摘要:
An aircraft includes a central wing accommodating passengers and/or freight and two lateral wings that pivot on the central wing about respective axes of rotation. The various wings obey the following geometric characteristics: 0.3×Long 1.4×Long, wherein Larg being the distance between the two axes, Long being the length of the central wing, Haut being the height of the central wing, Env being the wingspan of the aircraft. The axes of rotation are inclined by an angle relative to the vertical axis of the aircraft such that the lateral pivot from rear to front and vice versa so as to come closer to, or deploy on either side from, the fuselage.
摘要:
An image capturing system for shape measurement includes: an image capturing device configured to capture an image of a structure; an air vehicle; an on-board control device configured to control the image capturing device and the air vehicle in accordance with an image capturing scenario; and a remote control device configured to create an image capturing scenario and transfer the created image capturing scenario to the on-board control device. The air vehicle autonomously flies to image capturing points sequentially so as to capture images. The captured data is transmitted to the remote control device via a wireless LAN.
摘要:
A package delivery system can be implemented to forcefully propel a package from an unmanned aerial vehicle (UAV), while the UAV is in motion. The UAV can apply a force onto the package that alters its descent trajectory from a parabolic path to a vertical descent path. The package delivery system can apply the force onto the package in a number of different ways. For example, pneumatic actuators, electromagnets, spring coils, and parachutes can generate the force that establishes the vertical descent path of the package. Further, the package delivery system can also monitor the package during its vertical descent. The package can be equipped with one or more control surfaces. Instructions can be transmitted from the UAV via an RF module that cause the one or more controls surfaces to alter the vertical descent path of the package to avoid obstructions or to regain a stable orientation.
摘要:
A system for rapid separation of a flight data recorder from an aircraft comprises a flight data recorder; an emergency detection system comprising a plurality of sensors for detecting flight parameters and at least one computer processor for analyzing the flight parameters and determining, based on the analysis, that an emergency event is occurring; a rapid ejection system comprising a pneumatic system configured to eject the flight data recorder out of an opening in a housing and through the skin of the aircraft when the emergency detection system determines that the emergency event is occurring; and a soft landing system, said soft landing system being attached to the flight data recorder and configured to reduce force of impact upon landing and increase buoyancy of the flight data recorder.
摘要:
A method for deploying a payload into a body of water using a deployment vessel, the deployment vessel including a hull defining a payload compartment, the method including positioning the payload in the payload compartment of the deployment vessel, the deployment vessel and the payload having a buoyancy, wherein the buoyancy is initially negative, deploying the deployment vessel into the water at a drop zone, wherein the deployment vessel moves horizontally through the water as it submerges vertically downward under a force of gravity, changing the buoyancy to positive after a minimum horizontal distance is established between the drop zone and the deployment vessel, thereby causing the deployment vessel to surface and, after the surfacing of the deployment vessel, opening the hull to release the payload therefrom.
摘要:
A drop zone marker includes a parachute, a first light module connected to the parachute by a first length of cord and a second light module connected to the first light module by a second length of the cord. A ballast is connected to the second light module by a third length of the cord is provided for pulling downwardly the drop zone marker. The parachute is configured to include an integral packing/deployment bag within which all components of the drop zone marker are contained up until deployment.
摘要:
A package delivery system can be implemented to forcefully propel a package from an unmanned aerial vehicle (UAV), while the UAV is in motion. The UAV can apply a force onto the package that alters its descent trajectory from a parabolic path to a vertical descent path. The package delivery system can apply the force onto the package in a number of different ways. For example, pneumatic actuators, electromagnets, spring coils, and parachutes can generate the force that establishes the vertical descent path of the package. Further, the package delivery system can also monitor the package during its vertical descent. The package can be equipped with one or more control surfaces. Instructions can be transmitted from the UAV via an RF module that cause the one or more controls surfaces to alter the vertical descent path of the package to avoid obstructions or to regain a stable orientation.
摘要:
An aerial delivery system includes at least one container mounted on a platform, an impact attenuator initially interposed between the container and the platform, an activation tether arranged to cause contents of the container to disperse, and rigging material attached to the impact attenuator, the platform and the activation tether and configured to rotate the platform to face upward and the impact attenuator to face downward during aerial delivery.
摘要:
An aircraft including a fuselage having an outer face on which is fixed a second interface, at least one emergency beacon including a base having a first interface to cooperate with the second interface for fixing of the base onto the outer face, and a casing housing a control unit, a radio transmitter for transmitting a distress radio signal and detector to detect abnormal aircraft behavior, and fixing structure to take up a fixation position to ensure fixing of the casing onto the base or a separation position, in which it does not ensure fixing of the casing onto the base, the transition from the fixation position to the separation position being ordered by the control unit when the detector detect an abnormal behavior.
摘要:
A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.