CN106379539B - A kind of aircraft chassis with delivery functions - Google Patents

A kind of aircraft chassis with delivery functions Download PDF

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Publication number
CN106379539B
CN106379539B CN201610985293.2A CN201610985293A CN106379539B CN 106379539 B CN106379539 B CN 106379539B CN 201610985293 A CN201610985293 A CN 201610985293A CN 106379539 B CN106379539 B CN 106379539B
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China
Prior art keywords
bracket
stabilizer blade
aircraft
vacuum chuck
bogey
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CN201610985293.2A
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Chinese (zh)
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CN106379539A (en
Inventor
程强
闫国彬
李广朋
齐宝宝
任伟达
蔡力钢
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Beijing University of Technology
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Beijing University of Technology
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Priority to CN201610985293.2A priority Critical patent/CN106379539B/en
Publication of CN106379539A publication Critical patent/CN106379539A/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D9/00Equipment for handling freight; Equipment for facilitating passenger embarkation or the like

Abstract

A kind of aircraft chassis with delivery functions, the aircraft chassis include bracket, dispenser, and bracket has Self-balancing and shock-absorbing function.The surrounding of bracket is arranged in stabilizer blade, and stabilizer blade is the support construction of bracket, and the centre of bracket is dispatching accommodating chamber.Stabilizer blade is connect by buffering self-balancing spring arrangement with bracket stabilizing device, and the bottom of bracket stabilizing device is arranged in anti-skid device.When transport cargo needs to adsorb, vacuum chuck bogey is to connect vacuum absorption device.When transport cargo needs to contain, cabinet fixation hole is connected with cabinet folder bearing apparatus.When transport cargo needs to bundle, small hook is connected with rubber bandage connecting hole.Chassis design circularizes, and center of gravity is at center, and annulus lower part is the anti-skid device of special material, increases stationarity when aircraft landing.Bracket has Self-balancing and pooling feature, makes chassis more safety and stability by improving.

Description

A kind of aircraft chassis with delivery functions
Technical field
The present invention relates to one kind to be directed to different purposes, the aircraft of different class and a kind of course of new aircraft bottom for designing Frame.Belong to aircraft field, the diversification transport of the main practicability for increasing low side aircraft and middle and high end transporter aircraft.
Background technique
As the field of the rapid development of aircraft industry, application is more and more extensive, occur different class in the market Aircraft, the thing on this is once tall and big in terms of the military project " flies into common people house ".And aircraft is transported in express delivery The application of defeated aspect, current technology are not yet mature.With the rapid development of logistics, express delivery electric vehicle is more and more, this gives Urban transportation brings problems.China urban is forbidden to electric vehicle.This will all promote aircraft to lead in transport The development in domain.
One aspect of the present invention can make low side aircraft increase practicability and enjoyment, on the other hand can solve transport again The diversified problem of aircraft conveying articles.
Summary of the invention
The present invention provides a kind of aircraft chassis, more traditional chassis has design succinctly compared to practicability is increased, Many advantages, such as convenient to use.
In order to achieve the above object, the solution of the present invention is a kind of aircraft chassis with delivery functions, using module Change design, which includes bracket, dispenser;Dispenser includes vacuum absorption device, bundling apparatus, bracket tool There are Self-balancing and shock-absorbing function.
Bracket includes bracket stabilizer blade 1.1, vacuum chuck bogey 1.2, rubber bandage connecting hole 1.3, buffering self-balancing Spring arrangement 1.4, bracket stabilizing device 1.5, anti-skid device 1.6.
The surrounding of bracket is arranged in stabilizer blade 1.1, and stabilizer blade 1.1 is the support construction of bracket, and the centre of bracket is that dispatching accommodates Chamber.
Stabilizer blade 1.1 is connect by buffering self-balancing spring arrangement 1.4 with bracket stabilizing device 1.5, and anti-skid device 1.6 is arranged In the bottom of bracket stabilizing device 1.5.
Vacuum chuck bogey 1.2 is arranged at the top of the support construction being made of stabilizer blade 1.1, rubber bandage connecting hole 1.3 settings are in middle layer, rubber bandage connecting hole 1.3 and buffering 1.4 alternating parallel of self-balancing spring arrangement arrangement.
Vacuum chuck bogey 1.2 is to connect vacuum absorption device.
Anti-skid device 1.6 is rubber material or plastic material.
Buffering self-balancing spring arrangement 1.4 is compressed spring, and elasticity is formed between stabilizer blade 1.1 and bracket stabilizing device 1.5 Connection.
When transport cargo needs to adsorb, vacuum chuck bogey 1.2 is to connect vacuum absorption device.
When transport cargo needs to contain, rubber bandage connecting hole 1.3 and buffering self-balancing spring arrangement 1.4 connect It connects.
Vacuum absorption device includes vacuum chuck 2.1 and connecting line 2.2, and vacuum chuck 2.1 passes through connecting line 2.2 and flight The dynamical system of device controls connection, and vacuum chuck 2.1 is mounted on vacuum chuck bogey 1.2, the dynamical system of aircraft Power is provided for vacuum chuck 2.1.
Bundling apparatus includes rubber strip 3.1 and small hook 3.2, and small hook 3.2 is connect with rubber bandage connecting hole 1.3, rubber Adhesive tape 3.1 is connected between small hook 3.2.
Compared with prior art, the present invention has the advantage that
1, modularized design, it is convenient for disassembly and assembly, bundling apparatus can be unloaded when with adsorbent equipment, it can when with bundling apparatus Adsorbent equipment is unloaded.
2, multipurpose, multiple choices scheme.
3, vacuum absorption device safety and stability, strong antijamming capability, high reliablity.
4, bundling apparatus energy conservation and environmental protection, it is low in cost.
5, chassis design circularizes, and center of gravity is at center, and annulus lower part is the anti-skid device of special material, is increased Stationarity when aircraft lands.
6, bracket has Self-balancing and pooling feature, makes chassis more safety and stability by improving.
Detailed description of the invention
Fig. 1 is rack assumption diagram.
Fig. 2 is bracket pair figure.
Fig. 3 is buffering, self-balancing spring arrangement.
Fig. 4 is buffering, self-balancing spring arrangement pair figure.
Fig. 5 is vacuum absorption device figure.
Fig. 6 is bundling apparatus figure.
Fig. 7 is bundling apparatus pair figure.
Specific embodiment
As shown in figs. 1-7, for the aircraft of transport express delivery or take-away: if transporting more expensive article or day When gas is more severe, using vacuum absorption device, directly article is put under aircraft at this time, starts vacuum absorption device, it will Article is inhaled on board the aircraft, and destination is transported to.This safe and stable arrangement, high reliablity.
For wrapping up class article, then bundling apparatus is selected, directly package is bundled on bracket with rubber strip at this time, is buckled Hook, this device is simple and convenient easy to operate, and will not additionally increase too many cost, does not consume the energy content of battery.

Claims (3)

1. a kind of aircraft chassis with delivery functions, it is characterised in that: use modularized design, which includes Bracket, dispenser;Dispenser includes vacuum absorption device, bundling apparatus, and bracket has Self-balancing and shock-absorbing function;
Bracket includes bracket stabilizer blade (1.1), vacuum chuck bogey (1.2), rubber bandage connecting hole (1.3), buffers from flat Weigh spring arrangement (1.4), bracket stabilizing device (1.5), anti-skid device (1.6) and;
The surrounding of bracket is arranged in stabilizer blade (1.1), and stabilizer blade (1.1) is the support construction of bracket, and the centre of bracket is that dispatching accommodates Chamber;
Stabilizer blade (1.1) is connect by buffering self-balancing spring arrangement (1.4) with bracket stabilizing device (1.5), anti-skid device (1.6) Bottom in bracket stabilizing device (1.5) is set;
Vacuum chuck bogey (1.2) setting is at the top of the support construction being made of stabilizer blade (1.1), rubber bandage connecting hole (1.3) setting is in middle layer, rubber bandage connecting hole (1.3) and buffering self-balancing spring arrangement (1.4) alternating parallel arrangement;
Vacuum chuck bogey (1.2) is to connect vacuum absorption device;
Anti-skid device (1.6) is rubber material or plastic material;
Buffering self-balancing spring arrangement (1.4) is compressed spring, forms bullet between stabilizer blade (1.1) and bracket stabilizing device (1.5) Property connection;
When transport cargo needs to adsorb, vacuum chuck bogey (1.2) is to connect vacuum absorption device;
When transport cargo needs to bundle, small hook (3.2) and rubber bandage connecting hole (1.3) connection.
2. a kind of aircraft chassis with delivery functions according to claim 1, it is characterised in that: vacuum absorption device Including vacuum chuck (2.1) and connecting line (2.2), vacuum chuck (2.1) passes through the dynamical system of connecting line (2.2) and aircraft Control connection, vacuum chuck (2.1) are mounted on vacuum chuck bogey (1.2), and the dynamical system of aircraft is vacuum suction Disk (2.1) provides power.
3. a kind of aircraft chassis with delivery functions according to claim 1, it is characterised in that: bundling apparatus (3) Including rubber strip (3.1) and small hook (3.2), small hook (3.2) connect with rubber bandage connecting hole (1.3), rubber strip (3.1) It is connected between small hook (3.2).
CN201610985293.2A 2016-11-09 2016-11-09 A kind of aircraft chassis with delivery functions Active CN106379539B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610985293.2A CN106379539B (en) 2016-11-09 2016-11-09 A kind of aircraft chassis with delivery functions

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610985293.2A CN106379539B (en) 2016-11-09 2016-11-09 A kind of aircraft chassis with delivery functions

Publications (2)

Publication Number Publication Date
CN106379539A CN106379539A (en) 2017-02-08
CN106379539B true CN106379539B (en) 2019-09-27

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Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106621351A (en) * 2017-02-24 2017-05-10 武汉蛋玩科技有限公司 Novel toy robot
CN107554797B (en) * 2017-09-05 2019-12-13 安徽新博普曼智能科技股份有限公司 auxiliary bearing structure of delivery robot
CN107628253B (en) * 2017-10-11 2019-10-22 罗芳芳 A kind of support mechanism on distributed robot
CN111994760B (en) * 2020-09-16 2022-02-18 浙江乔派电梯装饰有限公司 Goods lift car
CN116280206B (en) * 2023-03-22 2024-01-12 深圳技术大学 Magnetic attraction type logistics unmanned aerial vehicle

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4553719A (en) * 1983-11-04 1985-11-19 David Ott Vehicle lifting system and method
CN103771132A (en) * 2014-01-24 2014-05-07 江苏大卫精工科技有限公司 Sucker-type plate transporting device
CN203854854U (en) * 2014-05-29 2014-10-01 金陵科技学院 Rotary wing type unmanned plane with damping landing gear
CN204323695U (en) * 2014-12-16 2015-05-13 湖南基石信息技术有限公司 Load platform and be provided with the unmanned vehicle of this load platform
CN204871589U (en) * 2015-05-14 2015-12-16 苏州绿农航空植保科技有限公司 Aircraft shock attenuation undercarriage
CN205327398U (en) * 2015-12-27 2016-06-22 北京航空航天大学 Small -size many rotor crafts shock attenuation undercarriage
CN205327421U (en) * 2016-01-27 2016-06-22 哈尔滨盛世特种飞行器有限公司 But aircraft of quick replacement medical kit
CN105966605A (en) * 2016-05-19 2016-09-28 郑琳琳 Delta parallel mechanism-based six-rotor aircraft

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4553719A (en) * 1983-11-04 1985-11-19 David Ott Vehicle lifting system and method
CN103771132A (en) * 2014-01-24 2014-05-07 江苏大卫精工科技有限公司 Sucker-type plate transporting device
CN203854854U (en) * 2014-05-29 2014-10-01 金陵科技学院 Rotary wing type unmanned plane with damping landing gear
CN204323695U (en) * 2014-12-16 2015-05-13 湖南基石信息技术有限公司 Load platform and be provided with the unmanned vehicle of this load platform
CN204871589U (en) * 2015-05-14 2015-12-16 苏州绿农航空植保科技有限公司 Aircraft shock attenuation undercarriage
CN205327398U (en) * 2015-12-27 2016-06-22 北京航空航天大学 Small -size many rotor crafts shock attenuation undercarriage
CN205327421U (en) * 2016-01-27 2016-06-22 哈尔滨盛世特种飞行器有限公司 But aircraft of quick replacement medical kit
CN105966605A (en) * 2016-05-19 2016-09-28 郑琳琳 Delta parallel mechanism-based six-rotor aircraft

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Inventor after: Cheng Qiang

Inventor after: Yan Guobin

Inventor after: Li Guangpeng

Inventor after: Qi Baobao

Inventor after: Ren Weida

Inventor after: Cai Ligang

Inventor before: Cheng Qiang

Inventor before: Yan Guobin

Inventor before: Qi Baobao

Inventor before: Ren Weida

Inventor before: Cai Ligang

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