Book Report on "System"
Book Report 6 pages (1962 words) Sources: 4
[EXCERPT] . . . .
$4,600.00Re-GENERATION SYSTEM THAT INLUDE:
battery charging at non-powered flight.
$275.00
OPTIONS:
1. 53" folding carbon fiber propeller added with two-piece machined hub
$1,250.00
2. Direct drive and fixed composite 53" propeller, $370.00
3. Reduction drive AND Super quiet 62" carbon fiber propeller
$1,895.00
COMPLETE SYSTEM:
that includes ElectraFlyer trike, Stratus wing, and medium battery pack, with charger. (Electric Aircraft Corporation (2007).
$20,990.00
CGS Aviation
CGS Aviation is another important ultra-light aircraft company. Part of the company model is Hawk SLSA and Hawk ELSA. The costs of the aircraft are between $47,995.00 and $57,995.00 Plus Delivery. The appendices 2 and 3 deliver the picture of CGS Aviation ultra-light aircraft.
Basic Ultra-light Aircraft Standard Equipment is as follows:
3-Position wing flaps
Full dual controls.
Rough terrain wheels - 16" x 6.5" x 6."
Streamlined aluminum wing struts,
Streamlined landing gear fairings,
Anodized tubing,
Folding tail,
Dacron sailcloth covering,
Hydraulic Brakes
Electric Start
Instruments:
Altimeter
Airspeed Indicator
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Compass
Tach/Hourmeter
Dual EGT
Water Temperature Gauge;
Intercom
ELT
6. Select the Preferred Solution
The analysis of the project reveals that the farmer should order for ELECTRAFLYER TRIKE, ultra-light electric powered aircraft from Electric Aircraft Corporation because the system meets all the technical requirements of the stakeholders.
List of References
Andrade de Oliveira, P.H.I. (2005). Development of Light Aircraft Flight Test Equipment.
Society of Automotive Engineers, Inc.
Electric Aircraft Corporation (2007). "Electra Flyer Technical details." Archived from the original on 12 November 2013. Retrieved 12 November 2013.
Leonard, J. (1999). Systems Engineering Fundamentals: Supplementary Text. USA. DIANE Publishing.
Viola, N., Corpino, S., Fioriti, M., et al.(2011). Functional Analysis in the Systems Engineering: Methodology and Applications. USA. InTech.
Appendices
Appendix 1: ELECTRAFLYER TRIKE ( Electric Aircraft Corporation)
Appendix 2: Hawk SLSA & ELSA CGS Aviation
Appendix 3: Hawk SLSA & ELSA CGS Aviation
System Design Synthesis
Yes
Motor
18 HP,
90% efficient at cruise
Low RPM, high torque unit.
26 pounds.
Max Thrust
Direct Drive - 53" Prop,
140 lbs, combined with reduction drive 1800 RPM,
63" Prop 155 lbs.
Controller
Pulse Width Modulation having electronic speed control to enhance highest efficiency.
Battery Packs
Custom built lithium-ion polymer designed to be used for highest capacity per weight (power density),
High discharge rate cells to be used for full power takeoff and climb.
5.6kwh capacity
Battery weight 47 kg
Flight Duration
Minimum of one hour
Cruise speed
90 km/h
Weight:
Trike with motor, gauges and controller ?
85 lbs (39 kg)?
Battery pack (5.6kwh)?
78 lbs (35 kg)?
Stratus wing?
84 lbs (38 kg)?
Part 103 ultralight ?
247 lbs (112 kg)?
A. Electrically powered and rechargeable from 230v, 50Hz single phase power;
B. flight time of 1 hour minimum;
C. transportable by a… READ MORE
Quoted Instructions for "System" Assignment:
1/This is an individual assignment that requires you to undertake key aspects of a systems design, demonstrate a grasp of systems engineering principles, standards and methods, and produce a professional-style report. 2/Statement of Need Farmers in remote areas of Australia have expressed the desire to have an Electrically Powered Ultra-light Aircraft (EPUA) for, principally, finding stock and, secondly, to monitor the presence of feral animals on their properties The following general needs have been advised: A. Be electrically powered and rechargeable from 230v, 50Hz single phase power; B. Have a flight time of 1 hour minimum; C. Be transportable by a motor vehicle towed trailer with a tray not bigger than 2.4 metres long by 1.8 metres wide; D. Have an assembly time prior to flight of less than 15 minutes from the commencement of unloading from the trailer to being ready for takeoff; E. Have a disassembly time after flight of less than 15 minutes from the commencement of disassembly to being on the trailer and being ready to depart; F. All activities associated with preparation for flight, flying and post flight (including trailer loading) to be practical for a single person. The Task ***** Conceptual Design The deliverable will comprise a skeleton conceptual design review data package comprising at least the following activities: *****¢ A needs analysis based on the design brief, common knowledge of light aircraft and model aircraft, and your imagination that surfaces the stakeholders, system context, at least one design scenario and key stakeholder needs.
*****¢ A set of key requirements. *****¢ Technical performance measures derived from the above two sets of information. *****¢ A functional analysis and allocation for the EPUA system. *****¢ Synthesis and generation of two candidate system concepts. *****¢ A trade-off between the two candidate solutions to select the preferred concept. *****¢ A brief description of the final conceptual design and a discussion on how well you expect it to address the user needs. Points Looked for : Scope *****¢ A few lines on nature of the system being designed, its intended purpose, the scope of the task (ie the life cycle phase) and what constitutes a task completion, ie a complete and documented systems design concept. Needs *****¢ Good range of stakeholders *****¢ Key needs captured from the task statement *****¢ Scenario(s) and their use of these to surface additional needs and sizing factors that can identify requirements *****¢ A context diagram *****¢ A short list of uniquely identified (numbered) key needs Requirements *****¢ 20-30 reasonable key requirements spread across the template, about half of which should be functional. These should o Be correctly written o Reflect the needs identified above and be traceable to them o Cover all topics to some extent o Have a stated verification method for each requirement: test, analysis, inspection, demonstration, or third party certification *****¢ Consistency across the requirements (ie they are not directly contradictory) Functional Analysis *****¢ Key diagrams that show functional decomposition: o Functional Flow Block Diagram (or equivalent) o Functional Hierarchy Diagram *****¢ All functional requirements (and hence needs) are reflected in the functions identified
Diagrams, especially FFBD, should be consistent with the scenario *****¢ Principally looking for *****˜primary***** functions; evidence of supporting functions would impress *****¢ Similarly if there are many interacting functions the use of an N2 diagram would impress Synthesis *****¢ Use of a morphological table or other structured synthesis method to devise candidate solutions *****¢ Design options produced should be derived from the functions (and hence requirements) listed earlier *****¢ Design options (candidate solutions) should be named (ie *****Low-Cost Option*****, *****Fully-Electrical Option*****, *****Low-Risk Option***** and described in a sentence or two so that the differentiation is clear. Trade-off *****¢ Demonstrated understanding of quantitative methods selected (normally MVA) *****¢ Good choice of trade-off attributes (typically TPMs, selected requirements, or needs) *****¢ Appropriate value functions: o Looking for x0 = specification limit; x* = that value of x beyond which no additional stakeholder value is derived Description *****¢ Brief description of selected solution that indicate what the solution is and why it would be a convincing product and would attract investors or company R&D funds *****¢ A block diagram or picture that indicates what the solution entails. *****¢ Sense that solution satisfies a good proportion of user needs (and requirements) Overall *****¢ Overall coherence of report (design package) *****¢ No appearance of new functions or requirements in synthesis or trade-off stages *****¢ Presence of references to the source materials used to generate the lectures and to problem -specific standards and components.
How to Reference "System" Book Report in a Bibliography
“System.” A1-TermPaper.com, 2013, https://www.a1-termpaper.com/topics/essay/conceptual-design/2838717. Accessed 1 Jul 2024.
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