Compression Moulding of Composite Tailboom Frames with Hybrid Fibre Architectures – Technology Demonstration

Continuous fibre (CF) aerospace preforms exhibiting excellent mechanical performance possess low formability characteristics and are confined to simple shell-like geometries with minimal curvatures, while incurring high-costs and long manufacturing times. On the other hand, long discontinuous fibre preforms such as randomly oriented strands (ROS) (bulk pre-impregnated finite sized chips of unidirectional or woven fabric material) […]

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Design, Analysis and Optimization of an Aircraft Seat

The certification of aircraft seats is a very costly process, and such the design of these seats is a detailed and time-consuming task. All new aircraft seat designs must go through rigorous physical testing to be certified as airworthy as per the Canadian Aviation Regulations (CARs). Because of this, many seats are overdesigned to avoid […]

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Buckling Analysis of Hybrid Composite-Metallic Stiffened Structures

In order to reduce the structural weight and operating cost of the aircraft, hybrid structures composed of composite skins and metallic sub-structures are commonly used as components of the wing and fuselage. The skin temperature change of the aircraft during takeoff and landing causes different amounts of deformation in composite and metallic materials due to […]

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An IoT Platform for Disaster Response

This project aims to develop a novel information-technology platform to improve the effectiveness of emergency response in disaster areas, ultimately saving lives. In case of any emergency response, the local communication infrastructure cannot be generally relied upon: therefore, we propose a distributed, self-organizing information system based on off-the-shelf mobile devices, supported by self-organizing, self-deploying UAVs. […]

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Cinema Sidewall – Aircraft Sidewall for Projection of Visual Content

With the rise in fuel prices, operators are constantly pushing aircraft manufacturers to find new ways to reduce their aircraft’s operating costs. One of the objectives of this project is to create a Bombardier toolkit for the C Series. This will allow the operators to input parameters such as the miss-rigging present on their control […]

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System Controller – Connector/Harness/Baseplate Redesign Feasibility Study

Electronic assemblies are used to control various systems in an aircraft. Under normal operating conditions, these assemblies undergo vibration, and therefore have an expected life span. Different designs are analyzed to reduce production cost, and these designs have to ensure that the electronic components contained within the hardware can tolerate the same operating conditions without […]

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Validation and calibration of Squeeze Film Damper Model with Experiment

This research project studies a specific component in the commercial aircraft engine called the squeezed film damper, or SFD. The SFD is applied to reduce the vibration of the engine rotor, which in turn reduces the noise and brings comfort to the passengers. The expected delivery from this project includes an advanced SFD model which […]

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Concept design and feasibility evaluation for the QEYSSat microsatellite mission

This project focuses on the concept design and ACS/Geolocation simulation of an Earth-observation microsatellite in Low Earth Orbit. MSCI has a long history of building microsatellites, but not for an Earth observation mission. In this research, we will evaluate the current MSCI multi-mission bus design capability, given its current hardware, for use in the QEYSSat […]

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Nonlinear Dynamic Analysis of Aero-Engines

Aero-engines are lightweight structures which are assembled of several thin walled cylindrical components (casings). Casings are joined by bolted flanges, and must withstand high forces. To accurately predict the response of casings assembly, the non-linear behavior of the casing joints must be considered. Currently, aero-engine manufacturers (i.e PWC) are facing serious limitations in matching the […]

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Feasibility Study of Switch Module Redesign

Structural and vibration analysis is performed on a proposed design change on electronic assembly to ensure that it meets customer requirements and is a more cost-effective design. Such design change should be cost efficient. The important aspect, in addition to the design, is interacting with different engineers at different positions in the company. Working with […]

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