGNMENT This is an individual assessment and not a group assessment. Maximum number of pages allowed: 16 pages, however you should attempt to use as few pages as possible. The assembly drawing does not count towards the page count. You are required to submit the following: 1. Executive summary (Max 250 words) on a single page. 2. Design report covering: a. An analysis of the crankshaft, to include Loads, stress states and minimum diameter calculations (Max 2 pages) b. 2. A critical of the design, with suggestions for improvement (Max 1 page) A general assembly drawing to BS 8888 of the engine (in third angle projection) containing: a. At least internal and external orthographic views, showing clearly all the main components, with sections as needed for detail and relative positions. b. Notes for layout and installation, service supply details, testing, relevant codes etc. so that a prospective buyer (an engineer) would have sufficient information to decide to order. c. Overall/ leading dimensions and engine weight. d. Parts list including component details – quantities, materials, and supply. e. Separate items identified with leader lines to balloons that include the item reference number linking to the parts list. The arrangement drawing should include a parts list containing materials specification and any treatments required. Where possible certain items (such as nuts and bolts) should be chosen from standard parts. 3. Manufacturing and materials report (Max 10 pages) a. Manufacturing i. Produce a single A4 page manufacturing flowchart for the crankshaft in the design given in file: Engine 001. Your flowchart should contain the following: 1. Images showing the component to be machined. 2. Evaluation of the component you have chosen from a machining point of view. 3. Step by step process images illustrating how you have produced the component. 4. Justification of any primary or secondary manufacturing processes. 5. At least two images of the CAM routine for the chosen component illustrating the machining strategy. Autodesk Fusion 360 (or equivalent) images should be used. If you do not have access to this software, then please contact Dr Hood in advance of the submission deadline. 6. Typical details for the tooling, fixturing, workpiece materials, typical machine tool, cutting tools, cutting parameters, etc. that you have used as well as typical cycle times. 7. Evaluation of the final machined component after the CAM simulation. 8. Any other information that you feel the reader needs to see to understand how the component you have selected is produced. ii. Create a process plan in the form of routing sheets with the operation list to achieve all technical requirements for the component. Include the machine tools and fixtures required to realise all operations in the process plan. iii. Provide a review of how the component will be integrated into the assembly process for the engine. iv. Provide a review of how the component design could be improved from a manufacturing point of view. b. Materials selection i. Critical analysis of materials. A systematic analysis should be carried out using CES EduPack for the component. ii. Life cycle analysis should be carried out using CES EduPack. This should include: 1. Eco-Audit of your chosen component to assess the environmental impact of different phases in the engine live-cycle (energy requirements and carbon emissions/footprint). 2. A “what-if” analysis that compares the eco-impact of two different materials and process choices on the energy footprint contribution of your chosen component. RECOMMENDED TEXTS • Swift KG, Booker JD, (2013) Manufacturing process selection handbook, ButterworthHeinemann • Ashby, M. (2011) Materials Selection in Mechanical Design (4th Edition), Elsevier • Scallan, P. (2003) Process Planning - The Design/Manufacture Interface, Elsevier • Kalpakjian, S. & Schmid S. (2007) Manufacturing processes for engineering materials (5th Edition) • Simmons, C H. and Maguire, D E. (2007). Manual of Engineering drawing to British and International Standards, Elsevier, ISBN: 0-7506-5120-2 • Budynas, R G and Nisbett, J K (2015). Shigley's Mechanical Engineering Design (Si), 10Ed, McGraw Hill, ISBN: 933922163X ADDITIONAL INFORMATION This information is offered to assist you in understanding what is required and should be read carefully. Drawings should be in third angle projection and contain a full parts list specifying bought-out as well as in-house (designed and manufactured) parts. Always draw and sketch in full size; by doing this you will better appreciate the various design problems as they emerge as well as showing the client exactly what they are getting. DETAILED LEARNING OUTCOMES 1. Understanding the technical requirements of a project brief, i.e. a. the operating cycle of a two-stroke engine b. the piston/cylinder porting requirements c. Awareness of the influence of stroke/bore ratios in engine design 2. Designing components to specific requirements, i.e. a. Appreciating the tolerances needed in small engine design b. Appreciating the cooling and lubrication requirements of small two-stroke engines c. Understanding the fuel oil mixtures required by two stroke engines d. Understanding a simple carburettor 3. Designing with consideration of the technology of manufacturing processes and material choice, i.e. a. Appreciating the choice of materials available and using this information to make good decisions regarding materials selection b. Appreciating the limitations of manufacturing processes and materials in achieving satisfactory product performance c. Assessing the environmental impact of different phases in the engine live-cycle (energy requirements and carbon emissions/footprint) 4. Presenting a case for a chosen design neatly and persuasively, including the use of British Standards 5. Interfacing design and manufacturing stages in product development with viable process planning decisions 6. Understanding the communication needed between engineers in delegating component design. 7. Analyse component designs from a manufacturing point of view. 8. Use CAM to develop preferred solution for the manufacture of components. 9. Develop a component from design to manufacture. 10. Produce a manufacturing flowchart detailing the techniques used that a reader can use and follow. 11. Understand the impact of design decisions on scale up production potential of products and manufacturing unit costs. 12. Conduct a critical analysis of existing product designs considering product life cycle considerations. 13. Design with consideration of manufacturing constraints and available materials, i.e. a. Appreciating the choice of materials available and using this information to make decisions regarding materials selection. b. Appreciating the limitations of manufacturing processes and materials in achieving satisfactory product performance. c. Assessing the environmental impact of different phases in the products’ lifecycle (energy requirements and carbon emissions/footprint). 14. Understand the communication needed between design and manufacturing engineers in product/component design, interfacing design and manufacturing stages in product development and process planning.
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Report for two stroke single cylinder
Two stroke single cylinder engine was provided for conceptual design. The findings were then
compiled in a report. Here is the outline of the report.

Executive Summary
Design Report
A. Crankshaft design
B. Material Used
C. Assembly Diagram
Design of 2 stroke cylinder
A. Cylinder
B. Cylinder Head
C. Piston
D. Piston Rings
E. Connecting Rods
F. Crankcase
G. Crankshaft
H. Fly Wheel Sparking Plugs
Machining component crankshaft
A. Details
1. Example
2. Example
B. Design
1. Example
2. Example

CAM for crankshaft
A. Details for tooling and machining
Material Used
References

Report for two stroke single cylinder

Page 2 of 2


Running head: THE SINGLE CYLINDER MODEL AIRCRAFT ENGINE

Report forsingle cylinder model aircraft engine
[Author Name(s), First M. Last, Omit Titles and Degrees]

Executive Summary
Single-cylinder machines are straightforward and small, and they often provide the most
performance within a certain range. If a cooling system is possible, cooling is easier than with
many chambers, which may result in weight savings. Construction of single-cylinder engines is
straightforward and cost-effective. An internal combustion engine's fundamental piston engine

1

THE SINGLE CYLINDER MODEL AIRCRAFT ENGINE

2

design is the single-cylinder engine. The development of the single-cylinder engine control unit
was the main objective of this study.
One piston movement is all it takes for the combustion phase to be finished in a 2-stroke engine.
A compression cycle is followed by a compressed fuel explosion. The new fuel entering the
cylinders on the return pushes the emissions out of the cylinder. Every rotation causes the
ignition coils to ignite. Two piston strokes are required to create one horsepower, which is how
these motors receive their moniker. Compared to 4-stroke engines, these cylinders offer a few
benefits. They typically weigh up to 50% less, are lighter, and provide greater torque at higher
RPMs. Two-stroke engines also have a more straightforward design, which makes them simpler
to maintain. When compared to 4-stroke motors, 2-stroke engines have the peculiar need that you
premix your gasoline and lubricant. Because cylinder pressure history directly affects output
power, combustion efficiency, and engine-out emissions, engine load research methodology is
the most efficient method for examining engine combustion behavior. To cover all the significant
components needed for a 2-stroke gas engine, we will be constructing a model using CAD. In the
following sections, we shall outline all of the report's findings.

Design Report
The reciprocating compressor engine's core is the crank train, which converts the pistons' linear
action into rotational motion, or conversely. Since the crank is exposed to several load cycles
throughout the course of its life span, the longevity of this part and fatigue efficiency must be
considered in the design phase. In the crankshaft business, the development and design of

THE SINGLE CYLINDER MODEL AIRCRAFT ENGINE

3

crankshafts have always been crucial to producing a product at a lower cost with the required
load capacity and lowest weight, in addition to other functional criteria. One of the most
important elements impacting an engine's performance is crankshaft movement. The crankshaft
is affected by torsional and lateral vibrations.
High forces generated by inertia and gas burning act on the crankshaft during operation. Two
other kinds of fluctuating loads, namely torsional load and bending load, are caused by the
pressure applied to the shaft. High bend and fatigue limits, as well as enhanced balance qualities,
are needed for crankshafts to function safely throughout the course of their service lives. The
crank is subjected to cyclic stress, and as a result, fatigue failure develops over time. The early
design stage itself has to take fatigue analysis into account. Shorter, light...


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