CN109018386A - A kind of anticollision mechanism of fuel tanker - Google Patents
A kind of anticollision mechanism of fuel tanker Download PDFInfo
- Publication number
- CN109018386A CN109018386A CN201810888736.5A CN201810888736A CN109018386A CN 109018386 A CN109018386 A CN 109018386A CN 201810888736 A CN201810888736 A CN 201810888736A CN 109018386 A CN109018386 A CN 109018386A
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- China
- Prior art keywords
- cavity
- fixedly connected
- litter
- fuel tanker
- pedestal
- 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.)
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Links
- 239000000446 fuel Substances 0.000 title claims abstract description 39
- 230000007246 mechanism Effects 0.000 title claims abstract description 33
- 239000000872 buffer Substances 0.000 claims abstract description 49
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 32
- 238000009434 installation Methods 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 2
- 230000006978 adaptation Effects 0.000 claims 1
- 230000005611 electricity Effects 0.000 claims 1
- 239000002828 fuel tank Substances 0.000 abstract description 19
- 238000000034 method Methods 0.000 description 7
- 230000008569 process Effects 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005389 magnetism Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Feeding And Controlling Fuel (AREA)
Abstract
The invention discloses a kind of anticollision mechanisms of fuel tanker, are related to fuel tanker technical field, including fuel tanker ontology, and the right side of the fuel tanker ontology is fixedly installed with fixed mechanism, and the right side of the fixed mechanism is fixedly installed with buffer gear.The anticollision mechanism of the fuel tanker, by being provided with the first litter, with the use of the first slip ring, the second slide block movement can be made more convenient, avoid the problem that Caton occurs during exercise in the second sliding block, by being provided with baffle, the second litter can be effectively avoided to slip the second slip ring, movable plate movement can be made more steady, by being provided with buffer gear, it can be avoided plug-in auxiliary fuel tank and auxiliary fuel tank damage occurred by bird strike, fuel leakage etc. influences the case where aircraft safety, improve the security performance of the device, by being provided with fixed mechanism, can make buffer gear disassembly overhaul it is more convenient, buffer gear is avoided to damage, avoiding the device, there are security risks.
Description
Technical field
The present invention relates to fuel tanker technical field, specially a kind of anticollision mechanism of fuel tanker.
Background technique
Auxiliary fuel tank refer to hang over the centre below fuselage or wing slightly and streamlined fuel tank pointed at both ends.Hang auxiliary fuel tank
Flight and cruise duration can be increased, and aircraft can throw away auxiliary fuel tank in air battle when necessary, with preferable
Mobility go into battle, the installation kenel of auxiliary fuel tank is segmented into two classes: can not abandon and can abandon, match in addition to early stage
Close fuselage shape and design can not other than disposal type auxiliary fuel tank, all with streamlined for main design direction in exterior design,
For the resistance that must be generation to be reduced, to airplane motion and stable negative effect, reduction hits other when separating with aircraft
Carry equipment either airframe structure etc..Some auxiliary fuel tanks have the small-sized fixed aerofoil of balance in tail portion, are exactly in function
In order to reach purpose above-mentioned.
During use, often there is the poor problem of crashworthiness in common fuel tanker, aircraft in flight,
If plug-in auxiliary fuel tank is by bird strike, it may occur that the case where auxiliary fuel tank damages, and fuel leakage etc. influences aircraft safety,
Therefore, it is proposed that a kind of anticollision mechanism of fuel tanker solves the problems, such as this.
Summary of the invention
The object of the invention is in order to make up for the deficiencies of the prior art, provide a kind of anticollision mechanism of fuel tanker,
It has the advantages that crashworthiness is good, solves the problems, such as that existing fuel tanker crashworthiness is poor.
The present invention is in order to solve the above technical problems, provide the following technical solutions: a kind of anticollision mechanism of fuel tanker, including
Fuel tanker ontology, the right side of the fuel tanker ontology are fixedly installed with fixed mechanism, the right side of the fixed mechanism
It is fixedly installed with buffer gear.
The buffer gear includes buffer stopper, the first sliding block, pedestal, positioning pipe, the first electromagnetism column, the first cavity, positioning
Column, the second cavity, the second electromagnetism column, the first litter, buffer spring, first sliding groove, second sliding slot, the second sliding block and first are sliding
Ring.
The fixed mechanism includes fixed block, mounting rod, the first pin shaft, clockwise and anticlockwise motor, threaded rod, baffle, the second pin
Axis, push-pull rod, connecting tube, screwed pipe, card slot, bearing, fixture block, the second slip ring, the first limit hole, through-hole, the second limit hole, sky
Chamber, mounting plate, gag lever post, movable plate and the second litter.
Further, the right side of the fuel tanker ontology is fixedly connected with fixed block, puts on the right side of the fixed block
It is equipped with pedestal, the inside of the fixed block offers cavity, and the right side of the fixed block is opened up there are two symmetrical through-hole,
And two through-holes are connected with cavity, the left side of the pedestal is fixedly connected there are two symmetrical mounting rod, two institutes
The left end for stating mounting rod extends through two through-holes and extends to the inside of cavity, and the upper surface of two mounting rods opens up
There is the first limit hole, the inner sidewall of the cavity is fixedly connected with that there are two symmetrical mounting plates, and two mounting plates are respectively positioned on
Between two through-holes, the fixation of the upper surface of each mounting plate is inlaid with connecting tube, places between two mounting plates
There are two symmetrical gag lever post, the inner roof wall and inner bottom wall of the cavity offer the second limit hole, two limits
One end that bar is located remotely from each other sequentially passes through connecting tube and the first limit hole respectively and extends to two mounting rods are located remotely from each other one
Side, and two gag lever posts socket-connect with two connecting tubes respectively, one end that two gag lever posts are located remotely from each other is located at two
The inside of a second limit hole, the inner sidewall of the cavity are fixedly connected with clockwise and anticlockwise motor, the right side of the clockwise and anticlockwise motor
Face is placed with movable plate, and movable plate is located between two mounting plates, and the right side fixation of the mounting plate is inlaid with screwed pipe,
The output end of the clockwise and anticlockwise motor is fixedly connected with threaded rod, and the right end of the threaded rod through screwed pipe and extends to movement
The right side of plate, and threaded rod is threadedly coupled with screwed pipe, the right side of the movable plate is fixed to inlay that there are two symmetrical the
Two slip rings, the inner sidewall of the cavity are fixedly connected there are two the second symmetrical litter, the left end of two second litter
It extends through two the second slip rings and extends to the left side of movable plate, and two the second litter are nested with two the second slip rings respectively
It connects, the top of the movable plate and the outer surface of bottom end pass through the second pin shaft and be fixedly hinged with push-pull rod, two push-and-pulls
The outer surface that bar is located remotely from each other one end passes through the fixed hinge in outer surface of the first pin shaft and two gag lever post one end close to each other respectively
It connects.
By using above-mentioned technical proposal, buffer gear disassembly can be made overhaul more convenient, avoid buffer gear
It damages, avoids the device there are security risk, keep its easy to use.
Further, the right side of the pedestal offers the first cavity, and the inner sidewall of first cavity is fixedly connected
There is the first electromagnetism column, buffer stopper is placed on the right side of the pedestal, the left side of the buffer stopper offers the second cavity, described
The inner sidewall of second cavity is fixedly connected with the second electromagnetism column, and it is sliding that the right side of the pedestal offers annular in shape first
Slot, the left side of the buffer stopper is fixedly connected with the first sliding block compatible with first sliding groove, and the first sliding block is connected to
The inside of one sliding slot, the inner roof wall and inner bottom wall of the first sliding groove offer second sliding slot, the upper surface of first sliding block
It is fixedly connected to the second sliding block compatible with second sliding slot with bottom surface, and the second sliding block is connected to the inside of second sliding slot,
The left side of first sliding block is fixedly connected with buffer spring, and the left end of the buffer spring and the inner sidewall of first sliding groove are solid
Fixed connection.
By using above-mentioned technical proposal, it can be avoided plug-in auxiliary fuel tank by bird strike and auxiliary fuel tank damage, combustion occur
The case where oil leakage etc. influences aircraft safety, improves the security performance of the device.
Further, the right side of each second sliding block is fixed is inlaid with the first slip ring, and each described second is sliding
The inner sidewall of slot is fixedly connected to the first litter, and the first litter socket-connects with the first slip ring.
By using above-mentioned technical proposal, the second slide block movement can be made more convenient, avoid the second sliding block during exercise
There is the problem of Caton.
Further, the right side fixation of the pedestal is inlaid with two groups of symmetrical positioning pipes, a left side for the buffer stopper
Side is fixedly connected with two groups of symmetrical positioning columns, and the left end of positioning column described in every group is located at the interior of two positioning pipes
Portion, and positioning column socket-connects with positioning pipe.
By using above-mentioned technical proposal, the movement of the first litter can be made more steady, avoid the first litter during exercise
The problem of tilting.
Further, the inner sidewall fixation of the cavity is inlaid with bearing, the outer surface of the threaded rod right end and bearing
Inner ring be fixedly connected.
By using above-mentioned technical proposal, threaded rod rotation can be made more steady, avoid threaded rod appearance in rotation
The problem of shaking, improves the stability of threaded rod.
Further, the right side of the fixed block offers card slot, and the left side of the pedestal is fixedly connected with fixture block,
And fixture block is connected to the inside of card slot.
By using above-mentioned technical proposal, it can effectively avoid fixture block from occurring shaking problem at steady state, improve
The stability and safety of the device.
Further, the left side of each second litter is fixedly connected to baffle, the vertical length of the baffle
Value is greater than the vertical length value of the second slip ring.
By using above-mentioned technical proposal, it can effectively avoid the second litter from slipping the second slip ring, movable plate can be made to move
It is dynamic more steady.
Compared with prior art, the anticollision mechanism of the fuel tanker have it is following the utility model has the advantages that
1, the present invention is used cooperatively positioning column, the movement of the first litter can be made more steady, kept away by being provided with positioning pipe
Exempt from the problem of the first litter tilts during exercise, improve the stability of the device, by being provided with the first litter, cooperates
Using the first slip ring, the second slide block movement can be made more convenient, avoid the problem that Caton occurs during exercise in the second sliding block.
2, the present invention can effectively avoid the second litter from slipping the second slip ring, can make movable plate by being provided with baffle
Movement is more steady, by being provided with card slot, is used cooperatively fixture block, effectively fixture block can be avoided to shake at steady state
Problem improves the stability and safety of the device.
3, the present invention can effectively avoid external rubbish from entering the first cavity and the second cavity by being provided with the first sliding block
Inside, ensure that the first electromagnetism column and the second electromagnetism column can work normally, by being provided with bearing, can make threaded rod turn
It is dynamic more steady, it avoids the problem that threaded rod shakes in rotation, improves the stability of threaded rod.
4, the present invention can be avoided plug-in auxiliary fuel tank by bird strike and auxiliary fuel tank damage occur by being provided with buffer gear
It is bad, fuel leakage etc. influence aircraft safety the case where, the security performance of the device is improved, by being provided with fixed mechanism, energy
So that buffer gear disassembly overhaul more convenient, avoids buffer gear from damaging, avoiding the device, there are security risks.
Detailed description of the invention
Fig. 1 is the main view of fuel tanker ontology of the present invention；
Fig. 2 is the sectional view of pedestal main view of the present invention；
Fig. 3 is structure enlargement diagram at A in Fig. 2 of the present invention；
Fig. 4 is the sectional view of fixed block main view of the present invention；
Fig. 5 is structure enlargement diagram at B in Fig. 4 of the present invention.
In figure: 1- buffer gear, 101- buffer stopper, the first sliding block of 102-, 103- pedestal, 104- positioning pipe, 105- first
Electromagnetism column, the first cavity of 106-, 107- positioning column, the second cavity of 108-, 109- the second electromagnetism column, the first litter of 110-, 111-
Buffer spring, 112- first sliding groove, 113- second sliding slot, the second sliding block of 114-, the first slip ring of 115-, 2- fixed mechanism, 201-
Fixed block, 202- mounting rod, the first pin shaft of 203-, 204- clockwise and anticlockwise motor, 205- threaded rod, 206- baffle, 207- second are sold
Axis, 208- push-pull rod, 209- connecting tube, 210- screwed pipe, 211- card slot, 212- bearing, 213- fixture block, the second slip ring of 214-,
The first limit hole of 215-, 216- through-hole, the second limit hole of 217-, 218- cavity, 219- mounting plate, 220- gag lever post, 221- are moved
Movable plate, the second litter of 222-, 3- fuel tanker ontology.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Fig. 1-5 is please referred to, the present invention provides a kind of technical solution: a kind of anticollision mechanism of fuel tanker, including aircraft oil
Case ontology 3, the right side of fuel tanker ontology 3 are fixedly installed with fixed mechanism 2, and the right side of fixed mechanism 2 is fixedly installed with
Buffer gear 1.
Buffer gear 1 includes buffer stopper 101, the first sliding block 102, pedestal 103, positioning pipe 104, the first electromagnetism column 105, the
One cavity 106, positioning column 107, the second cavity 108, the second electromagnetism column 109, the first litter 110, buffer spring 111, first are sliding
Slot 112, second sliding slot 113, the second sliding block 114 and the first slip ring 115.
Fixed mechanism 2 include fixed block 201, mounting rod 202, the first pin shaft 203, clockwise and anticlockwise motor 204, threaded rod 205,
Baffle 206, the second pin shaft 207, push-pull rod 208, connecting tube 209, screwed pipe 210, card slot 211, bearing 212, fixture block 213,
Two slip rings 214, through-hole 216, the second limit hole 217, cavity 218, mounting plate 219, gag lever post 220, move first limit hole 215
Movable plate 221 and the second litter 222.
Further, the right side of fuel tanker ontology 3 is fixedly connected with fixed block 201, and the right side of fixed block 201 is placed
There is a pedestal 103, the inside of fixed block 201 offers cavity 218, and the right side of fixed block 201 opens up that there are two symmetrical logical
Hole 216, and two through-holes 216 are connected with cavity 218, the left side of pedestal 103 are fixedly connected with that there are two symmetrical peaces
Bar 202 is filled, the left end of two mounting rods 202 extends through two through-holes 216 and extends to the inside of cavity 218, two installations
The upper surface of bar 202 offers the first limit hole 215, and the inner sidewall of cavity 218 is fixedly connected with that there are two symmetrical installations
Plate 219, and two mounting plates 219 are respectively positioned between two through-holes 216, the fixation of the upper surface of each mounting plate 219 is inlaid with
Connecting tube 209, places that there are two symmetrical gag lever post 220, the inner roof wall of cavity 218 and interior bottoms between two mounting plates 219
Wall offers the second limit hole 217, and one end that two gag lever posts 220 are located remotely from each other sequentially passes through connecting tube 209 and respectively
One limit hole 215 simultaneously extends to the side that two mounting rods 202 are located remotely from each other, and two gag lever posts 220 are connect with two respectively
Pipe 209 socket-connects, and one end that two gag lever posts 220 are located remotely from each other is located at the inside of two the second limit holes 217, cavity
218 inner sidewall is fixedly connected with clockwise and anticlockwise motor 204, and the right side of clockwise and anticlockwise motor 204 is placed with movable plate 221, and moves
Movable plate 221 is located between two mounting plates 219, and the right side fixation of mounting plate 219 is inlaid with screwed pipe 210, clockwise and anticlockwise motor
204 output end is fixedly connected with threaded rod 205, and the right end of threaded rod 205 through screwed pipe 210 and extends to movable plate 221
Right side, and threaded rod 205 is threadedly coupled with screwed pipe 210, and the right side of movable plate 221 is fixed to inlay that there are two symmetrical
Second slip ring 214, the inner sidewall of cavity 218 are fixedly connected there are two the second symmetrical litter 222, two the second litter 222
Left end extend through two the second slip rings 214 and extend to the left side of movable plate 221, and two the second litter 222 respectively with
Two the second slip rings 214 socket-connect, and the top of movable plate 221 and the outer surface of bottom end pass through 207 fixed hinge of the second pin shaft
There is push-pull rod 208, the outer surface that two push-pull rods 208 are located remotely from each other one end passes through the first pin shaft 203 and two gag lever posts respectively
The outer surface fixed hinge of 220 one end close to each other can make the disassembly of buffer gear 1 overhaul more convenient, avoid buffering
Mechanism 1 damages, and avoids the device there are security risk, keeps its easy to use.
Further, the right side of pedestal 103 offers the first cavity 106, and the inner sidewall of the first cavity 106 is fixedly connected
There is the first electromagnetism column 105, the first electromagnetism column 105 is switched on a kind of device for generating electromagnetism, in being externally wrapped with and its function for iron core
The conductive winding that rate matches, this coil to alive have magnetism as magnet, and the right side of pedestal 103 is placed with slow
Block 101 is rushed, the left side of buffer stopper 101 offers the second cavity 108, and the inner sidewall of the second cavity 108 is fixedly connected with second
Electromagnetism column 109, the second electromagnetism column 109 is switched on a kind of device for generating electromagnetism, in being externally wrapped with and its power phase for iron core
The conductive winding matched, this coil to alive have magnetism as magnet, and the right side of pedestal 103 is offered in annulus
The first sliding groove 112 of shape, the left side of buffer stopper 101 are fixedly connected with first sliding block 102 compatible with first sliding groove 112,
And first sliding block 102 be connected to the inside of first sliding groove 112, it is sliding that the inner roof wall and inner bottom wall of first sliding groove 112 offer second
Slot 113, the upper surface and bottom surface of the first sliding block 102 are fixedly connected to second sliding block 114 compatible with second sliding slot 113,
And second sliding block 114 be connected to the inside of second sliding slot 113, the left side of the first sliding block 102 is fixedly connected with buffer spring
111, the left end of buffer spring 111 is fixedly connected with the inner sidewall of first sliding groove 112, can be avoided plug-in auxiliary fuel tank by flying bird
The case where auxiliary fuel tank damage occurs for shock, and fuel leakage etc. influences aircraft safety, improves the security performance of the device.
Further, the right side of each second sliding block 114 fixation is inlaid with the first slip ring 115, each second sliding slot
113 inner sidewall is fixedly connected to the first litter 110, and the first litter 110 socket-connects with the first slip ring 115, can make
Two sliding blocks 114 move more convenient, avoid the problem that Caton occurs during exercise in the second sliding block 114.
Further, the right side fixation of pedestal 103 is inlaid with two groups of symmetrical positioning pipes 104, a left side for buffer stopper 101
Side is fixedly connected with two groups of symmetrical positioning columns 107, and the left end of every group of positioning column 107 is located at two positioning pipes 104
Inside, and positioning column 107 socket-connects with positioning pipe 104, and the movement of the first litter 101 can be made more steady, avoids first sliding
The problem of pole 101 tilts during exercise.
Further, the inner sidewall fixation of cavity 218 is inlaid with bearing 212, the outer surface of 205 right end of threaded rod and bearing
212 inner ring is fixedly connected, and the rotation of threaded rod 205 can be made more steady, and threaded rod 205 is avoided to occur shaking in rotation
Problem improves the stability of threaded rod 205.
Further, the right side of fixed block 201 offers card slot 211, and the left side of pedestal 103 is fixedly connected with fixture block
213, and fixture block 213 is connected to the inside of card slot 211, can effectively avoid fixture block 213 from occurring shaking problem at steady state,
Improve the stability and safety of the device.
Further, the left side of each second litter 222 is fixedly connected to baffle 206, the vertical length of baffle 206
Value is greater than the vertical length value of the second slip ring 214, can effectively avoid the second litter 222 from slipping the second slip ring 214, can make to move
The movement of movable plate 221 is more steady.
Working principle: clockwise and anticlockwise motor 204, the first electromagnetism column 105 and the second electromagnetism column 109 are connected to the battery it is logical,
Buffer stopper 101 is held mounting rod 202 from the inside of the insertion cavity 218 of through-hole 216 by staff, is inserted into fixture block 213
The inside of card slot 211, clockwise and anticlockwise motor 204, which is powered to starting, drives threaded rod 205 to rotate, in screwed pipe 210, the first pin shaft 203
Under the action of the second pin shaft 207, movable plate 221 is made to drive push-pull rod 208 that gag lever post 220 is pushed to pass through the first limit hole 215
Into the inside of the second limit hole 217, the first electromagnetism column 105 and the second electromagnetism column 109 are powered and start, and utilize the remote of homopolar-repulsion
From making buffer stopper 101 and pedestal 103 keep a fixed spacing, impact force generated when flying bird knocks buffer stopper 101, due to homopolarity phase
Reprimand buffers buffer stopper 101, pushes the movement of buffer spring 111 to carry out secondary buffer by the first sliding block 102, avoids plug-in pair
The case where by bird strike auxiliary fuel tank damage is occurred for fuel tank, and fuel leakage etc. influences aircraft safety, improves the peace of the device
Full performance keeps its easy to use.
In the description of the present invention, the terms "include", "comprise" or its any other variant are intended to nonexcludability
Include so that include a series of elements process, method, article or equipment not only include those elements, but also
Including other elements that are not explicitly listed, or further include for this process, method, article or equipment intrinsic want
Element.In the absence of more restrictions, the element limited by sentence " including a reference structure ", it is not excluded that including institute
State in the process, method, article or equipment of element that there is also other identical elements.It should be noted that, in this document, all
As the relational terms of " first ", " second " or the like are used merely to an entity or operation and another entity or operating space
It separates, without necessarily requiring or implying between these entities or operation, there are any actual relationship or orders.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (8)
1. a kind of anticollision mechanism of fuel tanker, including fuel tanker ontology (3), it is characterised in that: the fuel tanker ontology
(3) right side is fixedly installed with fixed mechanism (2), and the right side of the fixed mechanism (2) is fixedly installed with buffer gear
(1)；The buffer gear (1) includes buffer stopper (101), the first sliding block (102), pedestal (103), positioning pipe (104), the first electricity
Magnetic pole (105), the first cavity (106), positioning column (107), the second cavity (108), the second electromagnetism column (109), the first litter
(110), buffer spring (111), first sliding groove (112), second sliding slot (113), the second sliding block (114) and the first slip ring (115)；
The fixed mechanism (2) include fixed block (201), mounting rod (202), the first pin shaft (203), clockwise and anticlockwise motor (204),
Threaded rod (205), baffle (206), the second pin shaft (207), push-pull rod (208), connecting tube (209), screwed pipe (210), card slot
(211), bearing (212), fixture block (213), the second slip ring (214), the first limit hole (215), through-hole (216), the second limit hole
(217), cavity (218), mounting plate (219), gag lever post (220), movable plate (221) and the second litter (222).
2. a kind of anticollision mechanism of fuel tanker as described in claim 1, it is characterised in that: the fuel tanker ontology (3)
Right side be fixedly connected with fixed block (201), be placed with pedestal (103), the fixed block on the right side of the fixed block (201)
(201) inside offers cavity (218), and the right side of the fixed block (201) is opened up there are two symmetrical through-hole
(216), and two through-holes (216) are connected with cavity (218), there are two the left side of the pedestal (103) is fixedly connected
Symmetrical mounting rod (202), the left end of two mounting rods (202) extend through two through-holes (216) and extend to sky
The upper surface of the inside of chamber (218), two mounting rods (202) offers the first limit hole (215), the cavity
(218) inner sidewall is fixedly connected there are two symmetrical mounting plate (219), and two mounting plates (219) be respectively positioned on two it is logical
Between hole (216), the fixation of the upper surface of each mounting plate (219) is inlaid with connecting tube (209), two mounting plates
(219) it is placed between there are two symmetrical gag lever post (220), the inner roof wall and inner bottom wall of the cavity (218) offer
Second limit hole (217), one end that two gag lever posts (220) are located remotely from each other sequentially pass through connecting tube (209) and respectively
One limit hole (215) simultaneously extends to the side that two mounting rods (202) are located remotely from each other, and two gag lever posts (220) are respectively with two
A connecting tube (209) socket-connects, and one end that two gag lever posts (220) are located remotely from each other is located at two the second limit holes
(217) inner sidewall of inside, the cavity (218) is fixedly connected with clockwise and anticlockwise motor (204), the clockwise and anticlockwise motor
(204) right side is placed with movable plate (221), and movable plate (221) is located between two mounting plates (219), the installation
The right side fixation of plate (219) is inlaid with screwed pipe (210), and the output end of the clockwise and anticlockwise motor (204) is fixedly connected with spiral shell
The right end of rasp bar (205), the threaded rod (205) runs through screwed pipe (210) and extends to the right side of movable plate (221), and spiral shell
Rasp bar (205) is threadedly coupled with screwed pipe (210), and the right side of the movable plate (221) is fixed to inlay that there are two symmetrical
Second slip ring (214), the inner sidewall of the cavity (218) are fixedly connected there are two symmetrical the second litter (222), two institutes
The left end for stating the second litter (222) extends through two the second slip rings (214) and extends to the left side of movable plate (221), and two
A second litter (222) socket-connects with two the second slip rings (214) respectively, the top of the movable plate (221) and bottom end it is outer
Surface passes through the second pin shaft (207) and is fixedly hinged with push-pull rod (208), and two push-pull rods (208) are located remotely from each other one end
Outer surface pass through the outer surface fixed hinges of the first pin shaft (203) Yu two gag lever post (220) one end close to each other respectively.
3. a kind of anticollision mechanism of fuel tanker as described in claim 1, it is characterised in that: the right side of the pedestal (103)
Face offers the first cavity (106), and the inner sidewall of first cavity (106) is fixedly connected with the first electromagnetism column (105), described
It being placed on the right side of pedestal (103) buffer stopper (101), the left side of the buffer stopper (101) offers the second cavity (108),
The inner sidewall of second cavity (108) is fixedly connected with the second electromagnetism column (109), and the right side of the pedestal (103) opens up
Have first sliding groove annular in shape (112), the left side of the buffer stopper (101) is fixedly connected with and first sliding groove (112) phase
The first sliding block (102) of adaptation, and the first sliding block (102) is connected to the inside of first sliding groove (112), the first sliding groove
(112) inner roof wall and inner bottom wall offers second sliding slot (113), and the upper surface and bottom surface of first sliding block (102) are solid
Surely be connected with second sliding slot (113) compatible second sliding block (114), and the second sliding block (114) is connected to second sliding slot
(113) left side of inside, first sliding block (102) is fixedly connected with buffer spring (111), the buffer spring
(111) left end is fixedly connected with the inner sidewall of first sliding groove (112).
4. a kind of anticollision mechanism of fuel tanker as described in claim 1, it is characterised in that: each second sliding block
(114) the fixation of right side is inlaid with the first slip ring (115), and the inner sidewall of each second sliding slot (113) is fixed to be connected
It is connected to the first litter (110), and the first litter (110) socket-connects with the first slip ring (115).
5. a kind of anticollision mechanism of fuel tanker as described in claim 1, it is characterised in that: the right side of the pedestal (103)
Face is fixed to be inlaid with two groups of symmetrical positioning pipes (104), the left side of the buffer stopper (101) be fixedly connected with two groups it is opposite
The positioning column (107) of title, the left end of positioning column described in every group (107) is located at the inside of two positioning pipes (104), and positions
Column (107) socket-connects with positioning pipe (104).
6. a kind of anticollision mechanism of fuel tanker as described in claim 1, it is characterised in that: the inside of the cavity (218)
Wall fixation is inlaid with bearing (212), and the outer surface of threaded rod (205) right end is fixedly connected with the inner ring of bearing (212).
7. a kind of anticollision mechanism of fuel tanker as described in claim 1, it is characterised in that: the right side of the fixed block (201)
Side offers card slot (211), and the left side of the pedestal (103) is fixedly connected with fixture block (213), and fixture block (213) is clamped
In the inside of card slot (211).
8. a kind of anticollision mechanism of fuel tanker as described in claim 1, it is characterised in that: each second litter
(222) left side is fixedly connected to baffle (206), and the vertical length value of the baffle (206) is greater than the second slip ring (214)
Vertical length value.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201810888736.5A CN109018386B (en) | 2018-08-07 | 2018-08-07 | A kind of anticollision mechanism of fuel tanker |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810888736.5A CN109018386B (en) | 2018-08-07 | 2018-08-07 | A kind of anticollision mechanism of fuel tanker |
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| CN109018386A true CN109018386A (en) | 2018-12-18 |
| CN109018386B CN109018386B (en) | 2019-08-16 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201810888736.5A Active CN109018386B (en) | 2018-08-07 | 2018-08-07 | A kind of anticollision mechanism of fuel tanker |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109626313A (en) * | 2019-01-14 | 2019-04-16 | 墨宝股份有限公司 | A kind of unmanned fuel charger with defencive function |
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| US6491255B1 (en) * | 2000-12-15 | 2002-12-10 | Jeff Bracken | Crashworthy external auxiliary fuel tank for aircraft |
| CN104276289A (en) * | 2014-09-25 | 2015-01-14 | 安徽科耀智能科技有限公司 | Fuel tank protecting device of unmanned aerial vehicle |
| CN107082121A (en) * | 2017-03-30 | 2017-08-22 | 中国航空工业集团公司西安飞机设计研究所 | A kind of anti-bird hits auxiliary fuel tank |
| CN207683327U (en) * | 2018-01-09 | 2018-08-03 | 无锡巨日电子科技有限公司 | A kind of fuel tank with the heat-insulated bulletproof function of anticollision |
-
2018
- 2018-08-07 CN CN201810888736.5A patent/CN109018386B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6491255B1 (en) * | 2000-12-15 | 2002-12-10 | Jeff Bracken | Crashworthy external auxiliary fuel tank for aircraft |
| CN104276289A (en) * | 2014-09-25 | 2015-01-14 | 安徽科耀智能科技有限公司 | Fuel tank protecting device of unmanned aerial vehicle |
| CN107082121A (en) * | 2017-03-30 | 2017-08-22 | 中国航空工业集团公司西安飞机设计研究所 | A kind of anti-bird hits auxiliary fuel tank |
| CN207683327U (en) * | 2018-01-09 | 2018-08-03 | 无锡巨日电子科技有限公司 | A kind of fuel tank with the heat-insulated bulletproof function of anticollision |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN109626313A (en) * | 2019-01-14 | 2019-04-16 | 墨宝股份有限公司 | A kind of unmanned fuel charger with defencive function |
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|---|---|
| CN109018386B (en) | 2019-08-16 |
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