Invention content
The technical problem to be solved in the present invention is to provide a kind of Novel fire fighting apparatus, can solve above-mentioned show in the art
The problem of.
To solve the above problems, the present invention adopts the following technical scheme that:A kind of Novel fire fighting apparatus of the present invention, including machine
Body, is provided with traction structure in the fuselage, and the traction structure includes slid chamber and the sliding that is arranged in the slid chamber
Bar, the sliding bar and slid chamber sliding are connected, and the slid chamber right end connects outside, and the sliding bar right end is stretched
Go out the slid chamber and bottom hinge is connected with montant, the montant bottom is fixedly installed dilatory hook, the slid chamber top
It connects and is provided with guide runner, the sliding bar top left is fixedly installed protruding block, and the protruding block and the guide runner are slided
It moves and is connected, connected on the left of the slid chamber and be provided with the first hollow cavity, what can be circled round in first hollow cavity is provided with
First rotary shaft, first rotary shaft periphery are fixedly installed drop center wheel, and the sliding bar left end is fixedly connected with drawstring, institute
It states drawstring left end to be wound on the drop center wheel, is connected on the left of first hollow cavity and be provided with the second hollow cavity, described second is empty
It is connected on the left of the chambers of the heart and is provided with third hollow cavity, the first motor, first horse are fixedly installed on the left of the third hollow cavity
It is connected with the second rotary shaft up to right side power, second rotary shaft is put in the right in the third hollow cavity and described
Two rotary shaft right ends are fixedly installed the first toe joint wheel, are provided in the third hollow cavity and are engaged company with the first toe joint wheel
The the second toe joint wheel connect, the second toe joint wheel right side are fixedly installed stud, and the stud extends to the right and with described
Inner wall can circle round matings connection on the right side of two hollow cavities, and spiral shell type line is connected with slipping block on the stud, the slipping block and
The second hollow cavity sliding is connected, and the conversion chamber of right openings, the conversion intracavitary top are provided in the slipping block
The second motor is fixedly installed in wall, second motor bottom power is connected with third rotary shaft, the third convolution
Axis bottom and the conversion intracavitary bottom wall can circle round mating connection, and third rotary shaft periphery is fixedly installed the first flute profile
Wheel, is provided with the second flute profile wheel being connected with the first flute profile wheel in the conversion chamber, above and below the second flute profile wheel
Logical provide is equipped with the 4th rotary shaft, and the 4th rotary shaft and the conversion chamber roof and bottom wall can circle round mating connection, institute
It states fuselage roof end face position of keeping right and is fixedly installed mounting seat, the mounting seat top surface is fixedly installed warning flicker
Lamp, the warning flashing lamp are connect with the fuselage interior electric power, and noise abatement cushioning device is provided on first motor.
The drop center wheel lateral surface setting is with teeth as a preferred technical solution, the second flute profile wheel and the groove
Wheel is connected.
Second rotary shaft is connect with the fuselage inner wall clearance fit as a preferred technical solution,.
The noise abatement cushioning device includes being fixed at first motor both sides up and down as a preferred technical solution,
The noise abatement pad in face and the bradyseism plate for being fixed at first motor front and rear sides face, the noise abatement pad and the bradyseism plate phase
Connection.
The beneficial effects of the invention are as follows:
1. by controlling the first motor running, the first motor drives the second rotary shaft and the convolution of the first toe joint wheel, the first toe joint
Wheel drives the convolution of the second toe joint wheel, the convolution of the second toe joint wheel to drive stud convolution, stud that slipping block is driven to slide to the left, the second tooth
Type wheel is disconnected with drop center wheel, can pull out sliding bar at this time, and dilatory hook is fixedly connected with barrier, then controls
One motor antiport, the first motor drive the second rotary shaft and the first toe joint wheel reversely to circle round, and the first toe joint wheel drives the
Two toe joint wheels reversely circle round, and the convolution of the second toe joint wheel drives stud convolution, and stud drives slipping block to slide to the right, until the second tooth
Type wheel is connected with drop center wheel, then controls the second motor operations, and the second motor drives third rotary shaft and the first flute profile wheel
Convolution, the first flute profile wheel drive the second flute profile wheel convolution, the second flute profile wheel drive drop center wheel circle round coiling, to by around rise
Drawstring drives in sliding bar retraction slid chamber, to by barrier be dragged to distance similar in fuselage, then advanced band by fuselage
Dynamic barrier advances, and since the second motor does not work, the first flute profile wheel, the second flute profile wheel and drop center wheel are all kept fixed
It is motionless, ensure the stabilization of heave.
2. overall structure of the present invention is simple, easy to use, heave is stablized, and draws efficient.
Specific implementation mode
The preferred embodiment of the present invention is described in detail below in conjunction with the accompanying drawings, so that advantages and features of the invention energy
It is easier to be readily appreciated by one skilled in the art, so as to make a clearer definition of the protection scope of the present invention.
A kind of Novel fire fighting apparatus shown in -3 refering to fig. 1, including fuselage 10 are provided with dilatory knot in the fuselage 10
Structure, the traction structure include slid chamber 34 and the sliding bar 33 that is arranged in the slid chamber 34, the sliding bar 33 and institute
It states the sliding of slid chamber 34 to be connected, 34 right end of the slid chamber connects outside, and 33 right end of sliding bar stretches out the sliding
Chamber 34 and bottom hinge are connected with montant 35, and 35 bottom of the montant is fixedly installed dilatory hook 36,34 top of the slid chamber
It connects and is provided with guide runner 34,33 top left of sliding bar is fixedly installed protruding block 32, the protruding block 32 and described
The sliding of guide runner 34 is connected, and 34 left side of the slid chamber, which connects, is provided with the first hollow cavity 43, first hollow cavity 43
In can circle round be provided with the first rotary shaft 16,16 periphery of the first rotary shaft is fixedly installed drop center wheel 30, the sliding
33 left end of bar is fixedly connected with drawstring 31, and 31 left end of the drawstring is wound on the drop center wheel 30, and first hollow cavity 43 is left
Side, which connects, is provided with the second hollow cavity 24, and second hollow cavity, 24 left side, which connects, is provided with third hollow cavity 21, the third
21 left side of hollow cavity is fixedly installed the first motor 18, and 18 right side power of the first motor is connected with the second rotary shaft
19, second rotary shaft 19 is put in the right in the third hollow cavity 21 and 19 right end of the second rotary shaft is fixedly installed
First toe joint wheel 20 is provided with the second toe joint wheel being connected with the first toe joint wheel 20 in the third hollow cavity 21
22,22 right side of the second toe joint wheel is fixedly installed stud 23, the stud 23 extend to the right and with it is described second hollow
24 right side inner wall of chamber can circle round mating connection, and spiral shell type line is connected with slipping block 25, the slipping block 25 on the stud 23
It slides and is connected with second hollow cavity 24, be provided with the conversion chamber 14 of right openings in the slipping block 25, described turn
Change in 14 inner roof wall of chamber and be fixedly installed the second motor 26, second motor, 26 bottom power is connected with third rotary shaft
28,28 bottom of third rotary shaft and 14 inner bottom wall of conversion chamber can circle round mating connection, outside the third rotary shaft 28
It is fixedly installed the first flute profile wheel 27 week, second to be connected with the first flute profile wheel 27 is provided in the conversion chamber 14
Flute profile wheel 29, logical provide of about 29 the second flute profile wheel are equipped with the 4th rotary shaft 17, the 4th rotary shaft 17 with described turn
Changing 14 roof of chamber and bottom wall can circle round mating connection, and 10 top end surface of fuselage position of keeping right is fixedly installed mounting seat
11,11 top surface of the mounting seat, which is fixedly installed, warns flashing lamp 12, inside the warning flashing lamp 12 and the fuselage 10
Electric power connects, and noise abatement cushioning device is provided on first motor 18.
Wherein, with teeth, the second flute profile wheel 29 and 30 company of occlusion of the drop center wheel is arranged in 30 lateral surface of the drop center wheel
It connects.
Wherein, second rotary shaft 19 is connect with 10 inner wall clearance fit of the fuselage.
Wherein, the noise abatement cushioning device includes the noise abatement pad for being fixed at first motor, about 18 two sides
181 and it is fixed at the bradyseism plate 182 in first motor, 18 front and rear sides face, the noise abatement pad 181 and the bradyseism plate
182 are connected, and the noise abatement cushioning device can effectively reduce the noise and vibrations that the operating of the first motor 18 generates.
In the initial state, the slipping block 25 is located at 24 rightmost side of the second hollow cavity, second tooth to the present apparatus
Type wheel 29 is connected with the drop center wheel 30, and the sliding bar 33 is fixed.
When needing dilatory, controls first motor 18 and operate, first motor 18 drives second rotary shaft
19 and the first toe joint wheel 20 convolution, the first toe joint wheel 20 drive the second toe joint wheel 22 to circle round, described second
The convolution of toe joint wheel 22 drives the stud 23 to circle round, and the stud 23 drives the slipping block 25 to slide to the left, second tooth
Type wheel 29 is disconnected with the drop center wheel 30, can pull out the sliding bar 33 at this time, and by dilatory hook 36 and barrier
Be fixedly connected, then control 18 antiport of the first motor, first motor 18 drive second rotary shaft 19 and
The first toe joint wheel 20 reversely circles round, and the first toe joint wheel 20 drives the second toe joint wheel 22 reversely to circle round, and described the
The convolution of two toe joint wheels 22 drives the stud 23 to circle round, and the stud 23 drives the slipping block 25 to slide to the right, until described
Second flute profile wheel 29 is connected with the drop center wheel 30, then controls second motor 26 and work, 26 band of the second motor
It moves the third rotary shaft 28 and the first flute profile wheel 27 convolution, the first flute profile wheel 27 drives the second flute profile wheel
29 convolutions, the second flute profile wheel 29 drives the convolution coiling of the drop center wheel 30, to by being driven around the drawstring 31 risen
The sliding bar 33 is retracted in the slid chamber 34, to by barrier be dragged to distance similar in the fuselage 10, then pass through
The fuselage 10, which advances, drives barrier to advance, since second motor 26 does not work, the first flute profile wheel 27, institute
It states the second flute profile wheel 29 and the drop center wheel 30 all remains stationary, ensure the stabilization of heave.
The beneficial effects of the invention are as follows:
1. by controlling the first motor running, the first motor drives the second rotary shaft and the convolution of the first toe joint wheel, the first toe joint
Wheel drives the convolution of the second toe joint wheel, the convolution of the second toe joint wheel to drive stud convolution, stud that slipping block is driven to slide to the left, the second tooth
Type wheel is disconnected with drop center wheel, can pull out sliding bar at this time, and dilatory hook is fixedly connected with barrier, then controls
One motor antiport, the first motor drive the second rotary shaft and the first toe joint wheel reversely to circle round, and the first toe joint wheel drives the
Two toe joint wheels reversely circle round, and the convolution of the second toe joint wheel drives stud convolution, and stud drives slipping block to slide to the right, until the second tooth
Type wheel is connected with drop center wheel, then controls the second motor operations, and the second motor drives third rotary shaft and the first flute profile wheel
Convolution, the first flute profile wheel drive the second flute profile wheel convolution, the second flute profile wheel drive drop center wheel circle round coiling, to by around rise
Drawstring drives in sliding bar retraction slid chamber, to by barrier be dragged to distance similar in fuselage, then advanced band by fuselage
Dynamic barrier advances, and since the second motor does not work, the first flute profile wheel, the second flute profile wheel and drop center wheel are all kept fixed
It is motionless, ensure the stabilization of heave.
2. overall structure of the present invention is simple, easy to use, heave is stablized, and draws efficient.
The basic principles, main features and advantages of the present invention have been shown and described above.The technology of the industry
Personnel are it should be appreciated that the present invention is not limited to the above embodiments, and the above embodiments and description only describe this
The principle of invention, various changes and improvements may be made to the invention without departing from the spirit and scope of the present invention, these changes
Change and improvement all fall within the protetion scope of the claimed invention.The claimed scope of the invention by appended claims and its
Equivalent defines.