CN208828091U - It is a kind of to install the Fixed Wing AirVehicle undercarriage for folding sled additional - Google Patents

It is a kind of to install the Fixed Wing AirVehicle undercarriage for folding sled additional Download PDF

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Publication number
CN208828091U
CN208828091U CN201821294998.0U CN201821294998U CN208828091U CN 208828091 U CN208828091 U CN 208828091U CN 201821294998 U CN201821294998 U CN 201821294998U CN 208828091 U CN208828091 U CN 208828091U
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CN
China
Prior art keywords
undercarriage
sled
ontology
undercarriage ontology
additional
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
CN201821294998.0U
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Chinese (zh)
Inventor
郑翼
牛牧文
章志凯
冷根
黄俊前
朱延平
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Nanchang Hangkong University
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Nanchang Hangkong University
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
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Priority to CN201821294998.0U priority Critical patent/CN208828091U/en
Application granted granted Critical
Publication of CN208828091U publication Critical patent/CN208828091U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of Fixed Wing AirVehicle undercarriages for installing folding sled additional, including undercarriage ontology, tire, ski device, rotating device, undercarriage ontology and tire are attached by axis, ski device symmetry arrangement is in the two sides of undercarriage ontology, rotating device is set to ski device, between undercarriage ontology, wherein ski device includes sled, rotary support, rotary support is connected on the sled, rotating device includes main rotating shaft, secondary rotary shaft, main rotating shaft, it is connected between secondary rotary shaft by hydraulic rod piece, secondary rotary shaft is fixed in rotary support by vertical member, main rotating shaft is fixed on undercarriage ontology by rod piece.The utility model advantage: it installs additional and folds the Fixed Wing AirVehicle undercarriage of sled and encounter snowfield environment and still have and take off, land, sliding race, ground moving and the ability parked, non- snowfield environment undercarriage ontology disables ski device, and ski device is easily attached, structure is simple, easy to disassemble and maintenance.

Description

It is a kind of to install the Fixed Wing AirVehicle undercarriage for folding sled additional
Technical field
The utility model relates to airplane design technical fields, fly more particularly to a kind of fixed-wing for installing folding sled additional Device undercarriage.
Background technique
Landing gear is the important component with load and maneuverability of aircraft, during aircraft security landing It is responsible for extremely important mission.Undercarriage is support system necessary to taking off, land, sliding race, ground moving and park System, is one of main component of aircraft.But if meeting aircraft landing site to be covered by heavy snow, aircraft can not just be risen Drop is so as to cause influence economically.
Summary of the invention
In order to solve the above-mentioned technical problem, the utility model provides a kind of Fixed Wing AirVehicle for installing additional and folding sled Fall frame.
The utility model adopts the following technical solution: a kind of Fixed Wing AirVehicle undercarriage installing folding sled additional, including Undercarriage ontology, tire, ski device, rotating device, tire is located at undercarriage body bottom portion, between tire and undercarriage ontology It is attached by axis, ski device is symmetrically distributed in undercarriage ontology two sides, and rotation is equipped between ski device, undercarriage ontology Rotary device;
The ski device includes sled, rotary support, and rotary support is set to sled indent side, and the rotary support is used In carrying out rotary folding to sled, rotate sled to undercarriage ontology two sides, the rotating device includes main rotating shaft, secondary rotation Shaft, secondary rotary shaft connect with vertical member one end axis, and the vertical member other end is fixedly mounted in rotary support, main rotating shaft with Rod piece one end axis connects, and the rod piece other end is fixedly connected on undercarriage ontology, passes through liquid between the main rotating shaft, secondary rotary shaft Strut Part is fixedly connected, and the rotating device is for rotating sled to undercarriage body bottom portion, rotary support and rotating device It cooperates and can be realized the enabling and disabling of sled.
The utility model has the advantage that: installing the Fixed Wing AirVehicle undercarriage for folding sled additional and has in snowfield environment Fly, land, slide race, ground moving and the ability parked;When non-snowfield environment carry out landing when, sled can be rotated to rise Frame ontology two sides are fallen, and ski device is easily attached with undercarriage ontology, structure is simple, easy to disassemble and maintenance.
Detailed description of the invention
Fig. 1, which is that the utility model is a kind of, installs the structural schematic diagram one for folding the Fixed Wing AirVehicle undercarriage of sled additional.
Fig. 2, which is that the utility model is a kind of, installs the structural schematic diagram two for folding the Fixed Wing AirVehicle undercarriage of sled additional.
Fig. 3, which is that the utility model is a kind of, installs the structural schematic diagram three for folding the Fixed Wing AirVehicle undercarriage of sled additional.
Fig. 4, which is that the utility model is a kind of, installs the three of the structural schematic diagram three for folding the Fixed Wing AirVehicle undercarriage of sled additional View.
Description of symbols: the hydraulic rod piece 5- main rotating shaft of 1- vertical member 2- pair rotary shaft 3- rotary support 4- 6- rod piece 7- tire 8- sled 9- undercarriage ontology.
Specific embodiment
The preferred embodiment of the utility model is described in detail with reference to the accompanying drawing, so that the advantages of the utility model It can be easier to be readily appreciated by one skilled in the art with feature, to make the protection scope of the utility model apparent clear Define.
It is a kind of to install the Fixed Wing AirVehicle undercarriage for folding sled, including undercarriage ontology (9), tire (7), sled dress additional It sets, rotating device, tire (7) is located at undercarriage ontology (9) bottom, is carried out between tire (7) and undercarriage ontology (9) by axis Connection, ski device are symmetrically distributed in undercarriage ontology (9) two sides, and rotating dress is equipped between ski device, undercarriage ontology (9) It sets;
The ski device includes sled (8), rotary support (3), and rotary support (3) is set to sled (8) indent side, institute Rotary support (3) are stated for carrying out rotary folding to sled (8), keep sled (8) rotation described to undercarriage ontology (9) two sides Rotating device includes main rotating shaft (5), secondary rotary shaft (2), and secondary rotary shaft (2) connects with vertical member (1) one end axis, vertical member (1) other end is fixedly mounted in rotary support (3), and main rotating shaft (5) connects with rod piece (6) one end axis, and rod piece (6) other end is solid Surely it is connected on undercarriage ontology (9), connects between the main rotating shaft (5), secondary rotary shaft (2) by the way that hydraulic rod piece (4) are fixed It connects, the rotating device is used to rotate sled (8) to undercarriage ontology (9) bottom, and rotary support (3) and rotating device are mutual Cooperation can be realized the enabling and disabling of sled (8).
The utility model has conventional runway landing ability and snowfield landing ability, in conventional runway landing, two pieces Symmetrical sled (8) is received in undercarriage two sides, and all tire (7) contacts to earth.In snowfield landing, main rotating shaft (5) relative to Rod piece (6) rotation, so that hydraulic rod piece (4) be driven to rotate, secondary rotary shaft (2) is under the action of internal transmission mechanism with main rotation The identical angular speed rotation of axis (5), to drive vertical member (1) to rotate to direction identical with hydraulic rod piece (4), when hydraulic Rod piece (4) stops operating when rotating 180 degree, and rotary support (3) rotation stops, at this moment two sleds (8) are all arrived after being rotated by 90 ° Up to capable position is level with the ground, the flexible adjustment of hydraulic rod piece (4) touches sled (8) and ground.
Not limited to this, any change or replacement expected without creative work should all be covered in the utility model Protection scope within.Therefore, the protection scope of the utility model should be determined by the scope of protection defined in the claims.

Claims (2)

1. a kind of install the Fixed Wing AirVehicle undercarriage for folding sled, including undercarriage ontology (9), tire (7), sled dress additional It sets, rotating device, tire (7) is located at undercarriage ontology (9) bottom, is carried out between tire (7) and undercarriage ontology (9) by axis Connection, which is characterized in that ski device is symmetrically distributed in undercarriage ontology (9) two sides, ski device, undercarriage ontology (9) it Between be equipped with rotating device;The ski device includes sled (8), rotary support (3), and rotary support (3) is set to sled (8) indent Side, the rotating device include main rotating shaft (5), secondary rotary shaft (2), secondary rotary shaft (2) and vertical member (1) one end axis It connects, vertical member (1) other end is fixedly mounted in rotary support (3), and main rotating shaft (5) connects with rod piece (6) one end axis, rod piece (6) other end is fixedly connected on undercarriage ontology (9).
2. according to claim 1 install the Fixed Wing AirVehicle undercarriage for folding sled additional, which is characterized in that the main rotation It is fixedly connected between shaft (5), secondary rotary shaft (2) by hydraulic rod piece (4).
CN201821294998.0U 2018-08-13 2018-08-13 It is a kind of to install the Fixed Wing AirVehicle undercarriage for folding sled additional Expired - Fee Related CN208828091U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821294998.0U CN208828091U (en) 2018-08-13 2018-08-13 It is a kind of to install the Fixed Wing AirVehicle undercarriage for folding sled additional

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821294998.0U CN208828091U (en) 2018-08-13 2018-08-13 It is a kind of to install the Fixed Wing AirVehicle undercarriage for folding sled additional

Publications (1)

Publication Number Publication Date
CN208828091U true CN208828091U (en) 2019-05-07

Family

ID=66308973

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821294998.0U Expired - Fee Related CN208828091U (en) 2018-08-13 2018-08-13 It is a kind of to install the Fixed Wing AirVehicle undercarriage for folding sled additional

Country Status (1)

Country Link
CN (1) CN208828091U (en)

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20190507

Termination date: 20200813

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