Abstract: The present invention is a system for treating effluent from robotic equipment used to remove marine biofouling, primarily targeting organisms such as orange cup coral, which collect on hulls of floating units for transporting oil and derivatives thereof, or on production and exploration platforms. The system involves separating the flow into two elemental phases: solid and liquid. In the solid-phase flow, treatment is carried out in steps essentially comprising particle-size reduction, direct oxidation, oxidation residence, separation, drying, temporary hermetic storage, packaging, and automatic transportation for final storage. The liquid phase includes a step of centrifuging, adsorption, inerting, and discharge of treated effluent into the sea in accordance with environmental law. The entire system is automated to minimize manual actions and interventions, and is programmed to run without interruption as a function of the flowrate of raw effluent.

Abstract: An environmental control system for an aircraft includes a first conduit, a second conduit, and a connector assembly. The connector assembly is coupled to the first conduit and the second conduit for controlling a flow of air. The connector assembly includes a connector, a connector ring, and an orifice plate. The connector includes at least one wall including a ridge defining a receptacle and a connector slot defined within the ridge. The connector ring is attached to the connector and defines a connector ring slot and a covering portion. The connector ring slot aligns with the connector slot and the orifice plate is inserted into through the connector ring slot and the connector slot into the receptacle during installation of the orifice plate. The covering portion covers the connector slot and retains the orifice plate within the receptacle during operation of the environmental control system.

Abstract: A method of retrofitting an environmental control system of an aircraft includes inserting the orifice plate through the connector slot and the connector ring slot into the receptacle. The method also includes aligning the covering portion with the connector slot.

Abstract: A method of retrofitting an environmental control system of an aircraft includes inserting the orifice plate through the connector slot and the connector ring slot into the receptacle. The method also includes aligning the covering portion with the connector slot.

Abstract: An environmental control system for an aircraft includes a first conduit, a second conduit, and a connector assembly. The connector assembly is coupled to the first conduit and the second conduit for controlling a flow of air. The connector assembly includes a connector, a connector ring, and an orifice plate. The connector includes at least one wall including a ridge defining a receptacle and a connector slot defined within the ridge. The connector ring is attached to the connector and defines a connector ring slot and a covering portion. The connector ring slot aligns with the connector slot and the orifice plate is inserted into through the connector ring slot and the connector slot into the receptacle during installation of the orifice plate. The covering portion covers the connector slot and retains the orifice plate within the receptacle during operation of the environmental control system.

Abstract: A display assembly is adapted to be received by a vehicle console and includes a chassis, a display member, a hood, and a mechanical positioning mechanism. The mechanical positioning mechanism can be easily activated to adjust the display member between a hidden or closed position and a visible or open position. In one embodiment, the display assembly has a latch mechanism to maintain the display member in the hidden position.