CN206155815U

CN206155815U - Aircraft jato unit

Info

Publication number: CN206155815U
Application number: CN201621168651.2U
Authority: CN
Inventors: 张文渊
Original assignee: Individual
Current assignee: Individual
Priority date: 2016-11-02
Filing date: 2016-11-02
Publication date: 2017-05-10
Anticipated expiration: 2026-11-02

Abstract

The utility model provides an aircraft jato unit, belongs to space flight and aviation help -fly apparatus equipment technical field, including the runway, place recess, passive gyro wheel, driving belt, speedtransmitter, aircraft body, electronic cardboard, its characterized in that: top surface evenly distributed is equipped with a plurality of and places recess, every on the runway place the inside passive gyro wheel of the middle department's evenly distributed fixedly connected with a plurality of in top surface of controlling of recess, the winding of passive gyro wheel side top fixed surface has driving belt, around every place inside the recess each fixedly connected with speedtransmitter between the passive gyro wheel, the aircraft body has been placed on the top surface on the runway, the electronic cardboard of the inside rear fixedly connected with of runway enables the aircraft and takes off in the short distance, simple structure, and occupation space is few, is superior to steam and electromagnetic launch technique.

Description

A kind of aircraft jato unit

Technical field

This utility model belongs to Aero-Space help-fly apparatus technical field, and in particular to a kind of aircraft jato unit.

Background technology

In long-term working practice, pilot is driving an airplane in acceleration take-off process, and conventional airplane runway is long Degree is longer to the rate that breaks down is improved when taking off, and accelerates to make aero tyre serious wear for a long time on runway, it has not been convenient to Pilot operator is used and danger is taken off in raising.

The content of the invention

The purpose of this utility model is：Driving an airplane in acceleration take-off process to solve pilot, pilot Aircraft can be carried out in situ accelerating to reduce fault rate, it is possible to reduce aero tyre prevents from blowing out with the friction on ground, can make Aircraft takes off in short distance, simple structure, occupies little space, and better than steam and electromagnetic launch technology, technical scheme is as follows：

A kind of aircraft jato unit, it includes runway 1, places groove 2, passive roller 3, driving belt 4, speed biography Sensor 5, aircraft body 6, electronic clamp 7, it is characterised in that：Top end surface is evenly distributed and is provided with some on the runway 1 Individual placement groove 2, each described placement groove 2 inside left and right top end surface middle is evenly distributed and is fixedly connected with several quilts Dynamic roller 3, the side top end surface of the passive roller 3 is fixed and is wound with driving belt 4, before and after each inside the placement groove 2 Described passive roller 3 between be respectively fixedly connected with velocity sensor 5, top end surface is placed with aircraft on the runway 1 Body 6, the inside rear of the runway 1 is fixedly connected with electronic clamp 7, the placement internal depth of groove 2 and the quilt The overall diameter size of dynamic roller 3 is engaged, and the placement groove 2 is mutually permanently connected with the passive roller 3 by bearing, and each The side top end surface of the passive roller 3 is provided with brake gear, and the brake gear is fixedly connected on placement groove 2 side top End surfaces, and the position of groove 2 of placing is corresponding with the tire location of the lower section of the aircraft body 6, the electronic clamp 7 sets Put and be mutually permanently connected by rotating shaft with the runway 1 at placement groove 2 rear, and the electronic clamp 7, and the rotating shaft Right top end surface is fixedly connected with motor, and the top of the electronic clamp 7 is provided with sideboard, and the sideboard be inserted into it is winged Before the inside of machine runway 1 above top end surface, and the sideboard is connected with each other with the motor, each described driving belt 4 Upper top end surface is with top end surface on the runway 1 at grade.

The beneficial effects of the utility model are：Driving an airplane in acceleration take-off process to solve pilot, flying Office staff in situ can carry out in aircraft accelerating to reduce fault rate, it is possible to reduce aero tyre prevents from blowing out with the friction on ground, Aircraft can be made to take off in short distance, simple structure occupies little space, better than steam and electromagnetic launch technology.

Description of the drawings：

Fig. 1 is overall structure diagram of the present utility model.

Specific embodiment：

A kind of aircraft jato unit with reference to described in Fig. 1, it includes runway 1, places groove 2, passive roller 3, transmission Belt 4, velocity sensor 5, aircraft body 6, electronic clamp 7, it is characterised in that：Top end surface is average on the runway 1 It is distributed with several and places groove 2, each described placement groove 2 inside left and right top end surface middle is evenly distributed fixed company Several passive rollers 3 are connected to, the side top end surface of the passive roller 3 is fixed and is wound with driving belt 4, described before and after each to put Put and be respectively fixedly connected between the described passive roller 3 inside groove 2 velocity sensor 5, top end surface on the runway 1 Aircraft body 6 is placed with, the inside rear of the runway 1 is fixedly connected with electronic clamp 7, and the inside of placement groove 2 is deep Degree is engaged with the overall diameter size of the passive roller 3, and the placement groove 2 is interfixed with the passive roller 3 by bearing Connection, and each side top end surface of the passive roller 3 is provided with brake gear, and the brake gear is fixedly connected on described putting The side top end surface of groove 2 is put, and the position of groove 2 of placing is corresponding with the tire location of the lower section of the aircraft body 6, it is described Electronic clamp 7 is arranged on placement groove 2 rear, and the electronic clamp 7 and the runway 1 are interfixed company by rotating shaft Connect, and the right top end surface of the rotating shaft is fixedly connected with motor, the top of the electronic clamp 7 is provided with sideboard, and the work Dynamic baffle plate is inserted into top end surface top before the inside of runway 1, and the sideboard is connected with each other with the motor, each Top end surface is with top end surface on the runway 1 at grade on the driving belt 4.

When using, aircraft body 6 strong first is moved on runway 1, while the aero tyre in aircraft body 6 is stopped The top of groove 2 is being placed, while the electric motor starting on electronic clamp 7 rotates electronic clamp 7, the front end of electronic clamp 7 is being made and is flown The contact of machine tire support prevents aircraft body 6 from sliding backward, and then aircraft body 6 starts pusher aero tyre rotation simultaneously, Driving belt 4 is set to drive passive roller 3 to rotate simultaneously, then velocity sensor 5 sends when passive roller 3 rotates certain speed Signal makes brake gear moment that passive roller 3 to stop operating to brake gear, and the moment of last aircraft body 6 is in runway 1 On reach takeoff speed, while aircraft body 6 can quickly go up to the air.

Certainly, described above is not that, to restriction of the present utility model, this utility model is also not limited to the example above, Change, remodeling, addition or replacement that those skilled in the art are made in essential scope of the present utility model, also should Belong to protection domain of the present utility model.

Claims

1. a kind of aircraft jato unit, including runway（1）, place groove（2）, passive roller（3）, driving belt（4）, speed Degree sensor（5）, aircraft body（6）, electronic clamp（7）, it is characterised in that：The runway（1）Upper top end surface is average It is distributed with several and places groove（2）, each described placement groove（2）Internal left and right top end surface middle is evenly distributed solid Surely several passive rollers are connected with（3）, the passive roller（3）Side top end surface is fixed and is wound with driving belt（4）, each The placement groove in front and back（2）Internal described passive roller（3）Between be respectively fixedly connected with velocity sensor（5）, it is described to fly Machine runway（1）Upper top end surface is placed with aircraft body（6）, the runway（1）Internal rear is fixedly connected with electronic card Plate（7）.

2. a kind of aircraft jato unit according to claim 1, it is characterised in that：The placement groove（2）Internal depth with The passive roller（3）Overall diameter size is engaged, the placement groove（2）With the passive roller（3）It is mutually solid by bearing Fixed connection, and each described passive roller（3）Side top end surface is provided with brake gear, and the brake gear is fixedly connected on institute State placement groove（2）Side top end surface, and the placement groove（2）Position and the aircraft body（6）The tire location of lower section It is corresponding.

3. a kind of aircraft jato unit according to claim 1, it is characterised in that：The electronic clamp（7）It is arranged on placement Groove（2）Rear, and the electronic clamp（7）With the runway（1）It is mutually permanently connected by rotating shaft, and the rotating shaft is right Top end surface is fixedly connected with motor.

4. a kind of aircraft jato unit according to claim 3, it is characterised in that：The electronic clamp（7）Top is provided with work Dynamic baffle plate, and the sideboard is inserted into runway（1）Top end surface top before internal, and the sideboard with it is described Motor is connected with each other.

5. a kind of aircraft jato unit according to claim 3, it is characterised in that：Each described driving belt（4）Upper top Surface and the runway（1）Upper top end surface is at grade.