CN205293103U - Anticollision type unmanned vehicles - Google Patents

Anticollision type unmanned vehicles Download PDF

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Publication number
CN205293103U
CN205293103U CN201620015956.3U CN201620015956U CN205293103U CN 205293103 U CN205293103 U CN 205293103U CN 201620015956 U CN201620015956 U CN 201620015956U CN 205293103 U CN205293103 U CN 205293103U
Authority
CN
China
Prior art keywords
stop sleeve
bending pin
fixing housing
support
supporting leg
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
CN201620015956.3U
Other languages
Chinese (zh)
Inventor
张琳丽
沙恬果
金雅坤
唐廷顺
林星豪
李旭贺
穆楠
郝世超
韦洋红
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201620015956.3U priority Critical patent/CN205293103U/en
Application granted granted Critical
Publication of CN205293103U publication Critical patent/CN205293103U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides an anticollision type unmanned vehicles, including the host computer body and a plurality of motor support, be provided with a plurality of motor supports of evenly arranging around the host computer body, the end of every motor support is provided with a driving motor who takes the screw through the fixed lantern ring of motor respectively, it supports protector to be provided with one respectively in every motor support bottom, it comprises stop sleeve and supporting leg to support protector, upper and lower three angle connection plate that set up respectively at the stop sleeve, the inside bracing piece that is provided with of stop sleeve, inner and the inside piston boit of stop sleeve of bracing piece are connected, still be provided with the exhaust hole rather than the inside intercommunication on the stop sleeve lateral wall, set up the supporting leg at fixed casing lower extreme, the internal part of set casing do not is provided with the bending pin of two strip torsional springs. The utility model discloses a two sets of bending pins that set up on expanding spring, every fixed casing effectively cushion the striking that the aircraft received when flight, improved the anti striking ability of aircraft greatly.

Description

A kind of crash-proof unmanned vehicle
Technical field
This utility model relates to unmanned vehicle technical field, specifically a kind of crash-proof unmanned vehicle.
Background technology
Development along with unmanned vehicle, the activities such as unmanned vehicle is widely applied to landform detection, rescue is searched, take photo by plane, although current unmanned vehicle has greatly improved in performance, especially in the stability of flight, controllability, universality, increasingly press close to consuming public, but, the crashproof ability of current unmanned vehicle is still poor, and ordinary consumer is easily used to and collides with and damage.
Utility model content
For solving the problems referred to above, the purpose of this utility model is to provide a kind of crash-proof unmanned vehicle.
This utility model is for achieving the above object, a kind of crash-proof unmanned vehicle, including main body and multiple electric machine support, the electric machine support being provided around multiple uniform arrangement at main body, the end of each electric machine support is provided with a drive motor with propeller respectively through motor retaining collar, each drive motor is connected with the control circuit in main body and rechargeable battery respectively through wire, a support protecting appts it is respectively arranged with bottom each electric machine support, support protecting appts is made up of stop sleeve and supporting leg, triangular connecting plate it is respectively provided with up and down at stop sleeve, stop sleeve is internally provided with support bar, the inner of support bar is connected with the piston boit within stop sleeve, stop sleeve, outside support bar is provided with coil tension spring, and the end of stop sleeve is provided with the annular projection blocking piston boit and support bar, stop sleeve sidewall is additionally provided with and its internal steam vent connected, the outer end of support bar is connected to fixing housing, in fixing housing lower end, supporting leg is set, set casing internal body portion is not provided with the bending pin of two band torsion springs, and the bending pin of top is upward, bending pin upper end is made to be positioned at the side of propeller, the bending pin of lower section is acute angle with the angle of supporting leg, one end of bending pin and torsion spring are fixed in set casing body by rotating bar, one end of torsion spring is inserted in the cylindrical cavity body of bending pin, torsion spring bumping post it is respectively arranged with in cylindrical cavity body and in the set casing body of the torsion spring other end, the set casing body sidewall of the side that bending pin contacts with fixing housing is provided with rubber cushion blocks, the arc-shaped limit bar for stopping bending pin it is provided with in fixing housing upper end.
As further technical scheme: the bending pin of top is longer than the bending pin of lower section, and the lower end of lower section bending pin is lower than the lower end of supporting leg.
Owing to adopting above technical scheme, the shock that aircraft is subject to effectively is cushioned when flight by the two groups of bending pins arranged on coil tension spring, each fixing housing, there is provided more elastic external frame for aircraft, substantially increase the impact resistant capability of aircraft.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the I partial enlargement structural representation of Fig. 1.
In figure: 1 main body 2 electric machine support 3 motor retaining collar 4 propeller 5 drive motor 6 stop sleeve 7 supporting leg 8 triangular connecting plate 9 support bar 10 piston boit 11 steam vent 12 is fixed housing 13 torsion spring 14 bending pin 15 and rotated bar 16 circular cylindrical cavity 17 torsion spring bumping post 18 rubber cushion blocks 19 arc-shaped limit bar 20 coil tension spring 21 annular projection.
Detailed description of the invention
A kind of crash-proof unmanned vehicle, as shown in Fig. 1 Fig. 2, including main body 1 and multiple electric machine support 2, the electric machine support 2 being provided around multiple uniform arrangement at main body 1, the end of each electric machine support 2 is provided with a drive motor 5 with propeller 4 respectively through motor retaining collar 3, each drive motor 5 is connected with the control circuit in main body 1 and rechargeable battery respectively through wire, a support protecting appts it is respectively arranged with bottom each electric machine support 2, support protecting appts is made up of stop sleeve 6 and supporting leg 7, triangular connecting plate 8 it is respectively provided with up and down at stop sleeve 6, stop sleeve 6 is internally provided with support bar 9, the inner of support bar 9 is connected with the piston boit 10 within stop sleeve 6, support bar 9 outside stop sleeve 6 is provided with coil tension spring 20, and the end of stop sleeve 6 is provided with the annular projection 21 blocking piston boit 10 and support bar 9, stop sleeve 6 sidewall is additionally provided with and its internal steam vent 11 connected, the outer end of support bar 9 is connected to fixing housing 12, in fixing housing 12 lower end, supporting leg 7 is set, the internal bending pin 14 being respectively arranged with two band torsion springs 13 of fixing housing 12, and the bending pin 14 of top is upward, bending pin 14 upper end is made to be positioned at the side of propeller 4, the bending pin 14 of lower section is acute angle with the angle of supporting leg 7, one end of bending pin 14 and torsion spring 13 are fixed in fixing housing 12 by rotating bar 15, one end of torsion spring 13 is inserted in the circular cylindrical cavity 16 of bending pin 14, it is respectively arranged with torsion spring bumping post 17 in circular cylindrical cavity 16 and in the fixing housing 12 of torsion spring 13 other end, fixing housing 12 sidewall of the side that bending pin 14 contacts with fixing housing 12 is provided with rubber cushion blocks 18, fixing housing 12 upper end is provided with the arc-shaped limit bar 19 for stopping bending pin 14.
In order to reduce impact force when unmanned vehicle lands, the bending pin 14 of top is longer than the bending pin 14 of lower section, and the lower end of lower section bending pin 14 is lower than the lower end of supporting leg 7.
Certainly, described above is not that this utility model is also not limited to the example above to restriction of the present utility model; those skilled in the art; in essential scope of the present utility model, change, change, interpolation or the replacement made, all should belong to protection domain of the present utility model.

Claims (2)

1. a crash-proof unmanned vehicle, it is characterized in that: include main body (1) and multiple electric machine support (2), the electric machine support (2) being provided around multiple uniform arrangement at main body (1), the end of each electric machine support (2) is provided with a drive motor (5) with propeller (4) respectively through motor retaining collar (3), each drive motor (5) is connected with the control circuit in main body (1) and rechargeable battery respectively through wire, it is respectively arranged with a support protecting appts in each electric machine support (2) bottom, support protecting appts is made up of stop sleeve (6) and supporting leg (7), triangular connecting plate (8) it is respectively provided with up and down at stop sleeve (6), stop sleeve (6) is internally provided with support bar (9), the inner of support bar (9) is connected with the piston boit (10) of stop sleeve (6) inside, the support bar (9) that stop sleeve (6) is outside is provided with coil tension spring (20), and the end of stop sleeve (6) is provided with the annular projection (21) blocking piston boit (10) and support bar (9), stop sleeve (6) sidewall is additionally provided with and its internal steam vent (11) connected, the outer end of support bar (9) is connected to fixing housing (12), in fixing housing (12) lower end, supporting leg (7) is set, the internal bending pin (14) being respectively arranged with two band torsion springs (13) of fixing housing (12), and the bending pin (14) of top is upward, bending pin (14) upper end is made to be positioned at the side of propeller (4), the bending pin (14) of lower section is acute angle with the angle of supporting leg (7), one end of bending pin (14) and torsion spring (13) are fixed in fixing housing (12) by rotating bar (15), one end of torsion spring (13) is inserted in the circular cylindrical cavity (16) of bending pin (14), torsion spring bumping post (17) it is respectively arranged with in circular cylindrical cavity (16) and in the fixing housing (12) of torsion spring (13) other end, fixing housing (12) sidewall of the side that bending pin (14) contacts with fixing housing (12) is provided with rubber cushion blocks (18), the arc-shaped limit bar (19) for stopping bending pin (14) it is provided with in fixing housing (12) upper end.
2. a kind of crash-proof unmanned vehicle according to claim 1, it is characterised in that: the bending pin (14) of top is longer than the bending pin (14) of lower section, and the lower end of lower section bending pin (14) is lower than the lower end of supporting leg (7).
CN201620015956.3U 2016-01-11 2016-01-11 Anticollision type unmanned vehicles Expired - Fee Related CN205293103U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620015956.3U CN205293103U (en) 2016-01-11 2016-01-11 Anticollision type unmanned vehicles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620015956.3U CN205293103U (en) 2016-01-11 2016-01-11 Anticollision type unmanned vehicles

Publications (1)

Publication Number Publication Date
CN205293103U true CN205293103U (en) 2016-06-08

Family

ID=56485336

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620015956.3U Expired - Fee Related CN205293103U (en) 2016-01-11 2016-01-11 Anticollision type unmanned vehicles

Country Status (1)

Country Link
CN (1) CN205293103U (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106081079A (en) * 2016-08-15 2016-11-09 张琬彬 A kind of crashproof leg of unmanned plane rotor
CN107128482A (en) * 2017-05-03 2017-09-05 李秀荣 A kind of anticollision unmanned plane
WO2018032264A1 (en) * 2016-08-15 2018-02-22 张琬彬 Unmanned aerial vehicle machine body anti-collision structure
WO2018032262A1 (en) * 2016-08-15 2018-02-22 张琬彬 Unmanned aerial vehicle rotor anti-collision structure
WO2018032263A1 (en) * 2016-08-15 2018-02-22 张琬彬 Unmanned aerial vehicle rotor anti-collision support foot

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106081079A (en) * 2016-08-15 2016-11-09 张琬彬 A kind of crashproof leg of unmanned plane rotor
WO2018032264A1 (en) * 2016-08-15 2018-02-22 张琬彬 Unmanned aerial vehicle machine body anti-collision structure
WO2018032262A1 (en) * 2016-08-15 2018-02-22 张琬彬 Unmanned aerial vehicle rotor anti-collision structure
WO2018032263A1 (en) * 2016-08-15 2018-02-22 张琬彬 Unmanned aerial vehicle rotor anti-collision support foot
CN107128482A (en) * 2017-05-03 2017-09-05 李秀荣 A kind of anticollision unmanned plane

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160608

Termination date: 20170111

CF01 Termination of patent right due to non-payment of annual fee