CN110239717A - A kind of aircraft inside cabin formula article delivery device - Google Patents
A kind of aircraft inside cabin formula article delivery device Download PDFInfo
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- CN110239717A CN110239717A CN201910665505.2A CN201910665505A CN110239717A CN 110239717 A CN110239717 A CN 110239717A CN 201910665505 A CN201910665505 A CN 201910665505A CN 110239717 A CN110239717 A CN 110239717A
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- 230000007246 mechanism Effects 0.000 claims description 50
- 238000005192 partition Methods 0.000 claims description 21
- 230000011218 segmentation Effects 0.000 claims description 9
- 230000001133 acceleration Effects 0.000 claims description 7
- 230000009351 contact transmission Effects 0.000 claims description 2
- 230000005611 electricity Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 11
- 239000000463 material Substances 0.000 description 4
- 108010066057 cabin-1 Proteins 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000001727 in vivo Methods 0.000 description 1
- 230000001965 increasing effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000000837 restrainer Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
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Classifications
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- 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
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/12—Releasing
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Refuse-Collection Vehicles (AREA)
Abstract
The present invention discloses a kind of aircraft inside cabin formula article delivery device, delivery device is installed in aircraft cabin, the cabin includes cabin main body, hatchcover opening device is equipped in cabin main body, hatchcover opening device includes symmetrical bottom plate, filling in cabin equipped with array distribution is pressed from both sides, and filling folder includes filling clip shell body, is equipped with symmetrical throwing device in cabin main body.Delivery device of the present invention is by pulling safety rope, so that closing piece and the 5th through hole are detached from, first connecting rod is pushed to move down, first supporting block is in a vertical state, cancel the limit that outlet of jettisoninging is pressed from both sides to filling, the article that will jettisoning at this time presss from both sides outlet of jettisoninging from filling and is put into filling folder, realizes the carrying to more pieces of articles of jettisoninging；Article of jettisoninging is fallen into V-type funnel, and article of jettisoninging exports out by accelerating axis to carry out accelerating to dish out jettisoninging, and given one initial velocity of article of jettisoninging realizes that the continuous-stable of more pieces of articles of jettisoninging is jettisoninged, and it can be used repeatedly for filling folder, and reduction is jettisoninged cost.
Description
Technical field
The present invention relates to a kind of delivery device, specifically a kind of aircraft inside cabin formula article delivery device.
Background technique
Aircraft is the relative motion referred to fuselage and air, to obtain air force lift-off flight, and big
The aircraft of controllable flight is carried out in gas-bearing formation, the type of aircraft includes balloon, dirigible, manned aircraft and unmanned aerial vehicle etc..
As the continuous development of aeronautical technology develops, aircraft plays increasing effect in people's lives, extensively
It is general to be applied to that civilian, military, public administration is movable and the fields such as scientific research.On civilian, achievable shipping, passenger traffic, agricultural,
The task of fishery, forestry, meteorology, mine locating, aerial survety and aerophotography etc.；Militarily, it can be used for antisubmarine, transport
Soldiers, weapon and materiel；In public administration activity, it may also be used for police service, is rescued customs.Meanwhile aircraft is still
Carry out a kind of important tool of scientific research.Before the appearance of the spacecrafts such as artificial satellite and manned spaceship, related aerological,
Many research work of atmospheric physics, geophysics, geology, geography etc., all by means of aircraft.
Since the type of aircraft is more, selection is still scientific research, emergency help, air delivery with convenience flexibly
The important tool in the fields such as goods and materials.Such as launch sonde, emergency survival goods and materials.The throwing device of the prior art, there are following
Disadvantage, the carrying quantity for article of jettisoninging, multiple articles of jettisoninging are jettisoninged, the acquisition of initial velocity during article of jettisoninging is dished out, and are thrown
Throw the problems such as at high cost.
Summary of the invention
The purpose of the present invention is to provide a kind of aircraft inside cabin formula article delivery devices, by pulling safety rope, so that
Closing piece and the 5th through hole are detached from, and first connecting rod is pushed to move down, and the first supporting block is in a vertical state, are cancelled and being pressed from both sides to filling
It jettisonings the limit of outlet, the article that will jettisoning at this time is put into filling folder from the outlet of jettisoninging of filling folder, is realized to more pieces of articles of jettisoninging
Carrying；Article of jettisoninging is fallen into V-type funnel, jettisoning article jettisoning export out through acceleration axis carry out accelerate dish out, give
It jettisonings one initial velocity of article, realizes that the continuous-stable of more pieces of articles of jettisoninging is jettisoninged, it can be used repeatedly for filling folder, reduces and throws
Throw cost.
The purpose of the present invention can be achieved through the following technical solutions:
A kind of aircraft inside cabin formula article delivery device, delivery device are located in cabin, and the cabin includes cabin main body,
The top of cabin main body is equipped with filling and sandwiches mouth, and filling, which sandwiches in mouth, is equipped with disassembly shell, and the lower section of cabin main body is equipped with cabin
It jettisonings mouth.
It is equipped with symmetrical support frame in the cabin main body, is equipped with symmetrical support rod between support frame.
The support plate of array distribution is equipped in the cabin main body, support plate is equipped with the first through hole and second and runs through
The inside in hole, support plate is equipped with sliding slot.
Hatchcover opening device is equipped in the cabin main body, hatchcover opening device includes symmetrical first motor, the
One motor is fixed on the supporting plate, and first motor is equipped with symmetrical rotation axis, and rotation axis is equipped with symmetrical the
One belt pulley, two opposite support plates are equipped with the second belt pulley, pass through belt between the second belt pulley and the first belt pulley
Rotation connection.
The hatchcover opening device includes symmetrical bottom plate, and bottom plate is located at cabin and jettisonings in mouth, and bottom plate includes bottom plate
Main body, floor body are equipped with the first symmetrical link block, and the side of the first link block is equipped with first sliding axle, and first connects
Block is connect equipped with the second symmetrical link block, the second link block is equipped with third through hole, and rotation is set in third through hole
There is engagement shaft.
Filling in the cabin equipped with array distribution is pressed from both sides, and filling folder includes filling clip shell body, and filling folder is equipped with handle,
The lower section of filling folder is equipped with filling and presss from both sides outlet of jettisoninging, and the two sides of filling clip shell body are equipped with side plate, and the both ends of side plate are equipped with arc
Shape face.
The side plate is equipped with the limited block of array distribution, and limited block is equipped with limit slide opening, limits slide opening, limits slide opening
Interior sliding is equipped with first connecting rod, and the first end of first connecting rod is equipped with the 4th through hole and the 5th through hole, other end rotation connection
There is second connecting rod.
The opposite side of the side plate is equipped with connecting column, and connecting column one end is equipped with sliding eye, and the other end is equipped with putting hole, places
Hole is connected to sliding eye.
Say that spring catch, spring catch include second sliding axle on the side plate, one end of second sliding axle is equipped with closing piece, another
End is equipped with limit closing piece, and the one end and second sliding axle for limiting closing piece are fastenedly connected, and the other end is equipped with the first connecting shaft, and first connects
Spindle is equipped with the 6th through hole, is connected with connection ring in the 6th through hole, and two connection rings first pair pass through safety rope connection.
Elastic component is equipped in the putting hole.
The side of the filling clip shell body is equipped with rotation connection slot, and link block is equipped in rotation connection slot, is set on link block
There is connector sleeve, the side that filling clip shell body is equipped with rotation connection slot is equipped with connection support ring, and connection support ring is equipped with first
Rotation is equipped with connecting shaft in connecting hole, the first connecting hole and connector sleeve, and rotation is equipped with the first supporting block, the first support in connecting shaft
Block includes the first support block main body, and the first support block main body is equipped with the 7th through hole and the 8th through hole.
Symmetrical throwing device is equipped in the cabin main body, throwing device includes cabinet of jettisoninging, cabinet packet of jettisoninging
The shell jettisoninged is included, the lower section of shell is equipped with V-type funnel, is equipped with outlet of jettisoninging below V-type funnel, the lower section of V-type funnel is equipped with
Symmetrical support connecting plate supports and is rotatably connected to symmetrical acceleration axis on connecting plate, one end of axis is accelerated to be equipped with
Second motor, the second motor are fixed on support connecting plate.
One end of the cabinet of jettisoninging is equipped with the first support connecting plate, and the other end is equipped with the second support connecting plate, case of jettisoninging
It is equipped with the partition of array distribution in vivo, partition will jettisoning the long different region of cabinet segmentation, and partition one end is connected with the first support
Plate is fastenedly connected, and the other end is fastenedly connected with the second support connecting plate, both ends in each region, the first support connecting plate and the
The arc-shaped slot with arcwall face cooperation is equipped on two support connecting plates.
The first support connecting plate and the second support connecting plate are equipped with the arc shifting chute of array distribution, and partition is equipped with
Symmetrical square groove.
Second support connecting plate two sides, are successively arranged the first steering engine, the second steering engine, third steering engine and the 4th rudder up and down
Machine, the second steering engine are equipped with the first position-limit mechanism, and the first position-limit mechanism includes third connecting rod, one end of third connecting rod and the second rudder
The output shaft of machine is fastenedly connected, and the other end is rotatably connected to fourth link, and it is first right that fourth link is rotatablely connected with third connecting rod
End is rotatably connected to the 5th connecting rod, and control shaft is fastenedly connected on the 5th connecting rod, and control shaft is equipped with symmetrical second
Bracer, control shaft and the second support connecting plate, the first support connecting plate rotation connection.
4th steering engine is equipped with the second position-limit mechanism.
Third position-limit mechanism and the 4th position-limit mechanism are respectively equipped on first steering engine, third steering engine.
Further, the disassembly shell is fixed on filling by screw rod and sandwiches in mouth.
Further, the rotation axis is located at rotation in the second through hole by bearing；Second belt pulley passes through solid
Dead axle is located at rotation in the first through hole；The bottom plate is located at slide-and-guide in sliding slot by first sliding axle.
Further, the bottom plate is driven by engagement shaft and belt contacts, and first motor control bottom plate is located at cabin throwing
Throw the opening and closing in mouth.
Further, the elastic component is sleeved in second sliding axle, and one end of elastic component acts on the inner wall of putting hole,
The other end acts on closing piece；First supporting block is rotatablely connected by the 7th through hole and connecting shaft, is run through by the 8th
Hole and pin shaft cooperation are rotatablely connected with second connecting rod.
Further, one end of the second connecting rod and first connecting rod are rotatablely connected, and the other end and the first supporting block rotate
Connection controls the rotation of the first supporting block by moving up and down for first connecting rod, and article of jettisoninging intracorporal to filling clip shell carries out
Limit.
Further, described two second motors rotation direction on the contrary, symmetrical acceleration axis to jettisoning article into
Row accelerates to dish out；The filling folder of the array distribution is fastened in arc-shaped slot by arcwall face, by the support rod for claiming distribution
Filling folder is fixed.
Further, the symmetrical throwing device is contacted with each other by the first support connecting plate, the first position restrainer
Structure is identical as the second position-limit mechanism mechanism, and the second supporting block that the first position-limit mechanism and the second position-limit mechanism are controlled is located at partition
It will be in the same area for cabinet segmentation of jettisoninging.
Further, the third position-limit mechanism and the 4th position-limit mechanism are identical as the first position-limit mechanism structure, difference
It is, the length of fourth link is different, so that the second supporting block that the first position-limit mechanism is controlled with third position-limit mechanism is located at
Partition will jettisoning in the different zones that cabinet is divided, the second supporting block position that third position-limit mechanism and the 4th position-limit mechanism are controlled
It will be in the same area that jettisoning cabinet segmentation in partition.
Further, the second support connecting plate is equipped with symmetrical support connector sleeve, supports connector sleeve and spiral shell
Bar cooperation is fixed on the support frame by throwing device.
Beneficial effects of the present invention:
1, delivery device of the present invention, so that closing piece and the 5th through hole are detached from, pushes first connecting rod by pulling safety rope
It moves down, the first supporting block is in a vertical state, cancels and jettisoninging the limit of outlet to filling folder, and the article that will jettisoning at this time is from filling out
It fills folder outlet of jettisoninging to be put into filling folder, realizes carrying to more pieces of articles of jettisoninging；
2, delivery device of the present invention article of jettisoninging is fallen into V-type funnel, and article of jettisoninging exports out by accelerating axis jettisoninging
It carries out accelerating to dish out, given one initial velocity of article of jettisoninging realizes that the continuous-stable of more pieces of articles of jettisoninging is jettisoninged, and filling folder can
With Reusability, cost of jettisoninging is reduced.
Detailed description of the invention
The present invention will be further described below with reference to the drawings.
Fig. 1 is delivery device structural schematic diagram of the present invention；
Fig. 2 is delivery device structural schematic diagram of the present invention；
Fig. 3 is delivery device structural schematic diagram of the present invention；
Fig. 4 is structural diagram of base plate of the present invention；
Fig. 5 is present invention filling clamping structure schematic diagram；
Fig. 6 is present invention filling folder partial structure diagram；
Fig. 7 is present invention filling folder partial structure diagram；
Fig. 8 is present invention filling folder part-structure sectional view；
Fig. 9 is present invention filling folder partial structure diagram；
Figure 10 is throwing device structural schematic diagram of the present invention；
Figure 11 is throwing device partial structure diagram of the present invention；
Figure 12 is throwing device partial structure diagram of the present invention.
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 all other
Embodiment shall fall within the protection scope of the present invention.
A kind of aircraft inside cabin formula article delivery device, delivery device are located in cabin 1, as shown in Figure 1 and Figure 2, cabin 1
Including cabin main body 11, the top of cabin main body 11 is equipped with filling and sandwiches mouth 12, and filling, which sandwiches in mouth 12, is equipped with disassembly shell 2,
Disassembly shell 2 is fixed on filling by screw rod and sandwiches in mouth 12, and the lower section of cabin main body 11 is jettisoninged mouth 15 equipped with cabin.
It is equipped with symmetrical support frame 13 in cabin main body 11, is equipped with symmetrical support rod between support frame 13
131。
The support plate 14 of array distribution is equipped in cabin main body 11, support plate 14 is equipped with the first through hole 141 and second
The inside of through hole 142, support plate 14 is equipped with sliding slot 143, as shown in Figure 3.
Hatchcover opening device 3 is equipped in cabin main body 11, as shown in figure 3, hatchcover opening device 3 includes symmetrical the
One motor 31, first motor 31 are fixed in support plate 14, and first motor 31 is equipped with symmetrical rotation axis 32, rotation axis
32 are located at rotation in the second through hole 142 by bearing, and rotation axis 32 is equipped with the first symmetrical belt pulley 33, opposite
Two support plates 14 are equipped with the second belt pulley 34, and the second belt pulley 34 is located at rotation in the first through hole 141 by fixing axle,
It is rotatablely connected between second belt pulley 34 and the first belt pulley 33 by belt 35, belt 35 has toughness.
Hatchcover opening device 3 includes symmetrical bottom plate 36, is jettisoninged in mouth 15 as shown in figure 4, bottom plate 36 is located at cabin,
Bottom plate 36 includes floor body 361, and floor body 361 is equipped with the first symmetrical link block 362, the first link block 362
Side be equipped with first sliding axle 363, bottom plate 36 is located at slide-and-guide in sliding slot 143 by first sliding axle 363, and first connects
Block 362 is equipped with the second symmetrical link block 364, and the second link block 364 is equipped with third through hole 365, and third runs through
Rotation is equipped with engagement shaft 366 in hole 365, and bottom plate 36 controls bottom by engagement shaft 366 and 35 Contact Transmission of belt, first motor 31
Plate 36 is located at the opening and closing that cabin is jettisoninged in mouth 15.
Filling folder 4 in cabin 1 equipped with array distribution, as shown in Fig. 1, Fig. 5, Fig. 6, Fig. 7, filling folder 4 includes filling folder
Shell 41, filling folder 4 is equipped with handle 42, and the lower section of filling folder 4 is equipped with filling and presss from both sides outlet 401 of jettisoninging, filling clip shell body 41
Two sides are equipped with side plate 411, and the both ends of side plate 411 are equipped with arcwall face 4111.
Side plate 411 is equipped with the limited block 413 of array distribution, and limited block 413 is equipped with limit slide opening 414, limits slide opening
414, the interior sliding of limit slide opening 414 is equipped with first connecting rod 43, and the first end of first connecting rod 43 is equipped with the 4th through hole 431 and the 5th
Through hole 432, the other end are rotatably connected to second connecting rod 44.
The opposite side of side plate 411 is equipped with connecting column 412, as shown in figure 8,412 one end of connecting column is equipped with sliding eye 4121, separately
One end is equipped with putting hole 4122, and putting hole 4122 is connected to sliding eye 4121.
Say that spring catch 45, spring catch 45 include second sliding axle 451 on side plate 411, one end of second sliding axle 451 is equipped with
Closing piece 452, the other end are equipped with limit closing piece 453, and one end of limit closing piece 453 is fastenedly connected with second sliding axle 451, the other end
Equipped with the first connecting shaft 454, the first connecting shaft 454 is equipped with the 6th through hole 455, is connected with connection in the 6th through hole 455
Ring 47, two connection rings 47 first pair are connected by safety rope 48.
Elastic component 46 is equipped in putting hole 4122, elastic component 46 is sleeved in second sliding axle 451, one end of elastic component 46
The inner wall of putting hole 4122 is acted on, the other end acts on closing piece 452.
The side for filling clip shell body 41 is equipped with rotation connection slot 415, and link block 416, connection are equipped in rotation connection slot 415
Block 416 is equipped with connector sleeve 417, and the side that filling clip shell body 41 is equipped with rotation connection slot 415 is equipped with connection support ring 418,
It connects support ring 418 and is equipped with the first connecting hole 4181, rotation is equipped with connecting shaft in the first connecting hole 4181 and connector sleeve 417
419, rotation is equipped with the first supporting block 49 in connecting shaft 419, and the first supporting block 49 includes the first support block main body 491, such as Fig. 9 institute
Show, the first support block main body 491 is equipped with the 7th through hole 493 and the 8th through hole 492, and the first supporting block 49 is passed through by the 7th
Perforation 493 is rotatablely connected with connecting shaft 419, is rotatablely connected by the 8th through hole 492 and pin shaft cooperation with second connecting rod 44.
One end of second connecting rod 44 and first connecting rod 43 are rotatablely connected, and the other end and the first supporting block 49 are rotatablely connected, and are led to
Moving up and down for first connecting rod 43 is crossed, the rotation of the first supporting block 49 is controlled, the article of jettisoninging in filling clip shell body 41 is carried out
Limit.
Symmetrical throwing device 5 is equipped in cabin main body 11, as shown in Figure 10, throwing device 5 includes cabinet of jettisoninging
51, cabinet 51 of jettisoninging includes the shell 511 jettisoninged, and the lower section of shell 511 is equipped with V-type funnel 512, is equipped with below V-type funnel 512
It jettisonings outlet 514, the lower section of V-type funnel 512 is equipped with symmetrical support connecting plate 513, supports the company of rotation on connecting plate 513
It is connected to symmetrical acceleration axis 515, accelerates one end of axis 515 to be equipped with the second motor 516, the second motor 516 is fixed on support
On connecting plate 513, the rotation direction of two the second motors 516 is on the contrary, symmetrical acceleration axis 515 adds article of jettisoninging
Speed is dished out.
Jettisoning cabinet 51 one end be equipped with first support connecting plate 59, the other end be equipped with second support connecting plate 52, jettisoning
Be equipped with the partition 50 of array distribution in cabinet 51, partition 50 will jettisoning the long different region of the segmentation of cabinet 51,50 one end of partition with
First support connecting plate 59 is fastenedly connected, and the other end supports connecting plate 52 to be fastenedly connected with second, both ends in each region, the
The arc-shaped slot 521 cooperated with arcwall face 4111, array point are equipped on one support connecting plate 59 and the second support connecting plate 52
The filling folder 4 of cloth is fastened in arc-shaped slot 521 by arcwall face 4111, by claim 131 pairs of fillings of support rod of distribution press from both sides 4 into
Row limit is fixed.
Symmetrical throwing device 5 is contacted with each other by the first support connecting plate 59.
First support connecting plate 59 and the second support connecting plate 52 are equipped with the arc shifting chute 522 of array distribution, partition
50 are equipped with symmetrical square groove 501.
Second support 52 two sides of connecting plate, are successively arranged the first steering engine 523, the second steering engine 524, third steering engine 525 up and down
With the 4th steering engine 526, as shown in Figure 11, Figure 12, the second steering engine 524 is equipped with the first position-limit mechanism, and the first position-limit mechanism includes
Third connecting rod 53, one end of third connecting rod 53 and the output shaft of the second steering engine 524 are fastenedly connected, and the other end is rotatably connected to the 4th
The first opposite end that connecting rod 54, fourth link 54 and third connecting rod 53 are rotatablely connected is rotatably connected to the 5th connecting rod 55, the 5th connecting rod 55
On be fastenedly connected with control shaft 56, control shaft 56 is equipped with the second symmetrical supporting block 57, and control shaft 56 is supported with second
Connecting plate 52, first supports connecting plate 59 to be rotatablely connected.
4th steering engine 526 is equipped with the second position-limit mechanism, and the first position-limit mechanism is identical as the second position-limit mechanism mechanism, and the
One position-limit mechanism and the second supporting block 57 that the second position-limit mechanism is controlled be located at partition 50 will jettisoning cabinet 51 divide it is same
In region.
Third position-limit mechanism and the 4th position-limit mechanism, third limit are respectively equipped on first steering engine 523, third steering engine 525
Mechanism and the 4th position-limit mechanism are identical as the first position-limit mechanism structure, and difference is, the length of fourth link 54 is different, so that
The second supporting block 57 that first position-limit mechanism and third position-limit mechanism are controlled is located at the cabinet 51 that will jettisoning of partition 50 and divides not
With in region, the second supporting block 57 that third position-limit mechanism and the 4th position-limit mechanism are controlled, which is located at partition 50, will jettisoning cabinet 51
In the same area of segmentation.
Second support connecting plate 52 is equipped with symmetrical support connector sleeve 58, and support connector sleeve 58 and screw rod cooperation will
Throwing device 5 is fixed on support frame 13.
In use, so that closing piece 452 and the 5th through hole 432 are detached from, pushing first connecting rod 43 by pulling safety rope 48
It moves down, the first supporting block 49 is in a vertical state, cancels the limit that outlet 401 of jettisoninging is pressed from both sides to filling, will jettisoning object at this time
Product from filling folder jettisoning outlet 401 be put into filling folder 4 in, will filling folder 4 fill up after, pull first connecting rod 43 move up, bullet
Spring pin 45 is fastened in the 5th through hole 432 under the action of elastic component 46, and the first supporting block 49 is in horizontality pair at this time
Article of jettisoninging in filling folder 4 is limited, and filling folder 4 is sandwiched mouth 12 by filling and is placed on throwing device by drawing to handle 42
On 5, the filling folder 4 of array distribution is fastened in arc-shaped slot 521 by arcwall face 4111, pulls safety rope 48, the first support
Block 49 is under the action of jettisoninging article gravity, so that first connecting rod 43 moves down, unclamps safety rope 48, is blocked by spring catch 45
Conjunction is fixed the first supporting block 49 in the 4th through hole 431, and article of jettisoninging at this time passes through close to 4 sides of filling folder
Second supporting block 57 is supported, installing and dismounting shell 2.
Aircraft is when flying to designated position, through 4 lower section of filling folder in the second supporting block 57 of 4 sides of filling folder
Steering engine rotation so that article of jettisoninging is fallen in next second supporting block 57, now close to the second support of 4 sides of filling folder
Steering engine on block 57 is gone back to, and so that the second supporting block 57 is fallen in horizontality and limit to remaining article of jettisoninging, at this time
Steering engine rotation in the second supporting block 57 far from 4 sides of filling folder, so that article of jettisoninging is fallen into V-type funnel 512, while the
One motor 31 controls bottom plate 36 and opens, and article of jettisoninging goes out in outlet 514 of jettisoninging by accelerating axis 515 to carry out accelerating to dish out.
In the description of this specification, the description of reference term " one embodiment ", " example ", " specific example " etc. means
Particular features, structures, materials, or characteristics described in conjunction with this embodiment or example are contained at least one implementation of the invention
In example or example.In the present specification, schematic expression of the above terms may not refer to the same embodiment or example.
Moreover, particular features, structures, materials, or characteristics described can be in any one or more of the embodiments or examples to close
Suitable mode combines.
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, without departing from the spirit and scope of the present invention, various changes and improvements may be made to the invention, these changes
Change and improvement all fall within the protetion scope of the claimed invention.
Claims (10)
1. a kind of aircraft inside cabin formula article delivery device, delivery device is installed in aircraft cabin (1), which is characterized in that
The cabin (1) includes cabin main body (11), and the top of cabin main body (11) is equipped with filling and sandwiches mouth (12), and filling sandwiches mouth
(12) disassembly shell (2) is equipped in, the lower section of cabin main body (11) is equipped with cabin and jettisonings mouth (15)；
It is equipped with symmetrical support frame (13) in the cabin main body (11), is equipped with symmetrical branch between support frame (13)
Strut (131)；
The support plate (14) of array distribution is equipped in the cabin main body (11), support plate (14) is equipped with the first through hole
(141) and the second through hole (142), the inside of support plate (14) are equipped with sliding slot (143)；
Hatchcover opening device (3) are equipped in the cabin main body (11), hatchcover opening device (3) includes the first symmetrical electricity
Machine (31), first motor (31) are fixed on support plate (14), and first motor (31) is equipped with symmetrical rotation axis (32),
Rotation axis (32) is equipped with symmetrical the first belt pulley (33), and two opposite support plates (14) are equipped with the second belt pulley
(34), it is rotatablely connected between the second belt pulley (34) and the first belt pulley (33) by belt (35)；
The hatchcover opening device (3) includes symmetrical bottom plate (36), and bottom plate (36) is located at cabin and jettisonings in mouth (15), bottom
Plate (36) includes floor body (361), and floor body (361) is equipped with symmetrical the first link block (362), the first connection
The side of block (362) is equipped with first sliding axle (363), and the first link block (362) is equipped with the second symmetrical link block
(364), the second link block (364) is equipped with third through hole (365), and rotation is equipped with engagement shaft in third through hole (365)
(366)；
(4) are pressed from both sides in filling in the cabin (1) equipped with array distribution, and filling folder (4) includes filling clip shell body (41), filling folder
(4) handle (42) are equipped with, the lower section of filling folder (4) is equipped with filling folder and jettisonings outlet (401), fills the two sides of clip shell body (41)
It is equipped with side plate (411), the both ends of side plate (411) are equipped with arcwall face (4111)；
The side plate (411) is equipped with the limited block (413) of array distribution, and limited block (413) is equipped with limit slide opening (414),
It limits slide opening (414), sliding is equipped with first connecting rod (43) in limit slide opening (414), and the first end of first connecting rod (43) is equipped with the
Four through holes (431) and the 5th through hole (432), the other end are rotatably connected to second connecting rod (44)；
The opposite side of the side plate (411) is equipped with connecting column (412), and connecting column (412) one end is equipped with sliding eye (4121), another
End is equipped with putting hole (4122), and putting hole (4122) is connected to sliding eye (4121)；
It is said spring catch (45) on the side plate (411), spring catch (45) includes second sliding axle (451), second sliding axle (451)
One end be equipped with closing piece (452), the other end be equipped with limit closing piece (453), limit closing piece (453) one end and second sliding axle
(451) it being fastenedly connected, the other end is equipped with the first connecting shaft (454), and the first connecting shaft (454) is equipped with the 6th through hole (455),
Connection ring (47) are connected in 6th through hole (455), two connection rings (47) first pair pass through safety rope (48) connection；
Elastic component (46) are equipped in the putting hole (4122)；
The side of filling clip shell body (41) is equipped with rotation connection slot (415), is equipped with link block in rotation connection slot (415)
(416), link block (416) is equipped with connector sleeve (417), and filling clip shell body (41) is equipped with the side of rotation connection slot (415)
Equipped with connection support ring (418), connection support ring (418) be equipped with the first connecting hole (4181), the first connecting hole (4181) and
Rotation is equipped with connecting shaft (419) in connector sleeve (417), and rotation is equipped with the first supporting block (49) in connecting shaft (419), the first support
Block (49) includes the first support block main body (491), and the first support block main body (491) is equipped with the 7th through hole (493) and the 8th
Through hole (492)；
Symmetrical throwing device (5) is equipped in the cabin main body (11), throwing device (5) includes jettisoninging cabinet (51),
Cabinet (51) of jettisoninging includes the shell (511) jettisoninged, and the lower section of shell (511) is equipped with V-type funnel (512), V-type funnel (512)
Lower section is equipped with and jettisonings outlet (514), and the lower section of V-type funnel (512) is equipped with symmetrical support connecting plate (513), and support connects
It is rotatably connected to symmetrical acceleration axis (515) on fishplate bar (513), the one end of axis (515) is accelerated to be equipped with the second motor
(516), the second motor (516) is fixed in support connecting plate (513)；
One end of the cabinet of jettisoninging (51) is equipped with the first support connecting plate (59), and the other end is equipped with the second support connecting plate
(52), it jettisonings and is equipped with the partition (50) of array distribution in cabinet (51), partition (50) cabinet (51) segmentation length that will jettisoning is different
Region, partition (50) one end are fastenedly connected with the first support connecting plate (59), the other end and the second support connecting plate (52) fastening
Connection, both ends, the first support connecting plate (59) and second in each region support to be equipped with and arcwall face on connecting plate (52)
(4111) arc-shaped slot (521) cooperated；
First support connecting plate (59) and the second support connecting plate (52) are equipped with the arc shifting chute of array distribution
(522), partition (50) is equipped with symmetrical square groove (501)；
Second support connecting plate (52) two sides, are successively arranged the first steering engine (523), the second steering engine (524), third rudder up and down
Machine (525) and the 4th steering engine (526), the second steering engine (524) are equipped with the first position-limit mechanism, and the first position-limit mechanism includes that third connects
Bar (53), one end of third connecting rod (53) and the output shaft of the second steering engine (524) are fastenedly connected, and the other end is rotatably connected to the 4th
The first opposite end of connecting rod (54), fourth link (54) and third connecting rod (53) rotation connection is rotatably connected to the 5th connecting rod (55), the
It is fastenedly connected on five connecting rods (55) control shaft (56), control shaft (56) is equipped with symmetrical the second supporting block (57), control
Axis (56) processed and the second support connecting plate (52), the first support connecting plate (59) rotation connection；
4th steering engine (526) is equipped with the second position-limit mechanism；
First steering engine (523), third steering engine are respectively equipped with third position-limit mechanism and the 4th position-limit mechanism on (525).
2. a kind of aircraft inside cabin formula article delivery device according to claim 1, which is characterized in that the disassembly shell
(2) filling is fixed on by screw rod to sandwich in mouth (12).
3. a kind of aircraft inside cabin formula article delivery device according to claim 1, which is characterized in that the rotation axis
(32) rotation in the second through hole (142) is located at by bearing；Second belt pulley (34) is located at first by fixing axle and passes through
Perforating, (141) are interior to be rotated；The bottom plate (36) is located at sliding slot (143) interior slide-and-guide by first sliding axle (363).
4. a kind of aircraft inside cabin formula article delivery device according to claim 1, which is characterized in that the bottom plate (36)
By engagement shaft (366) and belt (35) Contact Transmission, first motor (31) control bottom plate (36) is located at cabin and jettisonings mouth (15)
Interior opening and closing.
5. a kind of aircraft inside cabin formula article delivery device according to claim 1, which is characterized in that the elastic component
(46) it is sleeved on second sliding axle (451), one end of elastic component (46) acts on the inner wall of putting hole (4122), and the other end is made
On closing piece (452)；First supporting block (49) is rotatablely connected by the 7th through hole (493) and connecting shaft (419), is led to
It crosses the 8th through hole (492) and pin shaft cooperation is rotatablely connected with second connecting rod (44).
6. a kind of aircraft inside cabin formula article delivery device according to claim 1, which is characterized in that the second connecting rod
(44) one end and first connecting rod (43) is rotatablely connected, and the other end and the first supporting block (49) are rotatablely connected, and passes through first connecting rod
(43) move up and down, controls the rotation of the first supporting block (49), limits to the article of jettisoninging in filling clip shell body (41).
7. a kind of aircraft inside cabin formula article delivery device according to claim 1, which is characterized in that described two second
The rotation direction of motor (516) is on the contrary, symmetrical acceleration axis (515) carries out accelerating to dish out to article of jettisoninging；The array
The filling folder (4) of distribution is fastened in arc-shaped slot (521) by arcwall face (4111), by the support rod (131) for claiming distribution
Filling folder (4) is fixed.
8. a kind of aircraft inside cabin formula article delivery device according to claim 1, which is characterized in that described symmetrical
Throwing device (5) by first support connecting plate (59) contact with each other, the first position-limit mechanism and the second position-limit mechanism mechanism phase
Together, the second supporting block (57) that the first position-limit mechanism and the second position-limit mechanism are controlled, which is located at partition (50), will jettisoning cabinet (51)
In the same area of segmentation.
9. a kind of aircraft inside cabin formula article delivery device according to claim 1, which is characterized in that the third limit
Mechanism and the 4th position-limit mechanism are identical as the first position-limit mechanism structure, and difference is, the length of fourth link (54) is different, make
The second supporting block (57) for being controlled of the first position-limit mechanism and third position-limit mechanism is located at partition (50) and will jettisoning cabinet (51)
In the different zones of segmentation, the second supporting block (57) that third position-limit mechanism and the 4th position-limit mechanism are controlled is located at partition (50)
It will jettisoning in the same area of cabinet (51) segmentation.
10. a kind of aircraft inside cabin formula article delivery device according to claim 1, which is characterized in that described second
It supports connecting plate (52) and is equipped with symmetrical support connector sleeve (58), support connector sleeve (58) and screw rod cooperate throwing device
(5) it is fixed on support frame (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910665505.2A CN110239717B (en) | 2019-07-23 | 2019-07-23 | Cabin type article throwing device in aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910665505.2A CN110239717B (en) | 2019-07-23 | 2019-07-23 | Cabin type article throwing device in aircraft |
Publications (2)
| Publication Number | Publication Date |
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| CN110239717A true CN110239717A (en) | 2019-09-17 |
| CN110239717B CN110239717B (en) | 2024-05-07 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910665505.2A Active CN110239717B (en) | 2019-07-23 | 2019-07-23 | Cabin type article throwing device in aircraft |
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| Country | Link |
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| CN (1) | CN110239717B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111025984A (en) * | 2019-12-23 | 2020-04-17 | 中国科学院光电研究院 | Near space ball carries control device that jettisonings |
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| CN210175126U (en) * | 2019-07-23 | 2020-03-24 | 安徽天路航空科技股份有限公司 | Device is put in to cabin formula article in aircraft |
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| US20130240674A1 (en) * | 2010-10-07 | 2013-09-19 | Etat Francais Represente Par Le Delegue General Pour L'armement | Securing/releasing device, and related airdrop device |
| US9676481B1 (en) * | 2015-03-27 | 2017-06-13 | Amazon Technologies, Inc. | Tether compensated airborne delivery |
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| CN106335640A (en) * | 2016-09-28 | 2017-01-18 | 中科新松有限公司 | Unmanned aerial vehicle based continuous dropping device and controller |
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| CN111025984A (en) * | 2019-12-23 | 2020-04-17 | 中国科学院光电研究院 | Near space ball carries control device that jettisonings |
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| Publication number | Publication date |
|---|---|
| CN110239717B (en) | 2024-05-07 |
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