Team 8A

AeroDynamos

Favion Harvard & Rachel Kabala

Overview & Problem Statement

Problem Statement

Habitat for Aviation’s aircraft hangar is unable to support Cessna 150 and Cherokee 140 due to an infrastructure design which does not allow the planes to move back and forth. They need a way to allow for sideways movement of the planes, allowing for aircraft to be present within the students learning space.

Overview

Over the years, North A,erica will start having a shortage of between 12,000 to 18,000 of aviation maintenance technicians. This problem promoted an organization in Swanton, Vermont called Habitat for Aviation  who plan to promote the next generation of aviation maintenance technicians and avionics specialists by teaching youth trades that would allow them to gain experience in these backgrounds. The welcoming environment would be where youth can deeply immerse themselves in the modern technology of aviation, learn a plethora of physics concepts, and give students space to be around airplanes in the hangar connected to the building. 

Prototype

Prototype 1: Tire Trailer 



Prototype 2: Tire Elevator 


Downside: the wheel of an airplane has an inboard and outboard  rim. Too much motion, unnecessary mechanism


Prototype 3: Scissor Tire 

Testing and Feedback 

Weight Analysis: CESSNA 150 & CHEROKEE PA-28 140

  • Cessna 150 empty weight: 1,122 lb (509 kg)
  • CESSNA 150 FUEL CAPACITY AT MAX: 22.5 US gal (18.7 imp gal; 85 L)
  • CESSNA 150 EMPTY WEIGHT + FUEL CAPACITY: 
  • CONVERTING GALLONS TO POUNDS: 22.5 GALLONS = 187.7 LBS
  • CESSNA 150 FUEL CAPACITY WEIGHT IN IBS + CESSNA 150 EMPTY WEIGHT= 1,309.7 LBS
  • Cherokee 140 empty weight: 1,290 lbs
  • Cherokee 140 FUEL CAPACITY AT MAX: 
  • Cherokee 140 EMPTY WEIGHT + FUEL CAPACITY: 36 gallons 
  • CONVERTING GALLONS TO POUNDS:  GALLONS = 300IBS
  • CHEROKEE 140 FUEL CAPACITY WEIGHT IN IBS + CHEROKEE 140 EMPTY WEIGHT= 1,590

80/20  Aluminum T-Slot Framing

Net force:  FNet = Fa + F
Forces Present: Gravity, Friction, Normal Force, 
Applied Force = NET FORCE
(calculating the NET force that will be present when utilizing the dolly because comparing 80/20 to lumber and steel; Its light lightweight, strong, and made to endure both indoor and outdoor use, resisting rust and corrosion.)
Friction: 
  • Utilized Black 80/20 with black coating to avoid too much Friction 
Minimum Yield Strength in Pounds:
  • 80/20's 6105-T5* alloy yield strength of 35,000 psi compares to A36 carbon steel's yield strength of 36,000 psi.
  •  aluminum weights 1/3 as much as iron, steel, copper or brass. (BASICALLY 80/20 IS REALLY LIGHT!).

Additionally
  • 80/20 is comparable to lumber and steel yet lightweight, strong, and made to endure both indoor and outdoor use, resisting rust and corrosion.

Tire Width Test 

  • Wanted to make sure the wheel fits between the product.
    • Observed the wheel, and saw how movement of the wheel worked. 
    • Tested the best ways of gripping the wheel, making sure that it does not slip. 
    • Approximate Wheel diameter: 15 inches.

P = F/A

Weight Testing 

We tested the materials we used to see the capacity to how much weight they can withstand.
  • Able to determine that the material we were using were strong enough, but also not too heavy. 
  • Able to assemble them so that they can hold the weight of the airplane. 
  • Created ways of purchasing cheaper products that was durable.

FeedBack 

Specifications 

1 ~ Facilitates Plane Movement in All Directions


2 ~ Adaptability to Different Aircraft Models


3 ~ Ease of Use


4 ~ Sustainability 


5 ~ Feasibility 


6 ~ Cost Efficient 


7 ~ Safety


8 ~ Accessibility