CN204275502U - Cableway remotely-piloted vehicle - Google Patents
Cableway remotely-piloted vehicle Download PDFInfo
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- CN204275502U CN204275502U CN201420552220.0U CN201420552220U CN204275502U CN 204275502 U CN204275502 U CN 204275502U CN 201420552220 U CN201420552220 U CN 201420552220U CN 204275502 U CN204275502 U CN 204275502U
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Abstract
The utility model relates to a kind of cableway remotely-piloted vehicle, be made up of cableway system, remotely-piloted vehicle, armful rope slip ring, suspension, in suspension, end connector is hinged with armful rope slip ring, lower end connector and remotely-piloted vehicle hinged, embrace rope slip ring and encircle cableway, remotely-piloted vehicle is suspended on cableway and flies.The utility model reasonable in design, have wide accommodation, safely and fast, small investment and the network of communication lines extensively can cover feature, be particularly useful for fast transportation with a varied topography, from far-off regions.
Description
Technical field
The utility model belongs to cableway technical field of transportation, especially cableway remotely-piloted vehicle.
Background technology
Cableway traffic: wirerope supports unsettled connection source and terminal by support, cable car locking is suspended on wirerope, and being moved by wirerope reaches transport object, or cable car sliding and running is between two fulcrums; Remotely-piloted vehicle: aircraft is aloft flown by remote control; Air transportation: utilize aircraft to carry out air transport; Electrified high-speed railway: utilize track and power transmission network, and automatically close up, moving block system, make bullet train reach high speed, safety, Effec-tive Function; Magnetic resonance wireless charging technology: convert electric energy to electromagnetic wave and send energy by coil, recipient accepts energy with same frequency resonance and is converted into electric energy, and the magnetic resonance charging electric car of Korean-made runs successfully; Quick cableway traffic system: by embracing rope slip ring, remotely-piloted vehicle being suspended on cableway, utilizing air push remotely-piloted vehicle high-speed cruising.
Cableway traffic weak point is that the cable car speed of service is slow, is unfavorable for the traffic of longer distance, or is only limited to high-speed cruising between two fulcrums; The shortcoming of electrified high-speed railway is because investing huge, therefore limits by geologic condition, economic benefit, can only do trunk design, and circuit can not extensively cover; The deficiency of air transportation is to need high standard airport, high standard human pilot, and large by weather effect, landing of taking off has excessive risk, is relatively applicable to overlength distance, high added value transport.
Utility model content
The purpose of this utility model is to overcome the deficiencies in the prior art, provide a kind of reasonable in design, applied widely, safely and fast, invest the little and remotely-piloted vehicle of stable performance.
Basic conception of the present utility model is: utilize the equipment such as an armful rope slip ring, suspension connecting rod to hang on cableway system by remotely-piloted vehicle, utilize the load-bearing of cableway system, track and Energy transfer performance, utilize and embrace the movement of rope slip ring on cableway, for remotely-piloted vehicle provides safe running way, reach the transport object of high speed, safety, cheapness, the extensive radiation of the network of communication lines.
The utility model solves its technical problem and takes following technical scheme to realize:
Based on the first technical scheme of same technical thought, cableway remotely-piloted vehicle, carry energy resource system by cableway system, remotely-piloted vehicle, aircraft, embrace rope slip ring, hang connecting rod and form, the upper gib head hanging connecting rod is hinged with link on armful rope slip ring, bearing on lower contact and carry-on engaging lug is coupling, embrace rope slip ring and encircle cableway wirerope, remotely-piloted vehicle is suspended on cableway, and aircraft is equipped with and carries energy resource system;
Cableway system in the first technical scheme corresponding, be made up of wirerope, pillar, armful cable ring, cantilever, platform, dead end anchor fixed rack, tensioning apparatus, control centre, embrace the slip of cable ring and encircle wirerope, embrace cable ring ear and pillar cantilever bolt, wirerope is suspended on cableway pillar, in two terminals of cableway, be provided with anchor supports, the assembly pulley of wirerope in anchor supports is connected with tensioning apparatus, below the cableway of anchoring post, be provided with platform, and control centre is located at the side of platform;
Based on same technical thought the second technical scheme, cableway remotely-piloted vehicle, by cableway system, electromagnetic wave coil, magnetic resonance generator, electromagnetic wave receiving equipment, remotely-piloted vehicle, embrace rope slip ring, suspension connecting rod is formed, embrace rope slip ring and encircle cableway wirerope, hang gib head on connecting rod hinged with link on armful rope slip ring, bearing on lower contact and remotely-piloted vehicle engaging lug is coupling, remotely-piloted vehicle is suspended on cableway, magnetic resonance generator to be arranged in cableway control centre and to be connected with electromagnetic wave coil, electromagnetic wave coil and cableway wirerope one and be positioned at immediately below wirerope, electromagnetic wave receiving equipment is installed on the inside of remotely-piloted vehicle, be connected with the sustainer of aircraft by wire,
Cableway system in the second technical scheme, be made up of wirerope, pillar, cantilever, armful cable ring, armful cable ring ear, platform, dead end anchor fixed rack, tensioning apparatus, control centre, electromagnetic wave coil, electromagnetic wave coil is arranged at immediately below wirerope, embrace the slip of cable ring and encircle wirerope, embrace cable ring ear and cantilever bolt, wirerope is suspended on cableway pillar, in two terminals of cableway, be provided with anchor supports, the assembly pulley of wirerope in anchor supports is connected with tensioning apparatus, be provided with platform close to below the cableway of anchor supports, control centre is located at platform side;
Based on the third technical scheme of same technical thought, cableway remotely-piloted vehicle, by cableway system, remotely-piloted vehicle, power supply, wire, airborne by electric system, elastic brush, cross-arm bar, embrace rope slip ring, suspension connecting rod is formed, embrace rope slip ring and encircle cableway wirerope, embrace between rope slip ring for two and be located by connecting by cross-arm bar, hang gib head and cross-arm bar on connecting rod hinged, bearing on lower contact and remotely-piloted vehicle engaging lug is coupling, remotely-piloted vehicle is suspended on cableway, cableway wirerope is made up of two steel combined with aluminum wireropes, power supply is connected with compound wirerope by wire, four elastic brush Jue Yuan Gu Installed are in embracing in rope slip ring diagonal positions, elastic brush and wirerope slidingly contact, just, negative the two poles of the earth brush is connected by electric system with airborne respectively by wire, be connected with sustainer by wire by electric system,
Cableway system in the third technical scheme is by a pair compound wirerope, pillar, insulator, embrace cable ring, embrace cable ring ear, platform, dead end anchor fixed rack, tensioning apparatus, control centre, connecting circuit is formed, a pair wirerope is by steel, aluminium compound is made, embrace cable ring and encircle wirerope, embrace cable ring ear and insulator bolt, insulator and pillar cantilever bolt, wirerope is suspended on cableway pillar, in two terminals of cableway, be provided with anchor supports, the assembly pulley of wirerope insulation in anchor supports is connected with tensioning apparatus, platform is being provided with close to below the cableway of anchoring post, control centre is located at platform side, power supply is connected with wirerope by wire,
Remotely-piloted vehicle described in above-mentioned three kinds of technical schemes, by sustainer, main wing, empennage, vertical tail, video system, instrument room, engaging lug, lower hanger, freight house, engaging lug bearing, girder, airborne energy resource system or magnetic resonance accept system or are subject to electric system, aileron, hydroplane, rudder, optical registration instrument, airborne signal transmitting system, airborne signal accepts control system, throttle motor, onboard instrument battery, aileron controls motor, hydroplane controls motor, rudder controls motor, aircraft road wheel, manual remote control emission system, ground signal accepts system composition, sustainer, main wing, empennage, vertical tail is installed on body, aileron is equipped with at main wing rear, hydroplane is equipped with at empennage rear, rudder is equipped with at vertical tail rear, before and after the through body of girder, engaging lug is installed in gravity balance point above aircraft body girder, engaging lug is equipped with bearing, video system is arranged on the dead ahead of instrument room, and lower hanger is arranged on the lower abdomen place of aircraft, below body, also road wheel is housed, freight house is provided with in fuselage, airborne energy resource system or magnetic resonance accept system or are installed in body by electric system, and instrument room is located at above body, optical registration instrument, airborne signal transmitting system, airborne signal accepts control system, throttle motor, onboard instrument battery, aileron controls motor, hydroplane controls motor, rudder controls motor and is arranged in instrument room, and airborne Signal reception control system receives the signal instruction of artificial remote control launching system, by throttle motor, aileron controls motor, hydroplane controls motor, rudder controls motor and controls sustainer throttle or size of current and aileron respectively, hydroplane, rudder angle, laser alignment instrument, video system is all connected with airborne signal transmitting system, by signal transmitting system, information data is passed back ground signal receiving system, and according to the information data received, manual remote control emission system transmits and controls aircraft flight state.
Described embraces cable ring, be made up of an armful cable ring, armful cable ring ear, armful cable ring teeth groove, screw hole, reflecting strips, two symmetrical semi-rings all with ring ear integrally, teeth groove is provided with two semi-ring junctions, above ring ear, symmetry has screw hole, two semi-ring bolts are fixed as integral loop, are provided with reflecting strips in the both side surface of ring ear;
Embrace rope slip ring to be made up of main ring body, main ring breach, roller, engaging lug, gim peg, coupling bar, generating laser, main ring body is the square that symmetrical halves docking is formed, breach is had directly over main ring, engaging lug is provided with immediately below main ring, gim peg runs through engaging lug, coupling bar is coupling engaging lug and link, and roller is that axle is packed on four limits of main ring with main ring, and generating laser is packed in by main ring breach;
Hang connecting rod, be made up of upper hookhead, anticreep languid, connecting rod, elastic rotary joint, lower contact, connecting rod upper end is provided with eave tile, and eave tile indentation, there is provided with anticreep languid, and connecting rod and lower contact save hinged by elastic rotary;
Advantage of the present utility model and beneficial effect are:
The utility model reasonable in design, have wide accommodation, safely and fast, small investment and the network of communication lines extensively can cover feature, be particularly useful for rapid transit with a varied topography, from far-off regions transport.
Accompanying drawing explanation
Fig. 1 is front view of the present utility model.
Fig. 2 is the A direction view of technical scheme one.
Fig. 3 is the A direction view of technical scheme two.
Fig. 4 is the A direction view of technical scheme three.
Fig. 5 is the plane figure schematic diagram of technical scheme one.
Fig. 6 is the plane figure schematic diagram of technical scheme two.
Fig. 7 is the plane figure schematic diagram of technical scheme three.
Fig. 8 is technical scheme two wirerope and electromagnetic antenna layout schematic cross-section.
Fig. 9 is the topology view embracing cable ring.
Figure 10 is the A direction view embracing cable ring.
Figure 11 is that upper and lower varied angle embraces cable ring.
Figure 12 is that flat bank embraces cable ring.
Figure 13 is the aircraft cross section schematic diagram that the first technical scheme uses.
Figure 14 is the aircraft cross section schematic diagram that the second technical scheme uses.
Figure 15 is the aircraft cross section schematic diagram that the third technical scheme uses.
Figure 16 is aircraft instrument room plane figure schematic diagram.
Figure 17 embraces the first technical scheme front view of rope slip ring.
Figure 18 embraces rope slip ring the second technical scheme front view.
Detailed description of the invention
Below in conjunction with accompanying drawing, utility model embodiment is further described:
Based on the first technical scheme of same technical thought, cableway remotely-piloted vehicle, carry energy resource system 2-12 by cableway system 1, remotely-piloted vehicle 2, aircraft, embrace rope slip ring 3, hang connecting rod 4 and form, the upper gib head 4-3 hanging connecting rod 4 is hinged with the engaging lug 3-6 embracing rope slip ring 3, bearing 2-10 on engaging lug 2-7 on lower contact 4-5 and aircraft 2 is coupling, embrace rope slip ring and encircle cableway wirerope 1-1, remotely-piloted vehicle is suspended on cableway 1, and aircraft is equipped with and carries energy resource system 2-12;
Cableway system in the first technical scheme corresponding, by wirerope 1-1, pillar 1-2, embrace cable ring 1-3, cantilever 1-10, platform 1-16, dead end anchor fixed rack 1-11, tensioning apparatus 1-12, control centre 1-15 is formed, embrace cable ring 1-3 slip and encircle wirerope 1-1, embrace cable ring ear 1-4 and pillar cantilever 1-10 bolt, wirerope is suspended on cableway pillar 1-2, in two terminals of cableway, be provided with anchor supports 1-11, the assembly pulley of wirerope in anchor supports is connected with tensioning apparatus 1-12, platform 1-16 is provided with below the cableway of anchoring post, control centre 1-15 is located at the side of platform,
Aircraft in the first scheme, using internal combustion engine or motor as power, carries fuel or battery equal energy source runs at random;
Based on same technical thought the second technical scheme, cableway remotely-piloted vehicle, by cableway system 1, electromagnetic wave coil 1-9, magnetic resonance generator 1-14, electromagnetic wave receiving equipment 2-27, remotely-piloted vehicle 2, embrace rope slip ring 3, hang connecting rod 4 to form, embrace rope slip ring 3 and encircle cableway wirerope 1-1, hang gib head 4-3 on connecting rod hinged with armful rope slip ring engaging lug 3-6, bearing 2-10 on lower contact 4-5 and remotely-piloted vehicle engaging lug 2-7 is coupling, remotely-piloted vehicle is suspended on cableway, magnetic resonance generator 1-14 to be arranged in cableway control centre 1-15 and to be connected with electromagnetic wave coil 1-9, electromagnetic wave coil and cableway wirerope 1-1 one and be positioned at immediately below wirerope, electromagnetic wave receiving equipment 2-27 is installed on the inside of remotely-piloted vehicle 2, by the sustainer 2-1 of wire and aircraft,
Cableway system in the second technical scheme, by wirerope 1-1, pillar 1-2, cantilever 1-10, embrace cable ring 1-3, embrace cable ring ear 1-4, platform 1-16, dead end anchor fixed rack 1-11, tensioning apparatus 1-12, control centre 1-15, electromagnetic wave coil 1-9 is formed, electromagnetic wave coil 1-9 is arranged at immediately below wirerope 1-1, embrace cable ring 1-3 slip and encircle wirerope, embrace cable ring ear 1-4 and cantilever 1-10 bolt, wirerope is suspended on cableway pillar 1-2, in two terminals of cableway, be provided with anchor supports 1-11, the assembly pulley of wirerope in anchor supports is connected with tensioning apparatus 1-12, platform 1-16 is being provided with close to below the cableway of anchor supports, control centre 1-15 is located at platform side,
In first scheme, the energy needed for aircraft, accepts the electromagnetic wave launched by magnetic resonance generator in electromagnetic wave coil below system acquisition wirerope by airborne nuclear magnetic resonance, and converts the running of electrical energy drive sustainer to;
Based on the third technical scheme of same technical thought, cableway remotely-piloted vehicle, by cableway system 1, remotely-piloted vehicle 2, power supply 1-17, wire 1-13, airborne by electric system 2-28, elastic brush 3-10, cross-arm bar 3-9, embrace rope slip ring 3, hang connecting rod 4 to form, embrace rope slip ring 3 and encircle cableway wirerope 1-1, embrace between rope slip ring for two and be located by connecting by cross-arm bar 3-9, hang gib head 4-3 and cross-arm bar on connecting rod hinged, bearing 2-10 on lower contact 4-5 and remotely-piloted vehicle engaging lug 2-7 is coupling, remotely-piloted vehicle 2 is suspended on cableway, cableway wirerope 1-1 is made up of two steel combined with aluminum wireropes, power supply 1-17 is connected with compound wirerope by wire 1-13, four elastic brush 3-10 Jue Yuan Gu Installed are in embracing in rope slip ring diagonal positions, elastic brush and wirerope slidingly contact, just, negative the two poles of the earth brush is connected by electric system with airborne respectively by wire, be connected with sustainer 2-1 by wire by electric system 2-28,
Cableway system in the third technical scheme is by a pair compound wirerope 1-1, pillar 1-2, insulator 1-8, embrace cable ring 1-3, embrace cable ring ear 1-4, platform 1-16, dead end anchor fixed rack 1-11, tensioning apparatus 1-12, control centre 1-15, connecting circuit 1-13 is formed, it is characterized in that: a pair wirerope is by steel, aluminium compound is made, embrace cable ring 3 and encircle wirerope 1-1, embrace cable ring ear 1-4 and insulator 1-8 bolt, insulator 1-8 and pillar cantilever 1-10 bolt, wirerope is suspended on cableway pillar 1-2, in two terminals of cableway, be provided with anchor supports 1-11, the assembly pulley of wirerope insulation in anchor supports is connected with tensioning apparatus 1-12, platform 1-16 is being provided with close to below the cableway of anchoring post, control centre 1-15 is located at platform side, power supply 1-17 is connected with wirerope by wire 1-13,
In the third scheme, power supply is transmitted by a pair steel combined with aluminum wirerope, article two, positive and negative electrode circuit function born respectively by wirerope, bear load-carrying function simultaneously, for aircraft provides suspension strut, elastic brush obtained from cable positive pole current transitions delivery of electrical energy needed for engine by electric system and, to engine, and form loop by elastic brush and cable negative pole;
Elastic brush is arranged on embraces rope slip ring four diagonal positions, with compound wirerope Elastic Contact, guarantees the continuity contacted;
Remotely-piloted vehicle described in above-mentioned three kinds of technical schemes, by sustainer 2-1, main wing 2-2, empennage 2-3, vertical tail 2-4, video system 2-5, instrument room 2-6, engaging lug 2-7, lower hanger 2-8, freight house 2-9, engaging lug bearing 2-10, girder 2-11, airborne energy resource system 2-12 or magnetic resonance accept system 2-27 or are subject to electric system 2-28, aileron 2-13, hydroplane 2-14, rudder 2-15, optical registration instrument 2-16, airborne signal transmitting system 2-17, airborne signal accepts control system 2-18, throttle motor 2-19, onboard instrument battery 2-20, aileron controls motor 2-21, hydroplane controls motor 2-22, rudder controls motor 2-23, aircraft road wheel 2-24, manual remote control emission system 2-25, ground signal accepts system 2-26 composition, sustainer 2-1, main wing 2-2, empennage 2-3, vertical tail 2-4 is installed on body, aileron is equipped with at main wing rear, hydroplane is equipped with at empennage rear, rudder is equipped with at vertical tail rear, before and after the through body of girder 2-11, engaging lug 2-7 is installed in gravity balance point above aircraft body girder, engaging lug is equipped with bearing 2-10, video system 2-5 is arranged on the dead ahead of instrument room 2-6, and lower hanger 2-8 is arranged on the lower abdomen place of aircraft, below body, road wheel 2-24 is also housed, freight house 2-9 is provided with in fuselage, airborne energy resource system 2-12 or magnetic resonance accept system 2-27 or are installed in body by electric system 2-28, and instrument room is located at above body, optical registration instrument 2-16, airborne signal transmitting system 2-17, airborne signal accepts control system 2-18, throttle motor 2-19, onboard instrument battery 2-20, aileron controls motor 2-21, hydroplane controls motor 2-22, rudder controls motor 2-23 and is arranged in instrument room, and airborne Signal reception control system receives the signal instruction of artificial remote control launching system, by throttle motor, aileron controls motor, hydroplane controls motor, rudder controls motor and controls sustainer throttle or size of current and aileron respectively, hydroplane, rudder angle, laser alignment instrument, video system is all connected with airborne signal transmitting system, by signal transmitting system, information data is passed back ground signal receiving system 2-26, and according to the information data received, manual remote control emission system transmits and controls aircraft flight state.
Described embraces cable ring 3, be divided into craspedodrome, height varied angle, flat bank three kinds, cross section resembles two band handle semicircles, docking teeth groove bolt is fixed into entirety, by embracing a cable ring 1-3, embrace cable ring ear 1-4, embrace cable ring teeth groove 1-5, screw hole 1-6, reflecting strips 1-7 form, two symmetrical semi-rings all with ring ear integrally, teeth groove 1-5 is provided with two semi-ring junctions, above ring ear, symmetry has screw hole 1-6, and two semi-ring bolts are fixed as integral loop, are provided with reflecting strips 1-7 in the both side surface of ring ear;
Embracing cable ring and move towards needs according to cableway, move towards section in level and use craspedodrome ring, being moved towards by level to use height varied angle ring when moving towards to become to height, using turning ring at flat bank place;
Embrace rope slip ring by main ring body 3-1, main ring breach 3-3, roller 3-2, engaging lug 3-6, gim peg 3-4, coupling bar 3-5, generating laser 3-7, link 3-8 is formed, main ring body 3-1 is the square that symmetrical halves docking is formed, breach 3-3 is had directly over main ring, engaging lug 3-6 is provided with immediately below main ring, gim peg 3-4 runs through engaging lug, coupling bar 3-5 is coupling engaging lug and link 3-8, link is for being connected with gib head on suspension connecting rod, roller 3-2 with main ring 3-1 for axle is packed on four limits of main ring, generating laser 3-7 is packed in by main ring 3-3 breach,
Embrace rope slip ring be used for load-carrying larger time, main ring body diameter is comparatively thick, the connection between each limit, the modes such as available plug-bolt is fixed, screw thread is fixed, welding;
When the light aircraft of suspended weights or analogue formation toy, embrace a rope slip ring main ring body and can be whole piece steel bar, breach has the elastic force opened to both sides;
Hang connecting rod 4, saved 4-2, lower contact 4-5 formed by upper hookhead 4-3, anticreep languid 4-4, connecting rod 4-1, elastic rotary, it is characterized in that connecting rod upper end is provided with eave tile, eave tile indentation, there is provided with anticreep languid, connecting rod and lower contact save hinged by elastic rotary, anticreep languid is used for locking gib head, anti-locking hook;
Generating laser is by embracing reflecting strips on cable ring ear to beam reflection, signal is sent to airborne laser aligner, and pass the signal to ground signal by airborne signal transmitting system and accept system 2-26, ground system is according to the information received, transmitted by manual remote control system 2-25 and control aircraft flight attitude, reach main ring breach and aim at object with an armful cable ring;
The effect of screen system 2-5 is real-time Transmission flight environment of vehicle state, is convenient to ground remote control and controls;
Embrace rope slip ring roller and wirerope Structure deformation, the cross section that root edge line is formed is greater than cableway wirerope cross section, along with aircraft rises and falls, cableway wirerope contacts possibility with armful each roller of rope slip ring, even exist of short duration contactless, therefore can reducing friction resistance, embrace rope slip ring to hang on cableway, unload, when aircraft is hanging on cableway wirerope, close up concavo-convex for the occlusion of two semi-rings, fix with gim peg, be engaged that concavo-convex can main ring to be made to close post-equalization stressed, coupling bar is used for embracing rope slip ring and hanging the hinged of connecting rod, can unload embracing rope slip ring from cableway when unclamping gim peg, aircraft can at ground run,
Hang the elastic rotary joint of connecting rod, damping effect can be played on the one hand, possesses spinfunction in the horizontal direction on the other hand, the bearing hung on the lower contact of connecting rod and aircraft on engaging lug is coupling, flying instrument can be made standby to bow, elevation angle degree, hang the safe distance that connecting rod can also keep remotely-piloted vehicle and wirerope and ground;
Cableway wirerope is suspended on cableway pillar by embracing cable ring, and embracing cable ring edge is that streamlined, flat, smooth ring ear just passes through relatively from embracing cable slip ring breach central authorities;
Cableway between two anchor supports is an anchor section, and the cableway of overlength can be formed by the linking of several anchor sections;
Platform is used for aircraft stop, different anchor section space transition;
Cableway system of the present utility model also can carry piloted vehicle, and the technical solution of the utility model can become model, is made into toy by micro;
It is emphasized that; embodiment described in the utility model is illustrative; instead of it is determinate; therefore the utility model is not limited to the embodiment described in detailed description of the invention; every other embodiments drawn according to the technical solution of the utility model by those skilled in the art, belong to the scope of the utility model protection equally.
Claims (10)
1. a cableway remotely-piloted vehicle, carry energy resource system by cableway system, remotely-piloted vehicle, aircraft, embrace rope slip ring, hang connecting rod and form, it is characterized in that: the upper gib head hanging connecting rod is hinged with link on armful rope slip ring, bearing on lower contact and carry-on engaging lug is coupling, embrace rope slip ring and encircle cableway wirerope, remotely-piloted vehicle is suspended on cableway, and aircraft is equipped with and carries energy resource system.
2. a cableway remotely-piloted vehicle, by cableway system, electromagnetic wave coil, magnetic resonance generator, electromagnetic wave receiving equipment, remotely-piloted vehicle, embrace rope slip ring, suspension connecting rod is formed, it is characterized in that: embrace rope slip ring and encircle cableway wirerope, hang gib head on connecting rod hinged with link on armful rope slip ring, bearing on lower contact and remotely-piloted vehicle engaging lug is coupling, remotely-piloted vehicle is suspended on cableway, magnetic resonance generator to be arranged in cableway control centre and to be connected with electromagnetic wave coil, electromagnetic wave coil and cableway wirerope one and be positioned at immediately below wirerope, electromagnetic wave receiving equipment is installed on the inside of remotely-piloted vehicle, be connected with the sustainer of aircraft by wire.
3. a cableway remotely-piloted vehicle, by cableway system, remotely-piloted vehicle, power supply, wire, airborne by electric system, elastic brush, cross-arm bar, embrace rope slip ring, suspension connecting rod is formed, it is characterized in that: embrace rope slip ring and encircle cableway wirerope, embrace between rope slip ring for two and be located by connecting by cross-arm bar, hang gib head and cross-arm bar on connecting rod hinged, bearing on lower contact and remotely-piloted vehicle engaging lug is coupling, remotely-piloted vehicle is suspended on cableway, cableway wirerope is made up of two steel combined with aluminum wireropes, power supply is connected with compound wirerope by wire, four elastic brush Jue Yuan Gu Installed are in embracing in rope slip ring diagonal positions, elastic brush and wirerope slidingly contact, just, negative the two poles of the earth brush is connected by electric system with airborne respectively by wire, be connected with sustainer by wire by electric system.
4. cableway remotely-piloted vehicle according to claim 1, described cableway system, be made up of wirerope, pillar, armful cable ring, cantilever, platform, dead end anchor fixed rack, tensioning apparatus, control centre, it is characterized in that: embrace the slip of cable ring and encircle wirerope, embrace cable ring ear and pillar cantilever bolt, wirerope is suspended on cableway pillar, in two terminals of cableway, be provided with anchor supports, the assembly pulley of wirerope in anchor supports is connected with tensioning apparatus, below the cableway of anchoring post, be provided with platform, control centre is located at the side of platform.
5. cableway remotely-piloted vehicle according to claim 2, described cableway system, by wirerope, pillar, cantilever, embrace cable ring, embrace cable ring ear, platform, dead end anchor fixed rack, tensioning apparatus, control centre, electromagnetic wave coil is formed, it is characterized in that: electromagnetic wave coil is arranged at immediately below wirerope, embrace the slip of cable ring and encircle wirerope, embrace cable ring ear and cantilever bolt, wirerope is suspended on cableway pillar, in two terminals of cableway, be provided with anchor supports, the assembly pulley of wirerope in anchor supports is connected with tensioning apparatus, platform is being provided with close to below the cableway of anchor supports, control centre is located at platform side.
6. cableway remotely-piloted vehicle according to claim 3, described cableway system, by a pair compound wirerope, pillar, insulator, embrace cable ring, embrace cable ring ear, platform, dead end anchor fixed rack, tensioning apparatus, control centre, connecting circuit is formed, it is characterized in that: a pair wirerope is by steel, aluminium compound is made, embrace cable ring and encircle wirerope, embrace cable ring ear and insulator bolt, insulator and pillar cantilever bolt, wirerope is suspended on cableway pillar, in two terminals of cableway, be provided with anchor supports, the assembly pulley of wirerope insulation in anchor supports is connected with tensioning apparatus, platform is being provided with close to below the cableway of anchoring post, control centre is located at platform side, power supply is connected with wirerope by wire.
7. according to claim 1, cableway remotely-piloted vehicle described in 2 or 3, described remotely-piloted vehicle is by sustainer, main wing, empennage, vertical tail, video system, instrument room, engaging lug, lower hanger, freight house, engaging lug bearing, girder, airborne energy resource system or magnetic resonance accept system or are subject to electric system, aileron, hydroplane, rudder, optical registration instrument, airborne signal transmitting system, airborne signal accepts control system, throttle motor, onboard instrument battery, aileron controls motor, hydroplane controls motor, rudder controls motor, aircraft road wheel, manual remote control emission system, ground signal accepts system composition, it is characterized in that: sustainer, main wing, empennage, vertical tail is installed on body, aileron is equipped with at main wing rear, hydroplane is equipped with at empennage rear, rudder is equipped with at vertical tail rear, before and after the through body of girder, engaging lug is installed in gravity balance point above aircraft body girder, engaging lug is equipped with bearing, video system is arranged on the dead ahead of instrument room, and lower hanger is arranged on the lower abdomen place of aircraft, below body, also road wheel is housed, freight house is provided with in fuselage, airborne energy resource system or magnetic resonance accept system or are installed in body by electric system, and instrument room is located at above body, optical registration instrument, airborne signal transmitting system, airborne signal accepts control system, throttle motor, onboard instrument battery, aileron controls motor, hydroplane controls motor, rudder controls motor and is arranged in instrument room, and airborne Signal reception control system receives the signal instruction of artificial remote control launching system, by throttle motor, aileron controls motor, hydroplane controls motor, rudder controls motor and controls sustainer throttle or size of current and aileron respectively, hydroplane, rudder angle, laser alignment instrument, video system is all connected with airborne signal transmitting system, by signal transmitting system, information data is passed back ground signal receiving system, and according to the information data received, manual remote control emission system transmits and controls aircraft flight state.
8. the cableway remotely-piloted vehicle according to claim 4,5 or 6, described embraces cable ring, be made up of an armful cable ring, armful cable ring ear, armful cable ring teeth groove, screw hole, reflecting strips, it is characterized in that: two symmetrical semi-rings all with ring ear integrally, teeth groove is provided with two semi-ring junctions, above ring ear, symmetry has screw hole, and two semi-ring bolts are fixed as integral loop, are provided with reflecting strips in the both side surface of ring ear.
9. the cableway remotely-piloted vehicle according to claim 1,2 or 3, described embraces rope slip ring, be made up of main ring body, main ring breach, roller, engaging lug, gim peg, coupling bar, generating laser, link, it is characterized in that: main ring body is the square that symmetrical halves docking is formed, breach is had directly over main ring, engaging lug is provided with immediately below main ring, gim peg runs through engaging lug, coupling bar is coupling engaging lug and link, roller is that axle is packed on four limits of main ring with main ring body, and generating laser is packed in by main ring breach.
10. the cableway remotely-piloted vehicle according to claim 1,2 or 3, described suspension connecting rod, be made up of upper hookhead, anticreep languid, connecting rod, elastic rotary joint, lower contact, it is characterized in that connecting rod upper end is provided with eave tile, eave tile indentation, there is provided with anticreep languid, and connecting rod and lower contact save hinged by elastic rotary.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420552220.0U CN204275502U (en) | 2014-09-24 | 2014-09-24 | Cableway remotely-piloted vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420552220.0U CN204275502U (en) | 2014-09-24 | 2014-09-24 | Cableway remotely-piloted vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN204275502U true CN204275502U (en) | 2015-04-22 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420552220.0U Expired - Fee Related CN204275502U (en) | 2014-09-24 | 2014-09-24 | Cableway remotely-piloted vehicle |
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| Country | Link |
|---|---|
| CN (1) | CN204275502U (en) |
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- 2014-09-24 CN CN201420552220.0U patent/CN204275502U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150422 Termination date: 20170924 |