CN202754144U - Undercarriage - Google Patents

Undercarriage Download PDF

Info

Publication number
CN202754144U
CN202754144U CN 201220369769 CN201220369769U CN202754144U CN 202754144 U CN202754144 U CN 202754144U CN 201220369769 CN201220369769 CN 201220369769 CN 201220369769 U CN201220369769 U CN 201220369769U CN 202754144 U CN202754144 U CN 202754144U
Authority
CN
China
Prior art keywords
lower bracket
lower support
utility
model
damping
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 - Lifetime
Application number
CN 201220369769
Other languages
Chinese (zh)
Inventor
徐�明
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.)
JIANGYIN CITY PUBLIC SECURITY BUREAU
Original Assignee
JIANGYIN CITY PUBLIC SECURITY BUREAU
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 JIANGYIN CITY PUBLIC SECURITY BUREAU filed Critical JIANGYIN CITY PUBLIC SECURITY BUREAU
Priority to CN 201220369769 priority Critical patent/CN202754144U/en
Application granted granted Critical
Publication of CN202754144U publication Critical patent/CN202754144U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Abstract

The utility model discloses an undercarriage. The undercarriage comprises a lower support (1), two upper supports (2) are upwards connected at the middle position of the lower support (1), two symmetrical bumps (4) are respectively upwards arranged at two ends of the lower support (1), a first damping leather ring (3) is arranged on the inner side of each bump (4) at two ends of the lower support (1), a second damping leather ring (5) is sleeved on the lower support (1) between the two upper supports (2), and the lower support (1) is a cuboid with the bottom elongated. The undercarriage is not prone to deform after long-term use.

Description

A kind of alighting gear
Technical field
The utility model relates to a kind of carry-on device, especially relates to a kind of alighting gear.
Background technology
When the police handles a case, in when, in some areas event or case occuring, when the ground scout vehicle can not be assessed omnidirection circumstance to the scene, can use that police unmanned plane is taken the bottom surface etc., but generally need to use the environment of this unmanned plane all more abominable, after often using, the alighting gear of unmanned plane easily is damaged.
The utility model content
Alighting gear long-term use after the perishable problem of the utility model in order to solve present police unmanned plane, a kind of alighting gear is provided for this reason, comprise lower bracket 1, the midway location of described lower bracket 1 upwards is connected with two upper brackets 2, the two ends of lower bracket 1 upwards are arranged with respectively a projection 4, two ends projection 4 inboards of described lower bracket 1 are overlapped respectively to overlap on the lower bracket 1 that has between 3, two upper brackets 2 of first a damping apron second a damping apron 5; Described lower bracket 1 is cuboid, and wide is 1~1.2mm, and length is 190~220mm, and height is 18~22mm.
The utility model alighting gear, described upper bracket 2 is arc, is connected with two reinforcement pins 6 between two upper brackets 2.
The beneficial effects of the utility model are:
The utility model can play the effect of damping when landing, and the bottom surface of lower bracket is elongated shape, has guaranteed that it is not yielding owing to being provided with three damping aprons at lower bracket, and is not fragile.
Description of drawings
The utility model will illustrate by example and with reference to the mode of accompanying drawing, wherein:
Fig. 1 is schematic diagram of the present utility model.
The specific embodiment
Disclosed all features in this specification sheets, or the step in disclosed all methods or the process except mutually exclusive feature and/or step, all can make up by any way.
Disclosed arbitrary feature in this specification sheets (comprising any accessory claim, summary and accompanying drawing) is unless special narration all can be replaced by other equivalences or the alternative features with similar purpose.That is, unless special narration, each feature is an example in a series of equivalences or the similar characteristics.
Alighting gear as shown in Figure 1, comprise lower bracket 1, the midway location of described lower bracket 1 upwards is connected with two upper brackets 2, the two ends of lower bracket 1 upwards are arranged with respectively a projection 4, two ends projection 4 inboards of described lower bracket 1 are overlapped respectively to overlap on the lower bracket 1 that has between 3, two upper brackets 2 of first a damping apron second a damping apron 5; Described lower bracket 1 is cuboid, and wide is 1~1.2mm, and length is 190~220mm, and height is 18~22mm.Described upper bracket 2 is arc, is connected with two reinforcement pins 6 between two upper brackets 2.The utility model can play the effect of damping when landing, and the bottom surface of lower bracket is elongated shape, has guaranteed that it is not yielding owing to being provided with three damping aprons at lower bracket, and is not fragile.
The utility model is not limited to the aforesaid specific embodiment.The utility model expands to any new feature or any new combination that discloses in this manual, and the arbitrary new method that discloses or step or any new combination of process.

Claims (2)

1. alighting gear, comprise lower bracket (1), it is characterized in that: the midway location of described lower bracket (1) upwards is connected with two upper brackets (2), the two ends of lower bracket (1) upwards are arranged with respectively a projection (4), two ends projection (4) inboard of described lower bracket (1) is overlapped respectively first a damping apron (3), and the upper cover of the lower bracket (1) between two upper brackets (2) has second a damping apron (5); Described lower bracket (1) is cuboid, and wide is 1~1.2mm, and length is 190~220mm, and height is 18~22mm.
2. alighting gear according to claim 1, it is characterized in that: described upper bracket (2) is arc, is connected with two reinforcement pins (6) between two upper brackets (2).
CN 201220369769 2012-07-30 2012-07-30 Undercarriage Expired - Lifetime CN202754144U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220369769 CN202754144U (en) 2012-07-30 2012-07-30 Undercarriage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220369769 CN202754144U (en) 2012-07-30 2012-07-30 Undercarriage

Publications (1)

Publication Number Publication Date
CN202754144U true CN202754144U (en) 2013-02-27

Family

ID=47733340

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220369769 Expired - Lifetime CN202754144U (en) 2012-07-30 2012-07-30 Undercarriage

Country Status (1)

Country Link
CN (1) CN202754144U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104002961A (en) * 2014-06-13 2014-08-27 韩世宇 Miniature helicopter undercarriage
CN107804456A (en) * 2016-09-08 2018-03-16 朗星无人机系统有限公司 A kind of how culvert vertical take-off and landing unmanned machine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104002961A (en) * 2014-06-13 2014-08-27 韩世宇 Miniature helicopter undercarriage
CN107804456A (en) * 2016-09-08 2018-03-16 朗星无人机系统有限公司 A kind of how culvert vertical take-off and landing unmanned machine

Similar Documents

Publication Publication Date Title
GB201208155D0 (en) Landing gear for an aircraft
USD693930S1 (en) Pair of struts for an orthopedic device
WO2014118688A3 (en) Absorbent tissue
WO2011135599A3 (en) Active platform for the landing of an aircraft on an access facility
CN202754144U (en) Undercarriage
CN204236768U (en) The remotely pilotless machine alighting gear of the simple and easy shock-damping structure of a kind of Novel dismountable
CN204137320U (en) Unmanned fog machine alighting gear
CN203473255U (en) Transporting, loading and unloading cart for cannonball or cabin
CN103143947B (en) The axle lateral surface of Lightweight balance shaft support cuts frock
CN203143191U (en) Nonslip corrugation type molded tray
CN207207742U (en) A kind of gear sheath corner binding structure
CN205327392U (en) Unmanned aerial vehicle centre frame structure
CN203740515U (en) Convenient and fast conveying tool for special terrain
CN203986943U (en) The mobile device of wardrobe
CN203975220U (en) A kind of unmanned plane main landing gear bumper
CN204507484U (en) Plastic bag sack launches bracing frame
CN203844774U (en) Shake-proof cart
CN204709177U (en) A kind of crotch is received and is carried diaper
CN204197396U (en) A kind of food transport device
CN202716216U (en) Assembly body structure
CN203600897U (en) Balance wheel rocker arm structure
CN204568684U (en) Blowing car
CN202864862U (en) Dismountable horizontal jack heightened top tray component
CN205180760U (en) Hand cart based removes steam pot
CN202344534U (en) Green tire storing tray with internal supporting body

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CX01 Expiry of patent term

Granted publication date: 20130227

CX01 Expiry of patent term