An engine inlet cover and a method for covering an engine inlet are provided. A method for covering an engine inlet includes providing a collapsible cover comprising a connection pin defining an axis; a frame including interconnected arms; and a web. Further, the method includes storing the collapsible cover in a stowed configuration in which the arms are aligned. Also, the method includes rotating the arms from the stowed configuration to an operating configuration in which the arms are radially spaced about the axis, enclosing the frame in the operating configuration with the web to define an interior volume, and placing the cover over the engine inlet.

A fueling mat includes a main body configured as a sheet. The main body includes an opening defined in the main body and a plurality of tabs. The opening defines an outer perimeter and the tabs extend inwardly from the outer perimeter. The tabs are configured to flex out of the opening. With this structure, the tabs can protect the region of a fuel port from damage, whether or paint or structural, during fueling and further can help cover the opened fuel port, at least fractionally, before a fuel nozzle is inserted.

A drone docking ports (DDP) mounted on a pole top in close proximity to an accident scene with an openable and closable enclosure, a docking plate having integrated battery wired or wireless recharging pads, and a control module (CM) is disclosed. The CM is adapted to autonomously control all functions of the DDP including actuation of the enclosure and relay of video, audio, and flight control information between the CM and a central monitoring center and/or emergency personnel. A drone with a top and bottom profile design allowing numerous drones to be stacked upon one another and store in the DDP. When the DDP enclosure is in an open position, a drone or stack of drones may initiate a flight from the DDP and to re-dock the drone or stack of drones when the flight is completed, the enclosure may be closed to protect the drone or stack of drones.

A cover for an opening on the exterior of an aircraft that contains a fire-resistant, high-temperature tolerant foam encased in a cover made of an aramid fabric. The cover is friction-fitted to the interior of the orifice. The cover can contain one or more durable rings embedded in the fire-resistant, high-temperature tolerant foam meant to protrude outward from the rest of the cover of the body to contact an interior of the orifice into which they are inserted holding the cover in place with friction instead of fasteners.

An unmanned aerial vehicle airport, an unmanned aerial vehicle system, a tour inspection system and an unmanned aerial vehicle cruise system. The unmanned aerial vehicle airport comprises a support base, a parking apron, a protective cover and a protective cover opening and closing driving device. The parking apron is installed on the top of the support base; the protective cover covers the top of the apron; the protective cover opening and closing driving device is installed between the support base and the protective cover, and the protective cover opening and closing driving device is configured to cause a bar linkage mechanism to drive the protective cover to switch between an open position and a closed position. The unmanned aerial vehicle airport is provided with the protective cover for the parking apron. If the protective cover is open, the unmanned aerial vehicle is parked on the parking apron, and takes off from the parking apron.

A device for the decontamination of materiel, notably an aircraft such as a military helicopter, using a nuclear, biological and/or chemical decontaminant. The device includes a protective cover that can be adapted to the shape of the materiel, able to form a fluid tight decontamination tunnel around the materiel; at least one decontamination module able to eliminate the contamination from the materiel arranged inside the tunnel formed by the protective cover; an air-blowing module able to be arranged at the entrance to the tunnel formed by the protective cover in order to dispatch air into the said tunnel; and a filtration module able to be positioned at the exit from the tunnel formed by the protective cover in order to destroy contaminated air vapours and/or to recover the decontaminant at the exit from the said tunnel.

A kiosk for use an unmanned aerial system (UAS) delivery system is disclosed. In one embodiment, the kiosk includes an enclosure comprising at least one vertical wall having a secured entrance therethrough to prevent unauthorized persons from entering the enclosure, wherein an external appearance of the enclosure corresponds to a location of the kiosk; a landing zone for an unmanned aerial vehicle (UAV) of the UAS located within the enclosure, the landing zone comprising infrastructure from which the UAV can take off and on which the UAV can land; sensors for detecting an environment of at least one of the kiosk and the enclosure; and a guidance system for providing signals to the UAV to guide the UAV into the enclosure and onto the landing zone.

The present invention is directed to a tool for handling pitot tube covers, which are configured in a general cylindrical shape. This tool includes a threaded post configured to receive an external extension. The bottom of the tool is constituted by two parallel support arms with a slot therebetween.

A protective tarpaulin for a propulsion engine of an aircraft is made of a material having an air permeability index that is sufficiently high to prevent the accumulation of moisture inside the engine or a nacelle surrounding the engine.

An unmanned aerial vehicle (UAV) storage and launch system, including: a UAV pod having an interior; and a telescoping UAV landing surface disposed in the interior of the UAV pod; where the telescoping UAV landing surface may translate up toward a top opening of the UAV pod, translate down into an interior of the UAV pod, or rotate relative to the UAV pod.