361 results about "Hangar" patented technology

The present invention relates to a collision avoidance warning system for an aircraft (1). The system comprises a light source (8, 9), sensors (10, 11, 12) mounted on the aircraft (1) and processing means for determining the dimensions and location of an object (15) relative to the aircraft (1) so as to determine whether a collision alert is to be given. The present invention is particularly suited to providing collision alert warnings on the ground, such as when the aircraft (1) is taxiing and manoeuvring on runways and in aircraft hangars.

The invention discloses an energy-dissipating hangar tunnel and an energy-dissipating supporting base thereof. The energy-dissipating supporting base comprises a spring guide rod, wherein the spring guide rod is sleeved in the spring; a protective shed is supported by the upper end of the spring guide rod; the lower end of the spring guide rod passes through a load-transferring steel plate; the upper end of the spring is fixed on the bottom surface of a load-transferring bracket; the lower end of the spring is supported on the load-transferring bracket; and the load-transferring steel plate is fixed on a support. The energy-dissipating hangar tunnel and the energy-dissipating supporting base thereof have the innovative points that: the energy-dissipating supporting base is simple in structure, low in cost, light in weight, high in rigidity and high in buffer capacity when impacted violently; and the energy-dissipating supporting base is suitable for performing energy dissipation on facilities easily subjected to violent impact, such as the hangar tunnel and the like.

An asymmetric aircraft (1) and an aircraft (1) that can operate from small ships (8) and be stored in high density with three aircraft or more in one helicopter hangar (107) without needing a landing gear or wing fold. These aircraft slide into and out of the hangar on dollies (90) like circuit boards in a computer and are launched and recovered using a large towed parafoil (6).

An inexpensive promotional hangar used to attach a neck or wrist strap to a desired item. The promotional hanger includes an elongated body made of a material divided into three sections. The first section extends from one end to approximately the mid-line axis of the body. A second section is formed adjacent to the first section that, during assembly, is folded upward to form an extending narrow tab. Located adjacent to the second section and opposite the first section is a third section. First and second fold lines are aligned transversely on the body, separating the first and second sections, and the second and third sections, respectively, and enabling the second section 30 to bend upward. A third fold line is transversely aligned over the second section, thereby enabling it to be folded in half to form a tab structure. An adhesive is spread over the entire back surface of the body, enabling the second section to be folded together to form the tab, and enabling the first and third sections to be attached to an item. Holes are manufactured in the second section to which a strap may be attached. A removable, protective sheet is then placed over the outer surface of the adhesive.

The invention discloses hangar equipment for unmanned aerial vehicles. The hangar equipment comprises an unmanned aerial vehicle storage structure, an automatic battery replacing structure, and an unmanned aerial vehicle takeoff and landing platform, wherein the unmanned aerial vehicle storage structure comprises an unmanned aerial vehicle parking garage and a lifting mechanism, the lifting mechanism is used for storing the unmanned aerial vehicles in the unmanned aerial vehicle parking garage and taking the unmanned aerial vehicles out of the unmanned aerial vehicle parking garage; the automatic battery replacing structure comprises a battery rack and a battery conveying mechanism arranged on one side of the battery rack, and the battery conveying mechanism is used for replacing batteriesfor the unmanned aerial vehicles on the lifting mechanism and conveying the batteries to corresponding charging bases of the battery rack; and the unmanned aerial vehicle takeoff and landing platformis used for takeoff and landing of the unmanned aerial vehicles. The unmanned aerial vehicle storage structure automatically stores the unmanned aerial vehicles in the unmanned aerial vehicle parkinggarage and takes the unmanned aerial vehicles out of the unmanned aerial vehicle parking garage, and the automatic battery replacing structure automatically replaces the batteries for the unmanned aerial vehicles and conveys the batteries to the corresponding charging bases of the battery rack for charging, so that the hangar equipment for the unmanned aerial vehicles has the functions of automatic parking, automatic battery replacement and automatic charging at the same time, and the use efficiency of a hangar for the unmanned aerial vehicles is greatly improved.

A hangar bar for a cathode plate and a method of producing a cathode for electrolytic recovery of metal. The hanger bar comprises a support element which is preferably stainless steel and hollow. An electrically conductive metal cladding is affixed the stainless steel bar by any appropriate mechanism, eg interference fit, welding, chemical or mechanical fastening or coextrusion or roll forming. Affixing the cladding to the stainless steel support element has significant advantages over conventional electroplating techniques including that a more precise engineering specification can be applied to the cladding thickness. This is important to maintain vertical alignment of the cathode plate in the electrolytic cell.

The invention discloses a distributed unmanned aerial vehicle charging machine hangar which comprises a machine hangar protection box body, a parking apron, a wireless charging module, a single chip microcomputer, a solar cell panel with a slidable cover, a storage battery pack and a GPS/Beidou positioning communication module, wherein the single chip microcomputer, the solar cell panel and the storage battery pack form a primary charging system, solar energy is stored in storage batteries by utilizing the solar cell panel, the wireless charging module and the storage battery pack form a secondary charging system, electric energy of the storage battery pack is charged to an unmanned aerial vehicle in an electricity shortage state, the single chip microcomputer controls the state of the slidable cover of the solar cell panel and closes the solar cell panel to protect the unmanned aerial vehicle or opens the solar cell panel for berthing or taking off of the unmanned aerial vehicle. Therefore, the hangar has the functions of berthing, protection, charging, positioning communication and the like of the unmanned aerial vehicle. Due to the fact that the solar cell panel is arranged, the hangar can be arranged in a field in a distributed mode and can accommodate several unmanned aerial vehicles. The distributed unmanned aerial vehicle charging machine hangar has the advantages of being free of maintenance, long in service, usable in an offline mode and the like.

Disclosed is a compressible sound attenuation core, having one or more flexible, inflatable chambers, having one or more internal sound baffles. The chamber(s) can have at least one sound attenuation material affixed to a first pre-dominant surface of the inflatable chamber(s). The sound attenuation core can be further framed by a novel extruded frame system that provides, inter-connectivity, support and integrity to form portable, modular sound attenuation panels that can be used to construct a variety of soundproofing devices, including but not limited to, partitions, walls, enclosures, structures, offices, aircraft hangars, and booths.

Disclosed is a lightweight modular structure that can be transported to the surface of an extraterrestrial mass in one rocket payload, and assembled rapidly by two robots. The structure is airtight, thermally insulated, resistant to micro-meteoroid penetration, includes an airlock, provides radiation shielding, and is capable of being pressurized and equipped with life support systems. The structure is designed to bear the exterior load of being buried under one to two meters of extraterrestrial material on extraterrestrial masses with gravity up to 40% of Earth's gravity, a configuration that can provide additional thermal insulation, additional radiation protection, and additional protection against micrometeoroid penetration. The structure can be assembled in different configurations, and may include one or more windows, and hangar-style doors at one or both ends to accommodate passage of large items. A plurality of these modular structures can be connected to each other utilizing an optional modular walkway. The structure can be used on extraterrestrial masses and on Earth for habitation, as a laboratory, as a greenhouse, and as a maintenance facility; it can be used on an extraterrestrial mass as a very large airlock, and it can be used on Earth as a biological/chemical warfare, or hazmat operations center or laboratory.

A pipe hangar that can be mounted in various orientations for adjustably securing or hanging a structure at different locations can include a housing having an adjusting strip, a locking tab, and multiple and differently oriented fastener structures, e.g., voids. The locking tab can include a strip guide and a lever including a tooth stop. The adjusting strip can include connecting teeth and be disposed on a bottom portion of the housing. The adjusting strip is adapted to be looped back over itself and placed between the strip guide and the housing such that the connecting teeth on the adjusting strip can be engaged by the tooth stop on the lever to lock the adjusting strip relative to the housing. A pipe or other structure disposed in the portion of the adjusting strip that is looped back over itself can be raised or lowered relative to the housing (and the structure to which the housing is mounted) by pressing the lever to release the adjusting strip connecting teeth from the tooth stop, moving the adjusting strip to a desired positioned relative to the housing, and releasing the lever to engage the tooth stop with the connecting teeth and lock the adjusting strip relative to the housing at the desired position.

The invention relates to a vehicle-mounted unmanned aerial vehicle parking hangar which comprises a pair of vehicle inner guide rails arranged in a carriage, a vehicle-parking charging platform installed on the vehicle inner guide rails, a hangar push-out mechanism fixedly connected with a stand column assembly and used for pushing the vehicle-parking charging platform to move along the vehicle inner guide rails, and a lifting platform arranged on the stand column assembly. Compared with the prior art, landing unmanned aerial vehicles can be pushed into a parking position in a vehicle body after being centered and then can be charged, the unmanned aerial vehicles can be pushed out to the lifting platform when the unmanned aerial vehicles need to take off from the vehicle body, the parkinghangar adopts a unit structure in design and comprises the vehicle-parking charging platform and the lifting platform, and the parking hangar can be flexibly assembled according to the number of actually-parked unmanned aerial vehicles.

A multilevel vertical general aviation hangar, comprising a traffic inflow/outflow path and a pallet stack subsystem. There is also a pallet turntable located with the path. A pallet shuttle moves the pallet and contained vehicle from the turntable to a lift. The lift moves the pallet and vehicle to a predetermined location within a storage structure.

A ground handling system for an airship which comprises a first track system to allow a plurality of docking carts to move from a hangar to a weathervane/launching/landing ring R. The docking carts are configured to complete a second track system. Carried by each of the docking carts is a mooring cart that carries a mooring structure. Upon the completion of the second track system by each of the docking carts, the mooring carts are able to move about the second track system. Thereby allowing the airship to be oriented in a desired manner to facilitate its launch or landing.

The invention discloses an automatic charging unmanned aerial vehicle hangar which comprises a time controller, a microprocessor and a solar charging module; the time controller transmits set time information to the microprocessor; the microprocessor controls opening and closing of a vehicle hangar door according to set time; when the vehicle hangar door is opened, the microprocessor controls an extension apron to stretch out of the vehicle hangar and an unmanned aerial vehicle parking on the extension apron is released for flight; and when the unmanned aerial vehicle falls onto extension apron, the pressure sensor receives pressure after the unmanned aerial vehicle falls and transmits a detected signal to the microprocessor, the microprocessor controls the extension apron to retract, and simultaneously controls the vehicle hangar door to be closed, and the unmanned aerial vehicle entering the vehicle hangar is charged through the solar charging module. The automatic charging unmanned aerial vehicle hangar is simple in structure, and has the reliability, the operability and the stability, and the situation that when the unmanned aerial vehicle finishing surveying and falls onto the vehicle hangar, the unmanned aerial vehicle can be automatically charged is ensured.

A conveyance storage apparatus includes an annular turntable having an outer circumference and a central opening defining a support surface therebetween for supporting a plurality of conveyances, particularly aircraft, on parking spaces thereon. The turntable is supported on a foundation, and a rotation assembly is positioned between the turntable and the foundation for permitting rotation of the turntable on the foundation between storage and enter/exit positions. A stationary core is positioned within the central opening of the turntable and the turntable is mounted for rotation around the stationary core. The turntable can be positioned within an enclosure having an opening sized to permit only a single conveyance to enter or exit the enclosure at a time. The rotation assembly is electronically programmable to respond to a predetermined access code by moving a predetermined parking space to a conveyance entrance/exit position in relation to the enclosure opening.

The invention discloses a traffic accident emergency rescue monitoring system and method based on a flight vehicle network.A dispatching system selects and assigns nearest flight vehicles to depart to the sky according to GPS positions of accident occurrence places; videos and images of the GPS positions are shot through cameras and are sent to the dispatching system, medical first-aid packets are delivered, voice broadcasting is performed, and the scene videos and images are processed and sent to an accident rescue monitoring center; the flight vehicles return to hangars after working.The system comprises the hangars arranged in a city in a network-shaped spaced mode and the dispatching system, wherein at least one flight vehicle is loaded in each hangar, and the dispatching system sends hangar opening signals to the hangars and sends flight signal, shooting control signals, broadcast control signals and release control signals to the flight vehicles.A flight control technology, an aerial photography and a network communication technology are ingeniously integrated, emergency rescue monitoring is achieved, and rapid, convenient and effective rescue works which cannot be provided by manmade rescues are provided.

A novel airplane shelter provides a plurality of arched vertical support members arranged axially along a line corresponding to the fuselage of an airplane to be sheltered. A cantilever beam is attached to the apex of each arched vertical support member, forming a “spine” along the top of the aligned arched support members. The cantilever beam is attached at one end to the rearwardmost arched support member, and the opposite end extends forwardly past the forwardmost arched support member to a point corresponding to the forwardmost point of an airplane to be sheltered. Separate lateral support members are placed at points corresponding to the wingtips of the airplane. The result is an open frame that defines a volume capable of enclosing an airplane. A covering material is placed over the open frame and stretched taut or otherwise secured over the entire structure.

A portable launch rig (PLR) may include a support structure including two side supports defining an interior space for lifting and filling a balloon envelope of a balloon. Wheels on each of the side supports enable the PLR to be moved in various directions in order to prepare the PLR for launching the balloon. The side supports are connected by a lateral support beam having a pair of cranes arranged thereon. Each crane has an arm arranged over the interior space that is connected to a spreader beam. The spreader beam includes a lift assembly configured to lift and inflate the balloon envelope within the interior space. The PLR includes a platform and perch for supporting and moving the balloon envelope. A door assembly of the PLR includes a plurality of hangar doors configured to block wind from a respective direction of each hangar door entering the interior space.

The invention belongs to the technical field of intelligent mechanical equipment, and particularly relates to an intelligent unmanned aerial vehicle hangar based on an automatic battery replacing device. The intelligent unmanned aerial vehicle hangar comprises a hangar cabin body, a parking apron and the rotatable automatic battery replacing device, wherein a two-degree-of-freedom mobile device ismounted on a hangar cabin door, and the two-degree-of-freedom mobile device can enable a telescopic electromagnetic adsorption device to move in a plane; the parking apron is a split type telescopicparking apron, and can move back and forth through a parking apron translation rod; and the rotatable automatic battery replacing device is installed at the bottom of the cabin body, the main shaft ofthe automatic battery replacing device can move up and down and rotate, and a laser positioning device and an image recognition device are arranged at the top of the main shaft so that batteries canbe autonomously and efficiently replaced through the cooperation of an airborne battery box.

The invention discloses an invisible aircraft carrier with high combat power and survivability. The invisible aircraft carrier is characterized in that: firstly, width of a flight deck is greatly reduced, the flight deck and the aircraft carrier body below the deck are changed to be more regularly strip-shaped, the surrounding outer surface of the aircraft carrier body is made into a structure that large areas of outward bent and inward bent planes are crossed, and an invisible material is additionally adhered to the outer surface of the aircraft carrier body or an invisible coating is additionally coated on the outer surface of the aircraft carrier body; secondly, an aircraft hangar with width of 40m and length of 200-300m is made on the lower part of the flight deck; or a vertical two-layer aircraft hangar is made below the aircraft carrier surface of a middle rear part so as to greatly increase the number of aircrafts carried by the aircraft hangar; thirdly, 4-5 flight flying and receiving hatchways are formed on the tail part of the flight deck and on two side edges or in the center of the aircraft carrier surface of the middle front part, and the aircraft carrier surfaces on the front parts of the four aircraft flying and receiving hatchways on the side edge of the flight deck are provided with catapults, or the forefront part of the aircraft carrier body is provided with a flying deck; and fourthly, the upper part of the flight deck on the aircraft carrier surface for landing and receiving aircrafts is provided with four or more arrester wires, and the aircraft carrier surface on the ahead part is provided with a barrier net. Thus, the aircraft carrier with high combat power and high invisibility can be made.

The invention relates to a safe and fast recovery and releasing system and method of an offshore operation helicopter. The safe and fast recovery and releasing system of the offshore operation helicopter comprises a hydraulic power system, a rapid mooring system and a pre-arranged track to realize a landing function, a feeler lever capturing function, a rapid mooring function, a function of pulling the helicopter into a hangar, a function of pulling the helicopter out of the hangar, a pulling straightening function and an unlocking and releasing function. According to the safe and fast recovery and releasing system and method of the offshore operation helicopter, the full process is automatically controlled; the method is more scientific and reliable; the helicopter can also be safely andstably pulled into the hangar or out of the hangar even under a complicated sea condition of 4 grade or above; and moreover, the operation in the whole process is simple, and manpower and material resources are saved.