Tuesday, September 16, 2014
Executive Summary of Research
Executive Summary of Research
My task for the WaterCopter project
is to design and craft a multicopter frame and lift system to be used in the
transportation and collection of water samples. In order to create a successful
product I must consider the materials used in the structure, the layout of the
structure, the arrangement of the motors and propellers, and the effect the
materials used in the structure will have on the samples the final product will
be taking.
Many materials are useful in
constructing a multicopter (see table 1). The overall goal of the materials is
to be light, durable, and strong. Cost is also a factor that must be taken into
consideration.
|
Material
|
Pros
|
Cons
|
|
Carbon Fiber
|
Lightweight, strong
|
Brittle, expensive, hard to
machine, hard to glue
|
|
Fiber Glass
|
Easier to machine and glue, less
expensive, less brittle
|
Slightly heavier, slightly less
strong
|
|
Aluminum
|
Easy to machine and construct,
cheap, readily available
|
Less strong, heavier, easily
warped, carries vibrations, blocks radio frequencies
|
|
Injection Molded Plastic
|
Zytel is very strong and light
|
Most other forms are cheap and
easily broken, less available, requires special machinery
|
|
Vacuum formed kydex
|
Very durable, great for water
resistant or water proof products
|
Requires special machinery
|
There are also many
options for the layout of the multicopter. Common types are the tri-branched,
quad-branched, and the single-copter (Advanced Multicopter Design).
One can attach one rotor to each branch, or
attach two adjacent rotors, stacked in a coaxial arrangement. A single rotor
arrangement is more efficient, however a coaxial arrangement is more stable
with smoother control and provides the most lift in the smallest area, and less
weight than an hexacopter or octocopter (Advanced Multicopter Design). Coaxial
layouts permit one motor loss, however they are more complex and thus less
reliable, heavier, and more costly.
Rotor size is dependent
on the intended lift capacity and clearance limit of the structure. Larger
rotors are more efficient but more prone to vibration and provide less stable
flight than smaller, faster rotors (Advanced Multicopter Design). Another very
important consideration for the materials used to construct the frame is the
effect it will have on the samples we take.
In summary, the materials must be
strong, light, and not release any harmful compounds into the water. The layout
must be capable of lifting the structure and the water sample. In order for the
WaterCopter to be successful, the materials, layout, and environmental impact
of the structure and lift system must be optimized.
Testing Procedures
Test Stage: Preliminary
State of Solution: On, stationary on
floor adjacent to table
Condition of Testing Stage:
Controlled environment, open area
Tools and Equipment Required: Table
Testing Procedures:
1. Activate
the rotors to ensure functionality
one foot off the ground for at least ten seconds
3. Raise
altitude to five feet off the ground
4. Steer
the vehicle to directly above the table
5. Slowly
lower the vehicle to approximately four inches off the table
6. Cut
power to the rotors
Test Type: Validation
Test Stage: Secondary
State of Solution: On, stationary on
floor outside of testing stage
Condition of Testing Stage: obstacle
course set around a small pool atleast three feet deep filled with water,
controlled environment
Tools and Equipment required:
obstacles for vehicle to maneuver, small pool, and large fan
Testing Procedures:
1. Pilot
vehicle through obstacle course
2. Return
vehicle to starting point and land
3. Repeat
step one with the large fan on and aimed at the course
4. Once
through the course, land the vehicle on the water
5. Complete
testing to analyze the water sampling mechanism
6. Repeat
step three in reverse
7. Land
the vehicle at the starting point
Specifications and Limitations
- Final Product must operate in varying weather conditions
- - Capabilities of electrical components
- - Power of motors
- - Stability of vehicle
- Control System must be remotely operated and have a large range and endurance
- - Battery life
- - Size and weight of product
- Structure and flight system must be small enough to maneuver dense environments
- - Amount of water needed for research
- - Lift capacity to size ratio
- Mechanisms must operate on battery power
- - Power required by mechanisms
- - Endurance of battery
- Structure and mechanisms must have easily replaceable or reparable parts
- - Complexity of structure and mechanisms
- Structure must be durable
- - Strength to weight ratio of materials
- - Simplicity of mechanisms
- Final product must leave minimal environmental impact
- - Sound pollution of motors
- Final Product must be able to land on water
- - Water resistance
- - Flotation
Design Brief
Develop and manufacture a remotely
operated vehicle to survey and take samples, causing minimal negative impact on
marine environments inaccessible or dangerous to the researchers and scientists
that control and utilize this vehicle periodically in locations of interest, in
order to research water quality.
Develop and manufacture a structure
and aerial lift system, used periodically throughout the year to maneuver
through dense environments and carry water samples from bodies of water for
scientists to analyze and record, to allow for less obtrusive research in
locations less accessible to humans.
Flight System
Develop and manufacture a structure
and aerial lift system, used periodically throughout the year to maneuver
through dense environments and carry water samples from bodies of water for
scientists to analyze and record, to allow for less obtrusive research in
locations less accessible to humans.Background Information
The Problem
The Customers
The
projected costumers of the product are research scientists, marine biologists
or chemists, ecologists, park employees, or any person interested in marine
research. These customers need samples to analyze in order to determine the
healthiness of an ecosystem. Our product will be capable of sampling water
remotely. These samples must be brought to a laboratory to be tested.

The Case
This
case must be addressed because contaminated data is a big problem in the
scientific world. Scientists want the purest data for accurate testing.
Improper data can cause fluctuations in results that require retesting and
waste money. These fluctuations in results can lead to larger errors later on
that build on the problem. In addition, most scientists have the best interests
of nature at heart, and providing a cost effective way to take pure samples
with minimal environmental impact addresses all of these issues.
The stakeholders of the project are those willing to
contribute their time and possibly money to our project in order to receive a
completed product that will benefit them in the future. These stakeholders
could be those in charge of research facilities, employees of those research
facilities, those in scientific disciplines, as well as those invested in our
project because of interest in our goal for the project.
The Mood
The
intended moods that we wish to show in our project are efficiency, reliability,
and durability. We want our quad-copter to be efficient in all of its methods
in order to become a realistic source of water collection. We want the
quad-copter to be reliable so that scientists in the field can feel confident
in the data they receive. Finally we would like to craft a durable product
capable of surviving the difficulties of water collection.

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