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.

A mobile calibration room may be used for calibrating one or more sensors used on unmanned aerial vehicles (UAVs). A system can include folding or collapsible walls to enable the system to be moved between a stowed position and a deployed position. In the deployed position, the system can comprise a calibration room including one or more 2D or 3D targets used to calibrate one or more sensors (e.g., cameras) on a UAV. The system can include a turntable to rotate the UAV about a first axis during calibration. The system can also include a cradle to rotate the UAV around, or translate the UAV along, a second axis. The turntable can include a frame to rotate the UAV around a third axis during calibration. The mobile calibration room can be coupled to a vehicle to enable the mobile calibration room to be moved between locations.

A lock-detecting system is configured to be installed in an aircraft to determine if a gust lock is emplaced on a flight control surface. The lock-detecting system includes at least one servo actuator and a computing device. The at least one servo actuator is associated with the flight control surface of the aircraft such that the servo actuator is configured to supply a force to a flight control surface when engaged. The computing device is configured to instruct the at least one servo actuator to actuate the flight control surface, acquire an indication that the flight control surface did not move in response to said actuation by the servo actuator, and alert a pilot to remove the gust lock from the flight control surface.

A system and a method for protecting a user from potentially falling unmanned aerial vehicle (UAV) or package or both are described herein. The system includes a base structure; and a roof structure attached to and extending from the base structure. The base structure is configured to support the roof structure. The roof structure is configured to support a weight of the UAV and package. The roof structure is configured to shield or protect a user from potentially falling UAV or package or both when the user is under the roof structure.

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.

An apparatus, system and method for covering an aircraft engine. The apparatus comprises front and rear spaced apart plates with an edge engaging portion therebetween and a connector for securing the apparatus to a body to be applied to the aircraft engine shroud. The system comprises a front cover sized to surround a front portion of the aircraft engine, at least one apparatus for covering an aircraft engine at least one hook comprising the apparatus adapted to engage a trailing edge of the shroud of the aircraft engine and a strap operably connected to each at least one hook and extending to the front cover. The method comprises locating the front cover over the front portion of the engine, securing at least one hook to trailing edge of the engine shroud and tightening a strap operably connected to the at least one hook and the front cover.

A device and a method for introducing a drone to an area of interest are presented. The delivery system may include a housing, a drone, either a timer or a receiver, a lock mechanism, and a biasing mechanism. The housing further includes a pair of parts with or without subparts. At least one sensor is attached to the drone. The timer or the receiver is secured to the housing and communicable with the lock mechanism to control function thereof. The lock mechanism is adapted to releasably secure the parts or the subparts. The drone is enclosed within the housing in a CLOSED configuration when the lock mechanism is locked. The biasing mechanism separates the parts or the subparts to an OPEN configuration when the lock mechanism is unlocked. The drone is introducible to the area of interest in the CLOSED configuration and separable from the housing in the OPEN configuration.

A protective cover for protecting aircraft engines is disclosed, the protective cover comprising a generally circular cross-section, a circumference, an outer side, and an inner side; said circumference being defined by a frame element having generally circular ring shape formed by a rod unit; said frame element comprising a plurality of attaching mechanisms being dispersed around said ring shaped frame, and being sized and configured to releasably attach said protective cover to an engine; said generally circular cross-section comprising one or more fabric layers contained in said ring shaped frame element. The protective cover is easily installed due to its attaching mechanisms and its breathable and durability protects the engine from damage.

A boom cover for covering a refueling boom, particularly a flying boom, of a refueling aircraft. The boom has a closure which has a shield sized to cover the open end of the refueling boom, to prevent intrusion of debris, animals, etc. The closure has a hoop for circumscribing the boom and drawing the shield taut for remaining on the boom and flaccid for attachment to and removal from the boom. The closure may be attached to and removed from the boom by a longitudinally rotatable handle which is manipulated by a ground operator. Optionally the handle may be removable from the closure for use on subsequent aircraft or storage.

Disclosed is a drone station which allows the center of resonance of a drone to be always accurately aligned regardless of the initial landing position of the drone. The disclosed drone station includes a landing guidance instrument and a wireless charging instrument which is formed on the landing guidance instrument and wirelessly transmits the power to a drone positioned thereon, the landing guidance instrument having an inclined surface which moves the landed drone onto the top of the wireless charging instrument.