CN203211515U - Multipurpose pneumatic type ejection airborne flight training device - Google Patents
Multipurpose pneumatic type ejection airborne flight training device Download PDFInfo
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- CN203211515U CN203211515U CN 201320055580 CN201320055580U CN203211515U CN 203211515 U CN203211515 U CN 203211515U CN 201320055580 CN201320055580 CN 201320055580 CN 201320055580 U CN201320055580 U CN 201320055580U CN 203211515 U CN203211515 U CN 203211515U
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Abstract
The utility model provides a multipurpose pneumatic type ejection airborne flight training device. A method of ejection is used for ejecting a training person to a high altitude, the training person uses an equipped airborne flight training outfit to carry out airborne landing or aerial flight training in the air, or the training person without any outfit is ejected to a safety protection facility to carry out parachuting basic training in a fixed point mode. The multipurpose pneumatic type ejection airborne flight training device comprises a base, a pneumatic ejection device, a saddle-shaped ejection seat, an elevation adjuster and a safe landing protection facility, wherein the elevation adjuster and the pneumatic ejection device are arranged on the base, the ejection seat is arranged on the pneumatic ejection device, and the safe landing protection facility is arranged on a landing point. The airborne flight training outfit comprises a parachute or a delta-wing aircraft or a wing air craft or a fixed-wing air craft or other individual soldier airborne flight devices. The multipurpose pneumatic type ejection airborne flight training device is not limited by the geographical environment, parachuting sports or delta-wing flight sports or wing flight sports or fixed-wing flight sports or paramotoring flight sports can be rapidly popularized, and meanwhile research, development and production of the sports apparatuses can be promoted.
Description
Technical field
The present invention relates to military sports training equipment technology field, specifically the high-mobility, multipurpose, wheeled vehicle pneumatic type of a kind of aircraft carrier aviator, parachutist, special war team member or extreme sport training usefulness is launched airborne flight training device.
Background technology
As everyone knows, aircraft carrier is a floating afloat adrm, the mode of taking off with aircraft carrier of powerful fight capability is catapult-assisted take-off, comparing take off its advantage of aircraft carrier of mode of the sliding formula of jumping is to fully loaded takeoff, have full load bullet-loading capacity and fuel load, stronger attacking ability and cruise duration are arranged, so the development aircraft carrier does not solve carrier-based aircraft ejector, aircraft carrier can only be a kind of ornaments or be a large-scale delivery ship, therefore carrier-borne aircraft aviator's catapult-assisted take-off is an indispensable training program, carrier-borne aircraft pilot ejection is in the world at present taken off to train and is mostly directly to carry out at aircraft carrier, because have only carrier-based aircraft ejector just arranged on the aircraft carrier, for a carrier-borne aircraft aviator new hand, in the primary stage of flying catapult-assisted take-off, owing to the big reason of ejection acceleration, aircraft brain moment ischemic behind the warship has the interim comatose state in ten seconds, aircraft is by autopilot flight, but the accident that falls into the sea out of control is quite a few because the aviator goes into a coma sees for aircraft, a carrier-borne aircraft aviator will train just can progressively adapt to launch usually and accelerate to take off through above the taking off of catapult-assisted take-off 30 sorties, becomes qualified carrier-borne aircraft aviator.The deficiency that this kind combat training mode exists is to rely on aircraft carrier, dependence carrier-borne aircraft and ejector, and training cost height has a big risk, fatal crass's danger is arranged at any time, at present, China does not have carrier-based aircraft ejector, so can't carry out a large amount of effective catapult-assisted take-off training to the carrier-borne aircraft aviator.
The combatant who comprises parachutist and Te war team delivers at a distance, utilize aircraft to make the delivery instrument exactly, high altitude bailout is by the indispensable training subject of delivery personnel, the parachute jumping elementary training of prior art is to utilize parachute tower, open parachute and people are risen to together the high-altitude of 50-100 rice by elevator, discharge slowly parachuting landing of chutist then, second step be in a helicopter or transport plane lift-off implement jumper training, the deficiency of above-mentioned training patterns is, the trial ground that elementary training need be fixed and parachute tower, can only carry out elementary muscle-setting exercise, second step must rely on aircraft, also be subjected to parachuting geographical environment and weather factor affecting etc., the trainer also influences training effect to skill level and the psychological factor that parachute kit uses, the do not open accident of falling to death the people of parachute kit also is that generation is arranged frequently, the equipment that does not also have at present to board and can accelerate to go up to the air jumper training to the carrier-borne aircraft aviator, and the equipment that can carry out high-altitude acceleration jumper training to special war team of parachutist does not just have to go by air yet.
Summary of the invention
Technical assignment of the present invention is to solve the deficiencies in the prior art, provides a kind of high-mobility, multipurpose, wheeled vehicle pneumatic type to launch airborne flight training device.
Technical scheme of the present invention realizes in the following manner, the method that utilization is launched is launched the high-altitude with the trainer, the trainer utilizes the airborne flight training that self is equipped with to be equipped in the airborne or airflight training of aerial enforcement, or trainer's fixed point of carrying no luggage launched the basic training of parachuting on the safety precaution facility, this training aids comprises base, pneumatic catapult-launching gear, shape of a saddle ejection-seat, elevation angle adjuster and safe landing protective equipment, elevation angle adjuster and catapult-launching gear are arranged on the base, ejection-seat is arranged on the catapult-launching gear, the safe landing protective equipment is arranged on the point that lands, wherein:
Base is used for the fixed elevation adjuster, comprises movable base and firm banking, and movable base is car chassis, and firm banking is high-rise;
Pneumatics comprises accumulator unit, cantilever beam, launches cylinder, grooved track and launch dolly,
Accumulator unitBe arranged on the base, cantilever beam is made up of cantilever beam and grooved track, and two channel suspending rails are fixed on the both sides that section is the cantilever beam top of rectangle, launch cylinder and are arranged in the middle of the cantilever beam;
The two ends of cantilever beam are provided with pulley, be provided with piston among launching cylinder, the two ends of piston connect trailing cable, two trailing cables pass the through hole in the middle of the cylinder cover mid seal of launching the cylinder two ends respectively, walking around the pulley at cantilever beam two ends is connected with the dolly two ends of launching in being arranged on the grooved track, shape of a saddle ejection-seat is fixed on and launches on the dolly, the bottom of launching cylinder also is provided with total inlet pipe, the total inlet pipe two ends are connected with the two ends of launching cylinder with low side electromagnetic switch triple valve by high-end electromagnetic switch triple valve, two electromagnetic switch triple valves are connected with ejection controller on being arranged on base by the control cable, the low side of cantilever beam also is provided with counterweight and supports, total inlet pipe is connected with total air inlet electromagnetic valve on the accumulator unit by high pressure hose, and accumulator unit is connected with high-pressure pump;
Elevation angle adjuster is used for regulating the elevation angle between cantilever beam and the ground, its structure is by bracing frame, sliding sleeve vertical lift hydraulic actuating cylinder, C shape sliding sleeve and sliding sleeve horizontal drive hydraulic actuating cylinder are formed, wherein, the section of C shape sliding sleeve is C shape, C shape sliding sleeve is connected with the cantilever beam basal sliding, one end and the cantilever beam of sliding sleeve horizontal drive hydraulic actuating cylinder are fixed, the other end is connected with C shape sliding sleeve, the top of sliding sleeve vertical lift hydraulic actuating cylinder is by hinge and high-end connection of C shape sliding sleeve, the lower end of sliding sleeve vertical lift hydraulic actuating cylinder is connected with base by hinge, the bottom of bracing frame is connected with base, and the top of bracing frame is connected by the low side of twisted axis with C shape sliding sleeve;
The bottom of shape of a saddle ejection-seat is the shape of a saddle and rides on the cantilever beam, and the both sides, top of shape of a saddle ejection-seat are provided with handrail, and two of shape of a saddle type seat bottom is surveyed and also is provided with pedal;
Ejection controller comprises micro controller system, plays point sensor, end point sensor, is arranged on load cell and jettison push-button switch under the shape of a saddle ejection-seat, wherein, end point sensor is arranged on 1-3 rice high-end apart from cantilever beam, and a point sensor is arranged on 1 meter apart from the cantilever beam low side; High-end and two electromagnetic switch triple valves low side have been subjected to point sensor, end point sensor and jettison push-button switch interlock control;
The control step is as follows:
The trainer is sitting on the ejection-seat, ejection controller detects the operation pressure that shows accumulator unit, the weight of ejection-seat, the operator launches parameter by keyboard to the micro controller system input, comprise ejection speed, height and the elevation angle, micro controller system shows the ejection altitude that can reach and lands the some distance by calculating, and adjust the elevation angle of cantilever beam automatically, operating personal is placed in landing position with the safe landing protective equipment, can implement to launch, suppose to decide the high-end for launching terminal point of cantilever beam, low side is for launching starting point, when jettison push-button switch sent electricity, total air inlet electromagnetic valve was opened the air inlet open of high-end electromagnetic switch triple valve, exhaust close, the inlet close of low side electromagnetic switch triple valve, Exhaust Open, the high pressure gas in the accumulator unit enter cylinder by total inlet pipe and the high-end admission port of cylinder, be positioned at the high-end piston of cylinder and move at the promotion lower cylinder low side of high pressure gas, piston launches movement by trailing cable traction shape of a saddle ejection-seat to cantilever beam is high-end;
When moving up, shape of a saddle ejection-seat approaches when launching end point sensor, after launching the end point sensor triggering, launch the high-end commutation three-way magnetic valve inlet close of cylinder, Exhaust Open, launch the exhaust close of cylinder low side commutation three-way magnetic valve, open admission port simultaneously, because the end point sensor that launches that arranges has a segment distance apart from the cylinder low side, piston carries out compressed action by inertia to the air in this segment distance cylinder, pressurized air produces damping to the motional inertia of piston, because ejection-seat is connected interlock with piston by hauling rope, ejection-seat is damped out of service;
Piston is when launching the terminal point inertia damping, the inlet close of the high-end commutation three-way magnetic valve of cylinder is launched in ejection controller control, Exhaust Open, launch the exhaust close of cylinder low side commutation three-way magnetic valve, air inlet open, high pressure gas enter cylinder by the admission port that launches the cylinder low side, and promoting piston again, to return cylinder high-end, and descending the returning of ejection-seat launched starting point;
Ejection-seat is descending to be returned when launching starting point, triggering is positioned at the point sensor that rises of cylinder low side, total air inlet electromagnetic valve is closed in ejection controller control, launch the inlet close of the high-end three-way magnetic valve of cylinder, Exhaust Open, launch the inlet close of the three-way magnetic valve of cylinder low side, Exhaust Open launches cylinder and enters the next one and launch set up procedure.
Airborne flight training equipment comprises: parachute, delta wing aircraft, wing dress aircraft, fixed-wing aircraft or the airborne flight instruments of other individual soldiers.
The safe landing protective equipment is made up of safety guard net and inflatable airbags, and safety guard net covers on inflatable airbags.
The safe landing protective equipment is sand ground, bay, lake or pond.
Outstanding beneficial effect of the present invention: simple in structure, be easy to processing, combination is installed, and convenient transportation train easy to usely, does not use aircraft can finish the acceleration ejection training, does not use aircraft also can finish parachuting training and extreme sport and trains.This device has safe and reliable; the safety precaution facilities protection is arranged; the training how many times can not cause any harm to the trainer yet; can increase substantially training effect; reduce the training risk; reduce the training cost; also be not subjected to geographical environment and climatic influences; human body is launched the high-altitude can also carry out the development of a lot of parachute kits and flying instrument by launching; such as: various parachutes; the delta wing aircraft; wing dress clothes; the development of fixed-wing aircraft and exploitation can not only be satisfied the needs of national defense and military, also can be used as the extreme sport equipment and promote the use of among the people; be conducive to improve the raising of military sports and popularize, have very wide market outlook.
Description of drawings
Fig. 1 is the structural representation of gas-powered catapult;
Fig. 2 is the general assembly structural representation that portable ejection bailout training aids uses state;
Fig. 3 is the general assembly structural representation of portable ejection bailout training aids static condition;
Fig. 4 is the general assembly structural representation of fixed type ejection bailout training aids;
Fig. 5 is positioned at the cantilever beam section structure scheme drawing that launches the dolly place.
Mark in the accompanying drawing is represented respectively: pulley 1, cantilever beam 2, grooved track 3, launch cylinder 4, sliding sleeve horizontal drive hydraulic actuating cylinder 5, C shape sliding sleeve 6, sliding sleeve vertical lift hydraulic actuating cylinder 7, ejection controller 8, accumulator unit 9, bracing frame 10, base 11, launch dolly 12, counterweight supports 14, total inlet pipe 15, trailing cable 16, piston 17, end point sensor 18, play point sensor 19, high-end electromagnetic switch triple valve 20, low side electromagnetic switch triple valve 21, total air inlet electromagnetic valve 22, pedal 23, cylinder cover 24, sealing member 25.
The specific embodiment
By reference to the accompanying drawings high-mobility, multipurpose, wheeled vehicle pneumatic type of the present invention being launched airborne flight training device is described in further detail.
High-mobility, multipurpose, wheeled vehicle pneumatic type of the present invention is launched airborne flight training device, be to utilize the method for launching that the trainer is launched the high-altitude, the trainer utilizes the airborne flight training that self is equipped with to be equipped in the airborne or airflight training of aerial enforcement, or trainer's fixed point of carrying no luggage launched the basic training of parachuting on the safety precaution facility, this training aids comprises base, pneumatic catapult-launching gear, shape of a saddle ejection-seat, elevation angle adjuster and safe landing protective equipment, elevation angle adjuster and catapult-launching gear are arranged on the base, ejection-seat is arranged on the catapult-launching gear, the safe landing protective equipment is arranged on the point that lands, wherein:
Base is used for the fixed elevation adjuster, comprises movable base and firm banking, and movable base is car chassis, and firm banking is high-rise;
Pneumatics comprises accumulator unit 9, cantilever beam 2, launches cylinder 4, grooved track 3 and launch dolly 12,
Accumulator unitBe arranged on the base, cantilever beam is made up of cantilever beam and grooved track, and two channel suspending rails are fixed on the both sides that section is the cantilever beam top of rectangle, launch cylinder and are arranged in the middle of the cantilever beam;
The two ends of cantilever beam 2 are provided with pulley 1, be provided with piston 17 among launching cylinder 4, the two ends of piston 17 connect trailing cable 16, two trailing cables 16 pass the through hole in the middle of cylinder cover 24 mid seal 25 of launching cylinder 4 two ends respectively, walking around the pulley 1 at cantilever beam 2 two ends is connected with dolly 12 two ends of launching in being arranged on the grooved track, shape of a saddle ejection-seat 13 is fixed on and launches on the dolly 12, the bottom of launching cylinder 4 also is provided with total inlet pipe 15, total inlet pipe 15 two ends are connected with the two ends of launching cylinder 4 with low side electromagnetic switch triple valve 21 by high-end electromagnetic switch triple valve 20, two electromagnetic switch triple valves are connected with ejection controller 8 on being arranged on base by the control cable, the low side of cantilever beam 2 also is provided with counterweight and supports 14, total inlet pipe 15 is connected with total air inlet electromagnetic valve 22 on the accumulator unit 9 by high pressure hose, and accumulator unit 9 is connected with high-pressure pump;
Elevation angle adjuster is used for regulating the elevation angle between cantilever beam 2 and the ground, its structure is by bracing frame 10, sliding sleeve vertical lift hydraulic actuating cylinder 7, C shape sliding sleeve 6 and sliding sleeve horizontal drive hydraulic actuating cylinder 5 are formed, wherein, the section of C shape sliding sleeve 6 is C shape, C shape sliding sleeve 6 is connected with cantilever beam 2 basal slidings, one end of sliding sleeve horizontal drive hydraulic actuating cylinder 5 and cantilever beam 2 are fixing, the other end is connected with C shape sliding sleeve 6, the top of sliding sleeve vertical lift hydraulic actuating cylinder 7 is by hinge and 6 high-end connections of C shape sliding sleeve, the lower end of sliding sleeve vertical lift hydraulic actuating cylinder 7 is connected with base 11 by hinge, the bottom of bracing frame 10 is connected with base 11, and the top of bracing frame 10 is connected by the low side of twisted axis with C shape sliding sleeve 6;
The bottom of shape of a saddle ejection-seat 13 is the shape of a saddle and rides on the cantilever beam 2, and the both sides, top of shape of a saddle ejection-seat 13 are provided with handrail, and two of shape of a saddle type seat 13 bottoms are surveyed and also are provided with pedal 23;
Ejection controller 8 comprises micro controller system, plays point sensor 19, end point sensor 18, is arranged on load cell 26 and jettison push-button switch under the shape of a saddle ejection-seat 13, wherein, end point sensor 18 is arranged on 1-3 rice high-end apart from cantilever beam 2, plays point sensor 19 and is arranged on 1 meter apart from cantilever beam 2 low sides; High-end and two electromagnetic switch triple valves low side have been subjected to point sensor 19, end point sensor 18 and jettison push-button switch interlock control;
The control step is as follows:
The trainer is sitting on the ejection-seat, ejection controller detects the operation pressure that shows accumulator unit, the weight of ejection-seat, the operator launches parameter by keyboard to the micro controller system input, comprise ejection speed, height and the elevation angle, micro controller system shows the ejection altitude that can reach and lands the some distance by calculating, and adjust the elevation angle of cantilever beam automatically, operating personal is placed in landing position with the safe landing protective equipment, can implement to launch, suppose to decide the high-end for launching terminal point of cantilever beam, low side is for launching starting point, when jettison push-button switch sent electricity, total air inlet electromagnetic valve was opened the air inlet open of high-end electromagnetic switch triple valve, exhaust close, the inlet close of low side electromagnetic switch triple valve, Exhaust Open, the high pressure gas in the accumulator unit enter cylinder by total inlet pipe and the high-end admission port of cylinder, be positioned at the high-end piston of cylinder and move at the promotion lower cylinder low side of high pressure gas, piston launches movement by trailing cable traction shape of a saddle ejection-seat to cantilever beam is high-end;
When moving up, shape of a saddle ejection-seat approaches when launching end point sensor, after launching the end point sensor triggering, launch the high-end commutation three-way magnetic valve inlet close of cylinder, Exhaust Open, launch the exhaust close of cylinder low side commutation three-way magnetic valve, open admission port simultaneously, because the end point sensor that launches that arranges has a segment distance apart from the cylinder low side, piston carries out compressed action by inertia to the air in this segment distance cylinder, pressurized air produces damping to the motional inertia of piston, because ejection-seat is connected interlock with piston by hauling rope, ejection-seat is damped out of service;
Piston is when launching the terminal point inertia damping, the inlet close of the high-end commutation three-way magnetic valve of cylinder is launched in ejection controller control, Exhaust Open, launch the exhaust close of cylinder low side commutation three-way magnetic valve, air inlet open, high pressure gas enter cylinder by the admission port that launches the cylinder low side, and promoting piston again, to return cylinder high-end, and descending the returning of ejection-seat launched starting point;
Ejection-seat is descending to be returned when launching starting point, triggering is positioned at the point sensor that rises of cylinder low side, total air inlet electromagnetic valve is closed in ejection controller control, launch the inlet close of the high-end three-way magnetic valve of cylinder, Exhaust Open, launch the inlet close of the three-way magnetic valve of cylinder low side, Exhaust Open launches cylinder and enters the next one and launch set up procedure.
Airborne flight training equipment comprises: parachute, delta wing aircraft, wing dress aircraft, the airborne flight instruments of other individual soldiers of fixed-wing aircraft.
The safe landing protective equipment is made up of safety guard net and inflatable airbags, and safety guard net covers on inflatable airbags.
The safe landing protective equipment is bay, lake or pond.
Movable base can use the car chassis repacking, installing elevation angle adjuster, bracing frame, the gentle injection device of moving of accumulator unit additional at movable base gets final product, if pneumatic catapult-launching gear by the power designs of launching 200 kilograms of human bodies, is needed only and changes shape of a saddle ejection-seat into large-scale unmanned plane that the unmanned aerial vehicle ejecting frame is ejectable weight more than 200 kilograms.
Human body limit launches flight training: training goal: improve the trainee to the tolerance of acceleration/accel, and for aircraft carrier provides a large amount of outstanding carrier-borne aircraft aviators, as civilian general, and the military sports campaign, strengthen nationwide physical condition and improve whole people's awareness of national defence;
Designing requirement: be 30-50 rice with the cantilever beam design length, the elevation angle 45 degree adopt and install at car chassis, launch 200 kilograms of weight, ejection altitude 50-100 rice with parabolic catapulting distance 50-100 rice, arranges the safe landing protective equipment of 50-100 square meter below the point that lands;
Training patterns: the trainer can take ejection-seat and launch lift-off, with parabolical mode free-falling body to the safe landing protective equipment, be equivalent to high platform diving cliff diving campaign, mountain stream bridge bungee jumping campaign, because a process that rises and land is arranged, has the longer hang time, can finish more action in the air, have more safety, pungency and sight, effect is better than high platform diving, cliff diving, the diving of mountain stream bridge or the bungee jumping of prior art, probably develops into global athletic competition project.
Carry the training of parachute kit ejection bailout: training goal: improve the trainee to the tolerance of acceleration/accel, be a large amount of outstanding carrier-borne aircraft aviator of aircraft carrier training, be airman, parachutist or the airborne technical ability of special war army personnel training, help the correct skilled parachute kit that uses of start-up, as civilian universal military sports campaign, can strengthen nationwide physical condition well, improve whole people's awareness of national defence.Be equivalent to parapenting, the steep cliff parachuting, the parachuting of mountain stream bridge, launch lift-off because use, a process that rises and land is arranged, has the longer hang time, the trainer can finish more action in the air, be added with perfect safety precaution facility outward, even parachute-opening error, the safe landing of also can fixing a point, can not cause casualties, so have more safety, pungency and sight, effect are better than the aircraft parachute jumping of prior art, high platform parachute jumping, the steep cliff parachute jumping, the parachute jumping of mountain stream bridge probably develops into global athletic competition project;
Designing requirement: be 30-50 rice with the cantilever beam design length, the elevation angle 45 degree, the skyscraper of employing more than 50-100 rice installed, launch weight 200-300 kilogram, ejection altitude 50-200 rice, with parabolic catapulting distance 200-300 rice, the safe landing protective equipment of 100-200 square meter is set below the point that lands;
Training patterns: the trainer wears parachute kit, take ejection-seat and launch lift-off, the parachute-opening success, the control parachute kit is being formulated the level point landing, if the parachute-opening error, just with parabolical mode parachuting to the safe landing protective equipment, after the landing, problem is found out in summing up experience, repetition training, (if adopt the aircraft mode to parachute, decided in case the parachute-opening error is just dead) till knowing skillfully.
Carry delta wing and launch flight training: training goal: improve the trainee to the tolerance of acceleration/accel, be a large amount of outstanding carrier-borne aircraft aviator of aircraft carrier training, be airman, parachutist or the special army's training special expertise of fighting, help the correct skilled delta wing aircraft that uses of start-up to carry out airflight, cultivate the special operations ability.As civilian universal military sports campaign, can strengthen nationwide physical condition well, improve whole people's awareness of national defence.Be equivalent to high mountain, steep cliff, the delta wing flight training of mountain stream bridge, lift-off is launched in use, not limited by geographical environment, ejection process has a process that rises and land, has the longer hang time, the trainer can enjoy the happy of airflight at any time easily, because perfect safety precaution facility is arranged, even flight error, the safe landing of yet can fixing a point can not cause casualties, so have more safety, pungency and sight, effect is better than the aircraft of prior art and throws in, high platform, hill top takeoff and, the jump start of mountain stream bridge probably develops into global athletic competition project;
Designing requirement: be 30-50 rice with the cantilever beam design length, the elevation angle 45 degree, the skyscraper of employing more than 50-100 rice installed, launch weight 200-300 kilogram, ejection altitude 50-200 rice, with parabolic catapulting distance 200-300 rice, the safe landing protective equipment of 100-200 square meter is set below the point that lands;
Training patterns: the trainer wears the delta wing aircraft, take ejection-seat and launch lift-off, fly successfully, the control delta wing is being specified the level point landing, if the flight error, just with parabolical mode parachuting to the safe landing protective equipment, after the landing, problem is found out in summing up experience, and repetition training is till skilled.
Wear wing dress clothes and launch flight training, training goal: carry out the wing dress sporting flying of China, break the restriction of world's wing dress flight geographical environment, such as the international wing dress demonstration flight of holding on mountain, Tianmen, Hunan in 2012, because there is the steep cliff of 1400 meters of sea level elevations on the mountain, Tianmen, the height above sea level of tai shan, famous tourist attraction: 1532.7 meters, why can not hold the flight of wing dress? because the one, the sporting flying of wing dress is not popularized, the 2nd, though there is height in Mount Taishan, slope, the south of the mountains has good level point again, but there is not vertical steep cliff, can not adorn the acceleration/accel that the aircrew provides free-falling body for the wing, if by ejection mode the training of protection ground is arranged, just can cultivate large quantities of wing dress sporting flying persons, if a cover ejector is set in the Peak of the Heavenly Emperor, Mount Taishan, provide flying height and flying speed by ejection mode for wing dress aircrew, will become possibility from the flight of Mount Taishan roof limb dress, if can hold the flight of international wing dress in Mount Taishan, will inevitably be to the tourist industry amount of providing in Mount Taishan and the tremendous increase of matter, certainly in each natural scenic spots with good conditionsi of the whole nation ejection trainer can be set, carry out wing dress flight training and performance, in addition, wing dress flight training effect militarily can not be despised;
Designing requirement: identical with embodiment 3, different is equipment can be installed on the high mountain summit, allow those possess sea level elevation and do not possess the high mountain sight spot of vertical dimension, also can become the township of the motion of parachute jumping, delta wing flight, powered paragliding and the flight of wing dress clothes;
Training patterns: give training in the training base that protective equipment is arranged earlier, by the low latitude to the high-altitude, the trainer wears wing dress clothes, takes ejection-seat and launches lift-off, and control wing dress clothes are being specified the level point landing, with parabolical mode parachuting to the safe landing protective equipment, by groping experience, repetition training is till the use that on top of wing dress is obeyed, everybody can both arrive and be arranged on launching of mountain top and carry out wing dress flight on the equipment at last, realizes the dream of freely circling in the air.
Except the disclosed technical characterictic of specification sheets of the present invention, be the known technology of those skilled in the art.
Claims (4)
1. a high-mobility, multipurpose, wheeled vehicle pneumatic type is launched airborne flight training device, it is characterized in that, the method that utilization is launched is launched the high-altitude with the trainer, the trainer utilizes the airborne flight training that self is equipped with to be equipped in the airborne or airflight training of aerial enforcement, or trainer's fixed point of carrying no luggage launched the basic training of parachuting on the safety precaution facility, this training aids comprises base, pneumatic catapult-launching gear, shape of a saddle ejection-seat, elevation angle adjuster and safe landing protective equipment, elevation angle adjuster and catapult-launching gear are arranged on the base, ejection-seat is arranged on the catapult-launching gear, the safe landing protective equipment is arranged on the point that lands, wherein:
Base is used for the fixed elevation adjuster, comprises movable base and firm banking, and movable base is car chassis, and firm banking is high-rise;
Pneumatics comprises accumulator unit, cantilever beam, launches cylinder, grooved track and launch dolly,
Accumulator unitBe arranged on the base, cantilever beam is made up of cantilever beam and grooved track, and two channel suspending rails are fixed on the both sides that section is the cantilever beam top of rectangle, launch cylinder and are arranged in the middle of the cantilever beam;
The two ends of cantilever beam are provided with pulley, be provided with piston among launching cylinder, the two ends of piston connect trailing cable, two trailing cables pass the through hole in the middle of the cylinder cover mid seal of launching the cylinder two ends respectively, walking around the pulley at cantilever beam two ends is connected with the dolly two ends of launching in being arranged on the grooved track, shape of a saddle ejection-seat is fixed on and launches on the dolly, the bottom of launching cylinder also is provided with total inlet pipe, the total inlet pipe two ends are connected with the two ends of launching cylinder with low side electromagnetic switch triple valve by high-end electromagnetic switch triple valve, two electromagnetic switch triple valves are connected with ejection controller on being arranged on base by the control cable, the low side of cantilever beam also is provided with counterweight and supports, total inlet pipe is connected with total air inlet electromagnetic valve on the accumulator unit by high pressure hose, and accumulator unit is connected with high-pressure pump;
Elevation angle adjuster is used for regulating the elevation angle between cantilever beam and the ground, its structure is by bracing frame, sliding sleeve vertical lift hydraulic actuating cylinder, C shape sliding sleeve and sliding sleeve horizontal drive hydraulic actuating cylinder are formed, wherein, the section of C shape sliding sleeve is C shape, C shape sliding sleeve is connected with the cantilever beam basal sliding, one end and the cantilever beam of sliding sleeve horizontal drive hydraulic actuating cylinder are fixed, the other end is connected with C shape sliding sleeve, the top of sliding sleeve vertical lift hydraulic actuating cylinder is by hinge and high-end connection of C shape sliding sleeve, the lower end of sliding sleeve vertical lift hydraulic actuating cylinder is connected with base by hinge, the bottom of bracing frame is connected with base, and the top of bracing frame is connected by the low side of twisted axis with C shape sliding sleeve;
The bottom of shape of a saddle ejection-seat is the shape of a saddle and rides on the cantilever beam, and the both sides, top of shape of a saddle ejection-seat are provided with handrail, and two of shape of a saddle type seat bottom is surveyed and also is provided with pedal;
Ejection controller comprises micro controller system, plays point sensor, end point sensor, is arranged on load cell and jettison push-button switch under the shape of a saddle ejection-seat, wherein, end point sensor is arranged on 1-3 rice high-end apart from cantilever beam, and a point sensor is arranged on 1 meter apart from the cantilever beam low side; High-end and two electromagnetic switch triple valves low side have been subjected to point sensor, end point sensor and jettison push-button switch interlock control.
2. training aids according to claim 1 is characterized in that, airborne flight training equipment comprises: parachute, delta wing aircraft, wing dress aircraft, fixed-wing aircraft.
3. training aids according to claim 1 is characterized in that, the safe landing protective equipment is made up of safety guard net and inflatable airbags, and safety guard net covers on inflatable airbags.
4. training aids according to claim 1 is characterized in that, the safe landing protective equipment is sand ground, bay, lake or pond.
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| CN 201320055580 CN203211515U (en) | 2013-01-31 | 2013-01-31 | Multipurpose pneumatic type ejection airborne flight training device |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116105780A (en) * | 2023-04-07 | 2023-05-12 | 江苏巨数智能科技有限公司 | Disposable sensor with pneumatic adjustment system |
-
2013
- 2013-01-31 CN CN 201320055580 patent/CN203211515U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116105780A (en) * | 2023-04-07 | 2023-05-12 | 江苏巨数智能科技有限公司 | Disposable sensor with pneumatic adjustment system |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130925 Termination date: 20140131 |