Compact Powered Door Opener

Project number
17043
Organization
AGM Container Controls
Academic year
2017-2018
Project goal: To design and build a door operator concealed in the door frame of a wheelchair lift in compliance with applicable ANSI/BHMA standards. The doors on wheelchair lifts are not automatic and require wheelchair users to operate them manually. The team designed and built a door operator, concealed in the door frame of an Ascension Protégé wheelchair lift, in compliance with applicable standards of the American National Standards Institute and the Builders Hardware Manufacturers Association. The opener enables a person in a wheelchair, or someone without use of their arms, to control their own lift entry and exit. The design consists of a mechanical actuator to move the door and software to regulate speed and operating procedure. A mechanical override, activated by pushing on the door, accounts for emergencies and power outages. In the event of obstructions, the software resets the current operation or allows the obstruction to be removed if there are multiple failed attempts. The system is also designed to be compact and modular for easy maintenance and implementation in other lifts.

Hardware Environmental Protection for Autonomous Large Mining Trucks

Project number
17042
Organization
Caterpillar Inc.
Academic year
2017-2018
Project goal: To redesign an enclosure for the autonomous control hardware on the sponsor’s mining trucks. Primary requirements were to provide sufficient cooling, to control dust intrusion, to remain close to the existing enclosure’s footprint, and to extend the service interval to 500 hours. The primary challenges of the project were the extreme heat and dust conditions in which the trucks operate. Many of these vehicles are in use around the world, so a retrofit design was chosen to allow simple field deployment on active vehicles. Blown air cools the electronics in the enclosure, so the cooling profile and temperatures were optimized using temperature and flow modeling in MatLab. Dust intrusion is managed three ways. First, the blower creates positive pressure inside the enclosure, which prevents dust ingress through cracks or holes. Second, a standard automotive filter was chosen for its low profile and wide cylindrical shape to fit the size constraints of the project while maximizing surface area to provide the longest life. It was determined a higher level HEPA filter was not needed as the target air quality within the enclosure was ISO 9, or standard room air quality. Third, two cyclone prefilters were used to prevent the air filter from becoming saturated, allowing 500 hours of service before needing to be changed. The design is compact, protruding only one inch beyond the original cabinet’s footprint, and compatible with the sponsor’s vehicle lines.

Multifrequency Antenna Mast System for Large Mining Trucks

Project number
17041
Organization
Caterpillar Inc.
Academic year
2017-2018
Project goal: To design, build and test a multi-frequency antenna mast for large mining trucks. The sponsor needed to update its antenna mast configuration to better interface its large mining trucks with the data and communication arrays used in its international markets. Design requirements stressed safety, dependability and durability. 3-D modeling was used to limit obstruction of the truck operator’s field of view and to verify that the antennas could be lowered to a safe working height. Finite element analysis modeling was performed to ensure that the antenna mast system’s natural frequency would not couple with the truck’s vibration spectrum; if the frequencies were too close,the resulting resonance would destroy the mast system. Finite element analysis was also used to verify that the antenna could withstand forces of 3g. The antenna mast system is reinforced with a steel frame and fitted with a rack and pinion system that uses an electric motor to raise and lower the antenna. The system has an enclosed housing to cover moving parts and prevent damage by flying debris. The sponsor plans to attach up to five antennas to the mast system to improve communications and data accumulation.

Oil Spray Cooling on Rotating Machines

Project number
17040
Organization
Honeywell Aerospace
Academic year
2017-2018
Project goal: To design and build a simplified version of the end turn region of an oil-cooled high-power-density aerospace generator and test for the most effective cooling configuration. The test fixture had to be built at full scale, be flexible enough for multiple configurations, and have a way to determine how well it was being cooled. The oil circulation system of the test fixture allows for the manipulation and measurement of the oil pressure, temperature and flow rate. It provides a constant source of oil to the nozzles that apply the cooling oil to the test item. Effective cooling of the end turn region is critical for proper generator performance. Oil pressure, temperature and flow rate were tested, as were nozzle type, configuration and quantity.Cooling effectiveness was determined using an infrared camera mounted within the system. The most effective configuration was determined using a design of experiments model.

Rotating Connect/Disconnect Under Load

Project number
17039
Organization
Honeywell Aerospace
Academic year
2017-2018
Project goal: To develop a prototype mechanism to mechanically connect and disconnect a gas turbine auxiliary power unit from the load compressor on large commercial aircraft. A review of existing mechanisms indicated that some type of clutch system would be required, and trade studies led to the selection of a design based on a synchro-mesh blocker ring. The first generation of the rotating connect/disconnect was developed and tailored to the sponsor’s torque, centrifugal and thermal load requirements and dimensional constraints. The first-generation mechanism was then evaluated under worst-case scenarios using a combination of manual and finite element analysis. Design aspects that did not meet performance requirements were identified then iteratively modified and re-evaluated until all performance requirements were met. Through this process a final generation mechanism was created and a 3-D printed demonstrator unit produced.

Inline Swirl Particle Separator III

Project number
17038
Organization
Honeywell Aerospace
Academic year
2017-2018
Project goal: To optimize a device from a previous design team that reduces air contamination in engine bleed lines and compressed air ducts without significant loss of air velocity or pressure. Turbine engines, used primarily in aircraft, operate in many environments and are expected to perform nominally, but contamination due to harsh environments has always been a problem. The inline swirl particle separator uses swirl vanes and air flowing through compressed air lines to create a helical airflow that exerts centrifugal force on particles and moves them to the outer perimeter of the flow. At this point, a diffuser incorporated into the flow separates cleaner air from particle-laden air, which is ejected from the engine. Filter boxes located at this intersection capture any remaining dust. To optimize this process, the team determined effectiveness and efficiency by using varying pipe lengths,swirl vane rotations, and diffuser gaps.

Landing Gear Bearing Test Machine

Project number
17037
Organization
RBC Sargent Aerospace & Defense
Academic year
2017-2018
Project goal: To design, build and test a bearing test machine to determine bearing service life. Journal bearings used in aircraft landing gear absorb radial and axial loads during landing and takeoff. Being non-serviceable and costly to replace, the service life of the bearings must be predictable and adequate for their application. The test machine uses off-the-shelf and fabricated components to move a shaft linearly through a bearing while a radial load of 3,000 pounds is applied. The team used SolidWorks to design the fabricated parts, conducted finite element analysis and motion simulation tests, and followed design for manufacturability practices to produce geometric dimensioning and tolerancing drawings. The linear shaft induces wear of the polytetrafluoroethylene liner, which is measured using a linear variable differential transformer sensor capable of detecting 0.0001 inches of displacement. Signals from the sensors are sent through the data acquisition system and into LabVIEW, which displays and records data. If any information received from the sensors exceeds safety criteria, the machine shuts off and removes load from the test piece. By gathering data on the wear characteristics of bearings smaller than those used in aircraft, it is the sponsor’s goal to create a scalable benchmark that will help establish industry standards regarding bearing service life.

Smart Museum Display Cabinet

Project number
17036
Organization
GEOST
Academic year
2017-2018
Project goal: To create a modern museum display cabinet that improves the protection and display of valuable items.Museum cabinet technology has remained fairly stagnant since its origin. In addition to protecting valuables from wear, dust and theft, contemporary museum cabinets must also consider factors such as temperature and lighting.The smart cabinet design incorporates wireless communication to control and monitor cabinet parameters. Using an advanced thermal model, a temperature-based thermal control system was designed. High-quality illumination is provided by LEDs with a high color-rendering index. The systems also incorporate a purpose-built power supply and a wireless entry notification system. Using an embedded microcontroller in the cabinet itself, the user is able to wirelessly control protective-action temperature thresholds and individual shelf lighting levels through a graphical user interface. This graphical user interface also displays entry notifications to the user when a cabinet door is opened.

Automated Fuel and Fluid Management

Project number
17035
Organization
Caterpillar Inc.
Academic year
2017-2018
Project goal: To design, test and build an automated system to record fuel consumption at the sponsor’s Tucson Proving Ground, where equipment testing uses thousands of gallons of diesel per week. The system replaces the current manual method of data collection with a mobile application that uses a tablet to collect and store fueling data, which is then sent to a sponsor server. A fabricated bracket allows the Windows tablet to be transported safely during data acquisition, after which reports are merged and produced automatically, and checked for quality using a custom application developed using Python and Visual Basic for Applications. The script then produces a final report that goes to billing and a report that identifies quality issues.

Reactor Design for NASA Oxygen Recovery

Project number
17034
Organization
Honeywell Aerospace
Academic year
2017-2018
Project goal: To develop a methane pyrolysis reactor to increase oxygen recovery aboard the International Space Station.On the International Space Station,carbon dioxide and hydrogen are run through a Sabatier reactor that produces methane and water. An electrolysis reactor splits the water into oxygen and hydrogen, and the methane is vented overboard. The reactor will close the resource loop in the air revitalization systems and reduce the need for hydrogen resupply.The methane pyrolysis reactor designed for this project uses waste methane from the current system to increase percentage oxygen recovery. The reactor takes in methane gas and heats it by induction to over 1,000 degrees Celsius while using a vacuum pump to keep the pressure below 300 torr. This combination of high heat and low pressure facilitates pyrolysis, which splits methane molecules into their constituent atoms, carbon and hydrogen. The carbon adheres to a porous substrate designed by the sponsor, and the hydrogen continues through the oxygen recovery system, starting the cycle over again.

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