163 results about "Ejection Seats" patented technology

A head and neck restraint system includes a headpiece, a saddle, and tensioners connecting the headpiece to the saddle. The headpiece resides on top of a crew member's head and the saddle includes a saddle strap residing under the crew member's buttocks. The tensioners are pneumatic muscles which contract when a flow of gas is provided by gas generators. The gas generators are triggered by a G-sensor or by the initiation of a predetermined event. Triggering signals pass through a manifold from an ejection seat, aircraft, or vehicle. Contraction of the pneumatic muscles pulls the headpiece toward the saddle, thereby restraining the head, neck, and spine. The system is worn as an undergarment or incorporated into a garment. A manual adjustment provides head support during flight. The system is particularly useful for preventing head and neck injuries during ejection from or crash of an aircraft or vehicle

An ejection seat includes a headrest that, upon initiation of the ejection seat, moves forward to support the pilot's head in a tilted-forward position. By holding the crewmember's head in a tilted-forward position, windblast forces are controlled to prevent the helmet from pulling upward and backward on the crewmember's head. The headrest may include a pair of struts that extend forward around the sides of the crewmember's helmet to support the crewmember's head against flailing from the windblast. A flexible panel extending between the struts and the headrest panel may also be included to further support the crewmember's head against windblast flailing.

A head and neck restraint system includes a headpiece, a saddle, and tensioners connecting the headpiece to the saddle. The headpiece resides on top of a crew member's head and the saddle includes a saddle strap residing under the crew member's buttocks. The tensioners are pneumatic muscles which contract when a flow of gas is provided by gas generators. The gas generators are triggered by a G-sensor or by the initiation of a predetermined event. Triggering signals pass through a manifold from an ejection seat, aircraft, or vehicle. Contraction of the pneumatic muscles pulls the headpiece toward the saddle, thereby restraining the head, neck, and spine. The system is worn as an undergarment or incorporated into a garment. A manual adjustment provides head support during flight. The system is particularly useful for preventing head and neck injuries during ejection from or crash of an aircraft or vehicle.

The invention provides a car driver and passenger life-saving escape system and an operation method thereof, which can quickly eject a driver and passengers out of a car with a narrower space under the extremely-dangerous situations that the car is strongly collided, overturns at a high speed, burns and explodes, falls off, or is caught in water, so as to reduce the probability of severe disability and death. The car driver and passenger life-saving escape system comprises a system control device, a car emergency alarm, an automatic braking flameout controller, an ejection seat, an emergency separation type ceiling, an elastic protection mesh film and the like. When the severe accidents are happened to the car, the driver manually triggers the car or the car automatically triggers when a system control module detects that the relevant value exceeds the critical value to send out alarm and braking flameout information and generate instantaneous high-pressure gas, so as to prop the emergency separation type ceiling open and drive seats, the driver and the passengers to be ejected towards the upper rear side of the car; and meanwhile, the elastic protection mesh film arranged in the ceiling is instantaneously pulled out to carry out elastic pullback on the driver and the passengers, so that the speed of the driver and the passengers to the ground is reduced, and the casualties are further reduced.

An ejection seat includes a headrest that, upon initiation of the ejection seat, moves forward to support the pilot's head in a tilted-forward position. By holding the crewmember's head in a tilted-forward position, windblast forces are controlled to prevent the helmet from pulling upward and backward on the crewmember's head. The headrest may include a pair of struts that extend forward around the sides of the crewmember's helmet to support the crewmember's head against flailing from the windblast. A flexible panel extending between the struts and the headrest panel may also be included to further support the crewmember's head against windblast flailing.

An emergency ejection seat adjustable along two independent axes: vertical adjustment (up and down) and horizontal adjustment (fore and aft). The ejection seat adjusts to accommodate all aircrew sizes, sitting shoulder heights, buttock-knee lengths, and functional limb reaches and is constructed of modular components which are easily removed and replaced. The ejection seat comprises a seat bucket structure, a seat insert, a linkage assembly and equipment bays. The linkage assembly interfaces between the ejection seat bucket structure and seat insert to allow both vertical and horizontal adjustment.

An arrangement in passenger vehicles, that diverts the impact energy in lateral or side impacts away from the passengers to the remaining mass of the vehicle thereby protecting the passengers, and in the same arrangement provides utilitarian access to the vehicle, such utilitarian access making it possible to both install multi-element contoured surround seats for passengers and the driver, and also a safety device for head-on collision protection that obviates the need for conventional seat belts and front impact airbags. An indo-skeletal structural arrangement proposed for the vehicle, provides further benefits by targeting the strength of the vehicle to protect passengers while minimizing other massive elements in the vehicle.

The invention provides a multipurpose pneumatic type ejection airborne landing flight training device, and an ejection method is utilized to eject training personnel to a high altitude, the training personnel utilize the airborne landing flight training devices equipped for the training personnel to perform airborne landing or air the training personnel flight training, or the trainers without any device are ejected to safety protection equipment in a fixed-point mode to perform parachuting basic training. The training device comprises a base seat, a pneumatic ejection device, a saddle-shaped ejection seat, an elevation angle adjuster and safe landing protection facilities, wherein the elevation angle adjuster and the ejection device are arranged on the base seat, the ejection seat is arranged on the ejection device, and the safe landing protection facilities are arranged on a landing point. The airborne landing flight training device comprises a parachute, a delta wing aircraft, a wing outfit aircraft, a fixed wing aircraft or other single pawn airborne landing flight devices, when the airborne landing flight training device is used, geographical environment limitation does not exist, parachuting, delta wing flight, wing outfit flight, fixed flight or pneumatic parachute flight motions can be popularized quickly, and meanwhile, the research and development of the sports equipment can further be driven.

An ejection seat arm flail injury prevention apparatus comprises a pair of rigid support arms on each side of the ejection seat that deploy outwardly to support a semi-rigid backstop substantially behind the ejection seat occupant. When the ejection seat is propelled out of the aircraft and is subjected to the windblast, the occupant's arms are allowed to flail in a rearward direction in the windblast until the occupant's arms impact the semi-rigid backstop. The backstop is semi-rigid in that it deforms sufficiently to enable the rearward motion of the occupant's arms to be arrested without impact injury, yet is sufficiently rigid to prevent the occupant's arms from rebounding off the backstop or striking the rigid support arms.

An ejection seat arm flail injury prevention apparatus comprises a pair of rigid support arms on each side of the ejection seat that deploy outwardly to support a semi-rigid backstop substantially behind the ejection seat occupant. When the ejection seat is propelled out of the aircraft and is subjected to the windblast, the occupant's arms are allowed to flail in a rearward direction in the windblast until the occupant's arms impact the semi-rigid backstop. The backstop is semi-rigid in that it deforms sufficiently to enable the rearward motion of the occupant's arms to be arrested without impact injury, yet is sufficiently rigid to prevent the occupant's arms from rebounding off the backstop or striking the rigid support arms.

The invention relates to an ejection seat simulator of extraction parachute type for experiencing escape from a manned aircraft which includes a base, a guide rail, a power device, a somatosensory seat, a head-mounted display, and a pair of control pull ring. A box, a controller and an air pump are disposed on the base. The power device includes a first support plate, a hydraulic rod, a guide wheel set, a first shaft, a connecting plate, a motor and a gear set. The control pull ring includes a ring body and a pull rope. The ring body is inlaid with a control button, a wireless transmission module, a tension sensor and a buffer spring. The ejection seat simulator of extraction parachute type for experiencing escape from a manned aircraft of the invention has advantages of having reasonable and simple structure, easy to operate, low price, safe and reliable, strong authenticity, high intelligence, which effectively solves the problem of being unable to experience or train escape in ejection seats in the real manned aircrafts.

A piezo-driven micro-droplet jet generator comprises an ejection seat, having an ejection plate with a plurality of ejection holes; a membrane, having a front side facing the ejection seat and a rear side; a piezoelectric plate, placed at the rear side of the membrane, at least partly touching the membrane and, when electric voltage is applied, driving a vibrating movement of the membrane towards the ejection plate; a base plate, at four corners thereof fastened to the ejection seat and to the membrane; and a flow path inside the ejection seat, allowing liquid to be let into a space inside the ejection seat; wherein liquid between the membrane and the ejection plate upon the vibrating movement undergoes pressure, being ejected through the plurality of ejection holes.

An ejection seat includes a headrest that, upon initiation of the ejection seat, moves forward to support the pilot's head in a tilted-forward position. By holding the crewmember's head in a tilted-forward position, windblast forces are controlled to prevent the helmet from pulling upward and backward on the crewmember's head. The headrest may include a pair of struts that extend forward around the sides of the crewmember's helmet to support the crewmember's head against flailing from the windblast. A flexible panel extending between the struts and the headrest panel may also be included to further support the crewmember's head against windblast flailing.

An arrangement in passenger vehicles, that diverts the impact energy in impacts away from the passengers to the remaining mass of the vehicle thereby protecting the passengers, and in the same arrangement provides utilitarian access to the vehicle, such utilitarian access making it possible to both install multi-element contoured surround seats for passengers and the driver, and also a safety device for head-on collision protection that obviates the need for conventional seat belts and front impact airbags. An indo-skeletal structural arrangement proposed for the vehicle, provides further benefits by targeting the strength of the vehicle to protect passengers while minimizing other massive elements in the vehicle.

The invention discloses a panel component drawing processing mold assembly for metal stamping, which comprises a lower mold base, a liquid storage tank, an oil supply pump, a jacking base, an upper mold base and a lower mold sleeve, and the lower surface of the upper mold base is fixedly connected with a punch , the lower die set is fixed on the lower die base and the inner surface of the lower die set is contacted with a bottom plate, the edge of the lower surface of the bottom plate is fixed with a support ring plate, the side of the lower die set is provided with a ring groove, and the liquid outlet of the oil supply pump passes through The pipeline communicates with the ring groove from the inner ring surface of the supporting ring plate, and the inner wall of the lower die sleeve is provided with an oil collecting groove, the oil collecting groove is connected to the liquid storage tank through the pipeline, and the oil inlet of the oil supply pump is connected to the liquid storage tank through the pipeline. This kind of metal stamping panel parts stretching processing mold assembly uses the inner bottom surface of the lower mold sleeve as the ejection surface to increase the ejection force area to avoid deformation, and brush the side wall with lubricating oil or remove it while ejecting. The mold agent assists in demoulding while protecting the surface of the mold and the surface of the workpiece to improve the stamping quality of the product.

The invention provides a low-altitude attitude control method for an ejection seat, and belongs to the field of aviation life-saving safety protection. The low-altitude attitude control method is mainly used for solving the problems of optimality and timeliness of control strategy of an aircraft during low-altitude flight. According to the low-altitude attitude control method, a mode of combininga genetic algorithm (GA) and a BP neural network algorithm is adopted to obtain a neural network structure between flight state parameters and control parameters, when a pilot needs ejection life-saving during low-altitude flight, the working states of a main rocket, a roll rocket and a pitching rocket are judged according to an established neural network, the optimal working time of each rocket and the optimal time for shooting a parachute are obtained, finally through a timing controller, optimal or near-optimal attitude control of a human-seat system during low-altitude life-saving is achieved, and the life-saving success rate can be effectively increased. Compared with a traditional mode control method, the low-altitude attitude control method has the advantages that timeliness is high, the control effect is close to the optimal effect, and fault tolerance is high.

An ejection seat having pitch, roll, and yaw control provided by three separate rocket motors where each rocket motor has a fixed nozzle and the entire rocket motor is rotated about a single axis corresponding to the minimum principal moment of inertia of the rocket. Actuation for each rocket motor is by means of a hydraulic rack and pinion actuator. Power for the hydraulic actuators is provided by a unique hydro-pneumatic amplifier that converts stored gas energy into pressurized hydraulic fluid. The high pressure hydraulic fluid is directed through conventional servo valves into the appropriate actuators to provide main, roll, pitch, and yaw thrust as required to achieve upright orientation and vertical flight.

An ejection seat having pitch, roll, and yaw control provided by three separate rocket motors where each rocket motor has a fixed nozzle and the entire rocket motor is rotated about a single axis corresponding to the minimum principal moment of inertia of the rocket. Actuation for each rocket motor is by means of a hydraulic rack and pinion actuator. Power for the hydraulic actuators is provided by a unique hydro-pneumatic amplifier that converts stored gas energy into pressurized hydraulic fluid. The high pressure hydraulic fluid is directed through conventional servo valves into the appropriate actuators to provide main, roll, pitch, and yaw thrust as required to achieve upright orientation and vertical flight.

The invention provides a modularized ejection seat and an escaping airplane comprising same, and relates to an escaping apparatus. The invention aims at providing a modularized ejection seat capable of helping passengers to rapidly escape from a compartment and an escaping airplane comprising the modularized ejection seat. The modularized ejection seat comprises a seat body and an ejection apparatus, wherein the seat body is fit to an ejection end of the ejection apparatus and can be separated from the ejection apparatus under the ejection effect of the ejection apparatus. The escaping airplane comprises an airplane body, an escaping window and the modularized ejection seat, wherein the escaping window is arranged on the airplane body; the ejection apparatus is fixedly arranged relative to the escaping window; and the seat body is opposite to the escaping window, and the seat body is completely separated from the airplane body by virtue of the escaping window under the ejection effect of the ejection apparatus.

A safety evacuation system for drivers and passengers of ground and water vehicles is proposed. The system is comprised of a sensor system, computer implemented model of risk assessments from collisions with surrounding objects, control system, safety escape channels, and ejection seats. The sensor system measures directions, speeds and distances of a vehicle to all objects, which may collide with the vehicle and pose risk of deaths or injures to humans in the vehicle. The computer-implemented model assesses the risk of deaths and injuries for humans, based on the measurements of the sensor system. The control system opens the escape channel and activates ejection seats based on the risk assessments from the computer-implemented model.

The invention relates to the field of safe driving, in particular to an ejection seat. The ejection seat comprises a seat body, an ejection device and a direction control system. The ejection device is mounted on the lower portion of the seat body, and the direction control system is mounted on the seat body and used for controlling an ejection direction of the seat body and controlling an advancing direction of the seat body. By the aid of the ejection seat, when a vehicle falls off a cliff, falls into a river, lake or sea or is in serious collision, a driver and / or a passenger can be ejected out while the ejection direction and the advancing direction of the seat body can be controlled, and the driver and / or the passenger are sent to a nearby safety region for protection after ejection.

An aircraft is provided and includes a fixed frame including a ledge and a seat pan on which seating elements for seating an aircraft crewperson are disposable. The seat pan includes a hinge about which the seat pan is pivotable relative to the fixed frame and a flange disposable on the ledge to establish a first pivot position for the seat pan relative to the fixed frame and a seat pan lifter coupled to the fixed frame and selectively interposable between the flange and the ledge to establish a second pivot position for the seat pan relative to the fixed frame.

The invention discloses a vehicle-mounted air-drop type forest fire extinguisher which comprises a cylindrical main body part, an air cap, an umbrella cover and a tail wing, wherein the air cap is arranged at the front end of the cylindrical main body part; the umbrella cover is arranged at the rear end of the cylindrical main body part; the tail wing is arranged at the tail part of the umbrella cover; the air cap is separated from the cylindrical main body part by virtue of a pressure-bearing seat; the cylindrical main body part is separated from the umbrella cover by virtue of an ejection seat; a fuze of which the section is convex is arranged in the umbrella cover, the protruding part props against the end part of the conical inner surface of the umbrella cover, and the bottom of the fuze is fixedly arranged on the bearing seat; a gap between the bearing seat and the ejection seat is filled with a fire extinguishing agent; one end of a long-strip-shaped central detonator is fixed together with the bearing seat, and the other end of the central detonator is suspended in the fire extinguishing agent; the interior of the umbrella cover is filled with a brake parachute; a bomb-parachute connector connected with the brake parachute is fixedly arranged in the middle of the end surface, which faces the umbrella cover, of the ejection seat; and a cutting rope is arranged at the upper end, which faces the umbrella cover, of the ejection seat. According to the fire extinguisher disclosed by the invention, each part is reliable in connection, and the filling quantity of the fire extinguishing agent is increased, so that the fire extinguishing efficiency is high.

A method for precisely controlling the time delay of a parachute opening device based on different temperatures, comprises the following steps: (1) after the starting of the ejection, high pressure fuel gas enters the thermal battery component of a parachute opening device from a seat control system, the thermal battery is activated, and the parachute opening device is powered; (2) the initialization of the parachute opening device system is conducted, the timer begins timekeeping, the power-on self-test of parachute opening device is conducted, and the preset delay time or artificially preset delay time is obtained from external memory according to the result of the power-on self-test; (3) the ambient temperature of the parachute opening device is obtained through a temperature sensor, the activation time of thermal battery is determined; (4) after the height of parachute opening device is determined and the height determining time is recorded, the real output delay time of the parachute opening device can be obtained by the following formula: real output delay time = preset delay time-thermal battery activation time-program running time-program running time; (5) executing the time delay action of the parachute opening device, and an ignition command is outputted. The accurate time delay output of the parachute opening device can be achieved at 55-70 DEG C, and the safety life saving performance of an ejection seat is improved at different temperatures.

The invention discloses a gasoline-engine-driven multi-rotor fire-extinguishing life-saving manned aircraft and belongs to the field of special aircrafts. The gasoline-engine-driven multi-rotor fire-extinguishing life-saving manned aircraft high in bearing capacity and long in duration is provided and carries a cockpit; an ejection seat, an operating bar and a display screen are fitted in the cockpit; an ejection parachute is fitted to the back of the ejection seat; the aircraft herein is a manned aircraft and remote-control aircraft; the aircraft herein is a multifunctional aircraft having anelectric block, a remote-control cable propeller and a life jacket or basket life stretcher is suitable for carrying out high-rise building or field lifesaving; with a fire-extinguishing rocket launcher and a fire-extinguishing rocket projectile, the aircraft herein is suitable for high-rise building fire extinguishing; a cargo hold provided herein allows cargoes to be conveyed; special instruments and devices are carried, so that the aircraft herein is available for high-rise building fire extinguishing and lifesaving, field search and lifesaving, goods air transportation and dropping, aerial patrolling and monitoring, pesticide spraying, and other special tasks.

The invention discloses a safety ejection seat for an automobile. The safety ejection seat comprises a seat body, two first electric cylinders, two side doors, two sliding frames and the like. The safety ejection seat is characterized in that the seat body comprises a bottom plate part and a backrest part, the backrest part is internally hollow, two guide rails are arranged on the two sides of the inner wall of the internal space correspondingly, two sliding frames are symmetrically installed on the guide rails in a sliding manner, and an electric cylinder installation seat is arranged at the middle position of the top of the inner wall. A boost power unit in the backrest is concealed in the backrest when not used and slides out when the boost power unit needs to be used, the space in the automobile is saved, meanwhile, a parachute system is arranged, and therefore the seat can land safely.