CN106081077A - A kind of can the shockproof flight instruments of multiple-effect of flying for long time - Google Patents

A kind of can the shockproof flight instruments of multiple-effect of flying for long time Download PDF

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Publication number
CN106081077A
CN106081077A CN201610706090.5A CN201610706090A CN106081077A CN 106081077 A CN106081077 A CN 106081077A CN 201610706090 A CN201610706090 A CN 201610706090A CN 106081077 A CN106081077 A CN 106081077A
Authority
CN
China
Prior art keywords
foot rest
bracing frame
aircraft
straight tube
additionally
Prior art date
Application number
CN201610706090.5A
Other languages
Chinese (zh)
Inventor
陈建霖
Original Assignee
成都翼高九天科技有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 成都翼高九天科技有限公司 filed Critical 成都翼高九天科技有限公司
Priority to CN201610706090.5A priority Critical patent/CN106081077A/en
Publication of CN106081077A publication Critical patent/CN106081077A/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by the ground or like engaging elements
    • B64C25/58Arrangements or adaptations of shock-absorbers or springs
    • B64C25/62Spring shock-absorbers; Springs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/08Helicopters with two or more rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02Aircraft characterised by the type or position of power plant
    • B64D27/24Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00Aircraft indicators or protectors not otherwise provided for
    • B64D45/04Landing aids; Safety measures to prevent collision with earth's surface
    • B64D45/06Landing aids; Safety measures to prevent collision with earth's surface mechanical
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • B64D47/08Arrangements of cameras
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Abstract

The invention discloses a kind of can the shockproof flight instruments of multiple-effect of flying for long time, including aircraft body, connecting on aircraft body has two to land foot rest, each foot rest that lands includes that two support straight tube and a bracing frame, are provided with a damping spring between each support straight tube and bracing frame;Damping straight tube it is additionally provided with inside damping spring;Also including that extends a foot rest on foot rest each landing, described prolongation foot rest is fixed on bracing frame by two buckles;Landing at two and be additionally provided with a guard rail between foot rest, the two ends of guard rail are connected with two bracing frames landed on foot rest respectively;Aircraft body is additionally provided with a solar battery sheet.Advantages of the present invention: solve land vibrations bring photographic head, The Cloud Terrace and land foot rest easily collide with damage problem;Solve land foot rest be weak to mill and be easily damaged when landing, aircraft can not maintain the problems such as flying for long time.

Description

A kind of can the shockproof flight instruments of multiple-effect of flying for long time
Technical field
The present invention relates to minute vehicle field, relate in particular to a kind of can the multiple-effect of flying for long time shockproof flight dress Put.
Background technology
Minute vehicle receives much attention owing to having special purposes.One important application is military surveillance, is equipped with To soldier class, carry out enemy's situation scouting and supervision.Can be additionally used in war danger estimation, target search, communication relay, monitoring chemistry, Nuclear or biological weapons, scouts interior of building situation.It is applicable to the multiple war environment such as city, jungle.Because it is easy to take Band, simple to operate, advantage that safety is good, can equip in a large number in army.In non-military field, it is configured with respective sensor Minute vehicle can be used to search disaster survivor, toxic gas or chemical substance source, eliminate crop pests etc..In reality In the life of border, the minute vehicle with photography function uses the most universal, but this minute vehicle land foot rest one As be made up of rigid, hard plastics or rustless steel, material is harder, the most wear-resisting, yielding, when landing, lands foot rest, photographic head Very big with the concussion impact that The Cloud Terrace is subject to, damage of easily being collided with.Even if landing on smooth ground, always can exist and taking the photograph The unclear problem of picture shot when landing as head.It addition, existing minute vehicle typically uses battery to power, at any time May not have electricity, cause aircraft can not maintain flying for long time, use dry cell power supply to be unfavorable for environmental conservation, wave simultaneously yet Take the energy.
Summary of the invention
It is an object of the invention to provide a kind of can the shockproof flight instruments of multiple-effect of flying for long time, solve existing miniature Aircraft when landing, the foot rest that lands be easily subject to impact and damage, and land foot rest be weak to mill problem;Solve existing When minute vehicle falls on uneven ground, the photographic head of minute vehicle and The Cloud Terrace easily collide with damage, the picture of shooting Face is ambiguous problem because being given a shock;Solve existing minute vehicle can not automatic power, cause the aircraft can not Maintain flying for long time, change battery trouble, the waste energy, the most durable problem.
The present invention is achieved through the following technical solutions:
A kind of can the shockproof flight instruments of multiple-effect of flying for long time, including aircraft body, aircraft body connects and has two The individual foot rest that lands, each foot rest that lands includes that two support straight tube and a bracing frame, are provided with two on each bracing frame (3) Individual slotted eye, is provided with a damping spring between each support straight tube and bracing frame;One end of described damping spring and support Straight tube is fixed, and the other end is fixed with bracing frame;Inside damping spring, be additionally provided with damping straight tube, one end of damping straight tube with Support is fixed, and the other end is placed in inside support straight tube;Also include that one extends foot rest, described prolongation foot on foot rest each landing Frame is fixed on bracing frame by two buckles;
Landing at two and be additionally provided with a guard rail between foot rest, what the two ends of guard rail were landed on foot rest with two respectively props up Support connects;Described guard rail be one by the bar pad having certain thickness rubber to make, be provided with at the two ends of guard rail Groove, the notch size of groove and the shaft diameter matches of bracing frame;Each groove is additionally provided with two circular holes, described circle The diameter in hole is equal with the diameter of slotted eye on bracing frame, uses the mode that screw bolt and nut is connected by guard rail It is fixed on bracing frame;
Aircraft body is additionally provided with a solar battery sheet, solar battery sheet and the charging within aircraft body Battery connects;Described solar battery sheet is positioned at the top of aircraft body, uses the mode that draw-in groove connects by solaode Sheet is fixed on aircraft body.
Further, arranging a damping straight tube inside damping spring, one end of damping straight tube is fixed with bracing frame, subtracts One end and the bracing frame of shake straight tube are fixing has been a supporting role, it is to avoid damping spring bending shifts, and causes landing foot rest Deformation.Additionally the other end of damping straight tube be placed in support straight tube inside, when designing simultaneously, it is desirable to damping straight tube not with support straight tube Being connected and also have a certain distance with supporting straight tube, such damping straight tube can move along with the compression of damping spring and past Support straight tube is internal mobile.Flight controller has constant weight, so flight controller is when landing, is positioned on flight controller The foot rest that lands can produce an active force over the ground, meanwhile, landing foot rest also can be by the opposition on ground.Because being subject to To the opposition on ground, the damping spring on foot rest that lands will be produced a thrust by compression, and damping spring produces The opposition on thrust and ground can be cancelled out each other, meanwhile, be placed in support one end of the damping straight tube within straight tube can be along with The compression of damping spring and more probe into inside support straight tube.The damping spring and the damping straight tube that arrange on foot rest solve existing Minute vehicle when landing, the foot rest that lands be easily subject to impact and damage, and land foot rest be weak to mill problem.
Also include that extends a foot rest on foot rest each landing, one prolongation foot rest is fixed on by two buckles Add on support and land the height of foot rest, both can ensure that the original-pack foot rest that lands was not dirty, and be not scraped off, fall can be reduced again The probability that camera lens when falling, The Cloud Terrace are injured.
Landing at two and arrange a guard rail between foot rest, guard rail is had certain thickness rubber blanket to make by one, For example with synthetic rubber.The top view of guard rail is a rectangle, and the width of guard rail can be with more slightly wider, as far as possible will shooting Head base and The Cloud Terrace surround, and when falling rough local time, the effect of camera head protecting can be more preferably.The two ends of guard rail are recessed Groove, groove has two apertures, is stuck on bracing frame by groove, and bolt passes aperture, uses nut by guard rail and bracing frame Fix.
Being additionally provided with inverter and transformator in aircraft body, solar battery sheet is arranged on the top of aircraft body Portion can be conducive to shining upon, in order to obtains luminous energy.The principle that solar battery sheet is powered is: solar irradiation is at quasiconductor P- N ties, and forms new hole-electron pair, and under the effect of P-N junction electric field, hole is flowed to P district by N district, and electronics is flowed to N by P district District, is formed for electric current after connecting circuit.The electric current that solaode produces is unidirectional current, and unidirectional current is transformed into after inverter Alternating current, then the voltage of the alternating current transmitted by inverter through transformator drops in the rechargeable battery range of nominal tension, then It is transmitted further to rechargeable battery.Using solar energy is that aircraft is powered, and solving existing minute vehicle can not automatic power, more Change battery trouble, the waste energy, the most durable problem.Backlight device that the present invention uses and transformator and solaode Sheet is all existing conventional.
Being additionally provided with the connecting hole of an annular on each support straight tube, the foot rest that lands is threaded connection part and passes Connecting hole is fixed with aircraft body.Further, each support straight tube is additionally provided with the connecting hole of an annular, falls Ground foot rest is threaded connection part and fixes with aircraft body through connecting hole.Supporting the connecting hole that annular is set on straight tube The foot rest that lands for convenience is threaded connection fixing with aircraft body, uses threaded connector through the such connection of connecting hole Fixed form has motility, and the foot rest that lands can take off at any time, does not occupies, it is simple to transport.
Described prolongation foot rest uses abrasion-resistive hard quality of rubber materials to make.Use the prolongation foot that abrasion-resistive hard quality of rubber materials is made Frame can be more resistant to mill, and service life is longer.
The present invention compared with prior art, has such advantages as and beneficial effect:
1, the present invention a kind of can the shockproof flight instruments of multiple-effect of flying for long time, solve existing minute vehicle and landing Time, the foot rest that lands be easily subject to impact and damage, and land foot rest be weak to mill problem;
2, the present invention a kind of can the shockproof flight instruments of multiple-effect of flying for long time, solve existing minute vehicle and fall in injustice Time on smooth ground, the photographic head of minute vehicle and The Cloud Terrace easily collide with damage, and the picture of shooting obscures because being given a shock Unclear problem;
3, the present invention a kind of can the shockproof flight instruments of multiple-effect of flying for long time, solving existing minute vehicle can not be automatic Power supply, causes aircraft can not maintain flying for long time, changes battery trouble, the waste energy, the most durable problem.
Accompanying drawing explanation
Accompanying drawing described herein is used for providing being further appreciated by the embodiment of the present invention, constitutes of the application Point, it is not intended that the restriction to the embodiment of the present invention.In the accompanying drawings:
Fig. 1 is the structural representation of the present invention;
Fig. 2 is that the present invention lands the structural representation of foot rest;
Fig. 3 is the structural representation of guard rail of the present invention.
Labelling in accompanying drawing and the component names of correspondence:
1-aircraft body, 2-supports straight tube, 3-bracing frame, 4-damping spring, 5-damping straight tube, and 6-extends foot rest, 7-card Button, 8-connecting hole, 9-guard rail, 10-groove, 11-circular hole, 12-solar battery sheet.
Detailed description of the invention
For making the object, technical solutions and advantages of the present invention clearer, below in conjunction with embodiment and accompanying drawing, to this Invention is described in further detail, and the exemplary embodiment of the present invention and explanation thereof are only used for explaining the present invention, do not make For limitation of the invention.
Embodiment 1:
As shown in Figure 1, Figure 2, Figure 3 shows a kind of can the shockproof flight instruments of multiple-effect of flying for long time, including aircraft body 1, Connecting on aircraft body 1 has two to land foot rest, it is characterised in that each foot rest that lands includes that two support straight tubes 2 and Individual bracing frame 3, is provided with two slotted eyes on each bracing frame 3, is provided with one between each support straight tube 2 and bracing frame 3 Individual damping spring 4;One end of described damping spring 4 is fixed with supporting straight tube 2, and the other end is fixed with bracing frame 3;At damping spring The 4 internal damping straight tubes 5 that are additionally provided with, one end of damping straight tube 5 is fixing with bracing frame 3, and it is internal that the other end is placed in support straight tube 2; Also including that extends a foot rest 6 on foot rest each landing, described prolongation foot rest 6 is fixed on bracing frame 3 by two buckles 7 On;
Landing at two and be additionally provided with a guard rail 9 between foot rest, the two ends of guard rail 9 are landed on foot rest with two respectively Bracing frame 3 connects;Described guard rail 9 be one by the bar pad having certain thickness rubber to make, set at the two ends of guard rail 9 It is equipped with groove 10, the notch size of groove 10 and the shaft diameter matches of bracing frame 3;Each groove 10 is additionally provided with two Circular hole 11, the diameter of described circular hole 11 is equal with the diameter of slotted eye on bracing frame 3, uses screw bolt and nut to coordinate even Guard rail 9 is fixed on bracing frame 3 by the mode connect;
Being additionally provided with a solar battery sheet 12 on aircraft body 1, the electric energy of acquisition is flown by solar battery sheet 12 Rechargeable battery charging within row device body 1;Described solar battery sheet 12 is positioned at the top of aircraft body 1, uses draw-in groove Solar battery sheet 12 is fixed on aircraft body 1 by the mode connected.
Being additionally provided with the connecting hole 8 of an annular on each support straight tube 2, the foot rest that lands is threaded connection part and wears Cross connecting hole to fix with aircraft body 1.Described prolongation foot rest 6 uses abrasion-resistive hard quality of rubber materials to make.
A kind of can the design principle of the shockproof flight instruments of multiple-effect of flying for long time: flight controller has constant weight, So flight controller is when landing, the foot rest that lands being positioned on flight controller can produce an active force over the ground, meanwhile, Landing foot rest also can be by the opposition on ground.Because by the opposition on ground, land the damping bullet on foot rest Spring 4 will be produced a thrust by compression, and the thrust of damping spring 4 generation can be cancelled out each other with the opposition on ground, with Time, the one end being placed in support damping straight tube 5 within straight tube 2 more can probe into along with the compression of damping spring 4 in support straight tube 2 Portion.Land on foot rest arrange damping spring 4 and damping straight tube 5 solve existing minute vehicle and be easily subject to when landing To concussion, the float causing shooting is unclear, and lands foot rest and be easily subject to impact and the problem damaged.
Also include that extends a foot rest 6 on foot rest each landing, by two buckles 7, a prolongation foot rest 6 is fixed Bracing frame 3 adds and lands the height of foot rest, both can ensure that the original-pack foot rest that lands was not dirty, and be not scraped off, again can The probability that when reducing landing, camera lens, The Cloud Terrace are injured.Additionally extending foot rest 6 uses natural rubber material to make, and more resistant to mill, uses the longevity Order longer.
Landing at two and arrange a guard rail 9 between foot rest, guard rail 9 uses synthetic rubber to make.When falling in injustice The local time in of sliding, there are this guard rail 9, photographic head and The Cloud Terrace can avoid colliding with below photographic head, photographic head and The Cloud Terrace A good protection can be obtained.
In aircraft body 1, it is additionally provided with inverter and transformator, uses monocrystaline silicon solar cell sheet 12 to be arranged on The top of aircraft body 1 can be conducive to shining upon, in order to obtains luminous energy.The electric current that solaode 12 produces is direct current Electricity, unidirectional current is transformed into alternating current after inverter, then the voltage of the alternating current transmitted by inverter through transformator drops to In the rechargeable battery range of nominal tension, then it is transmitted further to rechargeable battery.Using solar energy is that aircraft is powered, and solves existing Minute vehicle can not automatic power, change battery trouble, waste the energy, the most durable problem.
Above-described detailed description of the invention, has been carried out the purpose of the present invention, technical scheme and beneficial effect further Describe in detail, be it should be understood that the detailed description of the invention that the foregoing is only the present invention, be not intended to limit the present invention Protection domain, all within the spirit and principles in the present invention, any modification, equivalent substitution and improvement etc. done, all should comprise Within protection scope of the present invention.

Claims (3)

1. can the shockproof flight instruments of multiple-effect of flying for long time, including aircraft body (1), on aircraft body (1) Connect and have two to land foot rest, it is characterised in that each foot rest that lands includes that two support straight tube (2) and a bracing frame (3), Each bracing frame (3) is provided with two slotted eyes, between each support straight tube (2) and bracing frame (3), is provided with one subtracts Shake spring (4);One end of described damping spring (4) is fixed with supporting straight tube (2), and the other end is fixed with bracing frame (3);In damping The internal damping straight tube (5) that is additionally provided with of spring (4), one end of damping straight tube (5) is fixing with bracing frame (3), and the other end is placed in and props up Support straight tube (2) is internal;Also including that extends a foot rest (6) on foot rest each landing, described prolongation foot rest (6) passes through two cards Button (7) is fixed on bracing frame (3);
Landing at two and be additionally provided with a guard rail (9) between foot rest, land foot rest respectively with two at the two ends of guard rail (9) On bracing frame (3) connect;Described guard rail (9) be one by the bar pad having certain thickness rubber to make, at guard rail (9) two ends are provided with the shaft diameter matches of groove (10), the notch size of groove (10) and bracing frame (3);Each recessed Being additionally provided with two circular holes (11) on groove (10), the diameter of the diameter of described circular hole (11) slotted eye upper with bracing frame (3) is big Little equal, guard rail (9) is fixed on bracing frame (3) by the mode using screw bolt and nut to be connected;
Aircraft body (1) is additionally provided with a solar battery sheet (12), the electricity that solar battery sheet (12) will obtain The rechargeable battery charging that aircraft body (1) is internal can be given;Described solar battery sheet (12) is positioned at the top of aircraft body (1) Portion, solar battery sheet (12) is fixed on aircraft body (1) by the mode using draw-in groove to connect.
The most according to claim 1 a kind of can the shockproof flight instruments of multiple-effect of flying for long time, it is characterised in that each Support the connecting hole (8) being additionally provided with an annular on straight tube (2), the foot rest that lands be threaded connection part through connecting hole with Aircraft body (1) is fixed.
The most according to claim 1 a kind of can the shockproof flight instruments of multiple-effect of flying for long time, it is characterised in that described in prolong Long foot rest (6) uses abrasion-resistive hard quality of rubber materials to make.
CN201610706090.5A 2016-08-23 2016-08-23 A kind of can the shockproof flight instruments of multiple-effect of flying for long time CN106081077A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610706090.5A CN106081077A (en) 2016-08-23 2016-08-23 A kind of can the shockproof flight instruments of multiple-effect of flying for long time

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610706090.5A CN106081077A (en) 2016-08-23 2016-08-23 A kind of can the shockproof flight instruments of multiple-effect of flying for long time

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107883927A (en) * 2017-11-09 2018-04-06 陕西科技大学 Quadrotor plant growth inspection system
CN108545206A (en) * 2018-04-03 2018-09-18 芜湖超科机电设备有限公司 A kind of aerophotography unmanned plane
CN110550217A (en) * 2019-09-21 2019-12-10 浙江驭云航空科技有限公司 Unmanned aerial vehicle's extension continuation of journey device

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2607232A1 (en) * 2011-12-21 2013-06-26 Eurocopter Deutschland GmbH Landing gear vibration absorber for a helicopter and method of operating said landing gear vibration absorber
CN104044731A (en) * 2014-06-26 2014-09-17 深圳市哈博森科技有限公司 Aircraft landing device and aircraft
CN205150253U (en) * 2015-11-26 2016-04-13 江西天祥通用航空股份有限公司 Novel helicopter joins externally pesticide spraying machine
CN205327398U (en) * 2015-12-27 2016-06-22 北京航空航天大学 Small -size many rotor crafts shock attenuation undercarriage
CN205418094U (en) * 2016-03-18 2016-08-03 天际智控成都科技有限责任公司 Push -button aircraft
CN206087275U (en) * 2016-08-23 2017-04-12 成都翼高九天科技有限公司 But jar -proof flying device of solar energy power supply multiple -effect

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2607232A1 (en) * 2011-12-21 2013-06-26 Eurocopter Deutschland GmbH Landing gear vibration absorber for a helicopter and method of operating said landing gear vibration absorber
CN104044731A (en) * 2014-06-26 2014-09-17 深圳市哈博森科技有限公司 Aircraft landing device and aircraft
CN205150253U (en) * 2015-11-26 2016-04-13 江西天祥通用航空股份有限公司 Novel helicopter joins externally pesticide spraying machine
CN205327398U (en) * 2015-12-27 2016-06-22 北京航空航天大学 Small -size many rotor crafts shock attenuation undercarriage
CN205418094U (en) * 2016-03-18 2016-08-03 天际智控成都科技有限责任公司 Push -button aircraft
CN206087275U (en) * 2016-08-23 2017-04-12 成都翼高九天科技有限公司 But jar -proof flying device of solar energy power supply multiple -effect

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107883927A (en) * 2017-11-09 2018-04-06 陕西科技大学 Quadrotor plant growth inspection system
CN108545206A (en) * 2018-04-03 2018-09-18 芜湖超科机电设备有限公司 A kind of aerophotography unmanned plane
CN108545206B (en) * 2018-04-03 2020-09-01 山东昊盾警用装备有限公司 Unmanned aerial vehicle for aerial photography
CN110550217A (en) * 2019-09-21 2019-12-10 浙江驭云航空科技有限公司 Unmanned aerial vehicle's extension continuation of journey device

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Application publication date: 20161109

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