CN110239717B - Cabin type article throwing device in aircraft - Google Patents
Cabin type article throwing device in aircraft Download PDFInfo
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- CN110239717B CN110239717B CN201910665505.2A CN201910665505A CN110239717B CN 110239717 B CN110239717 B CN 110239717B CN 201910665505 A CN201910665505 A CN 201910665505A CN 110239717 B CN110239717 B CN 110239717B
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- 230000007246 mechanism Effects 0.000 claims description 46
- 238000005192 partition Methods 0.000 claims description 21
- 230000009351 contact transmission Effects 0.000 claims description 3
- 230000001133 acceleration Effects 0.000 claims description 2
- 238000011160 research Methods 0.000 description 4
- 108010066057 cabin-1 Proteins 0.000 description 3
- 238000012856 packing Methods 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000007726 management method Methods 0.000 description 2
- 238000005303 weighing Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process 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
- 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)
- Refuse-Collection Vehicles (AREA)
- Toys (AREA)
Abstract
The invention discloses a cabin-type article throwing device in an aircraft, which is arranged in an aircraft cabin, wherein the cabin comprises a cabin main body, a cabin cover opening device is arranged in the cabin main body, the cabin cover opening device comprises a symmetrically distributed bottom plate, filling clamps distributed in an array are arranged in the cabin, each filling clamp comprises a filling clamp shell, and a symmetrically distributed throwing device is arranged in the cabin main body. According to the throwing device, the safety rope is pulled, so that the locking block is separated from the fifth through hole, the first connecting rod is pushed to move downwards, the first supporting block is in a vertical state, the limit of the throwing outlet of the filling clamp is canceled, at the moment, the throwing objects are placed into the filling clamp from the throwing outlet of the filling clamp, and the bearing of a plurality of throwing objects is realized; the throwing articles fall into the V-shaped funnel, the throwing articles are accelerated to be thrown out through the accelerating shaft at the throwing outlet, an initial speed of the throwing articles is set, continuous and stable throwing of a plurality of throwing articles is achieved, the filling clamp can be used repeatedly, and throwing cost is reduced.
Description
Technical Field
The invention relates to a throwing device, in particular to an aircraft interior cabin type article throwing device.
Background
The aircraft refers to an aircraft capable of achieving aerodynamic lift-off flight by means of relative movement of a fuselage and air and performing controllable flight in the atmosphere, and types of aircraft include balloons, airships, unmanned planes, and the like.
With the continuous development of aviation technology, aircrafts play an increasing role in people's life, and have been widely applied to the fields of civil use, military use, public management activities, scientific research and the like. The civil engineering can finish the tasks of freight transportation, passenger transportation, agriculture, fishery, forestry, meteorological, prospecting, aerial measurement, aerial photography and the like; in military, it can be used for counterdiving, transporting arms, weapons and combat supplies; in public management activities, it can also be used for police, customs, rescue, etc. At the same time, aircraft is also an important tool for scientific research. Many research efforts in high altitude weather, atmospheric physics, geophysics, geology, geography, etc., have been conducted with the aid of aircraft prior to the advent of satellites and manned spacecraft.
Because of more types of aircrafts, the selection is flexible, the application is convenient, and the aircraft is still an important tool in the fields of scientific research, emergency rescue, aerial delivery of goods and materials and the like. Such as launching sonde, emergency lifesaving supplies, etc. The throwing device in the prior art has the following defects that the carrying quantity of the throwing objects, the throwing of a plurality of throwing objects, the acquisition of initial speed in the throwing process of the throwing objects, high throwing cost and the like.
Disclosure of Invention
The invention aims to provide an aircraft inner cabin type article throwing device, which is characterized in that a lock block is separated from a fifth through hole by pulling a safety rope, a first connecting rod is pushed to move downwards, a first supporting block is in a vertical state, the limit of a filling clamp throwing outlet is canceled, at the moment, a throwing article is placed into a filling clamp from the filling clamp throwing outlet, and the bearing of a plurality of throwing articles is realized; the throwing articles fall into the V-shaped funnel, the throwing articles are accelerated to be thrown out through the accelerating shaft at the throwing outlet, an initial speed of the throwing articles is set, continuous and stable throwing of a plurality of throwing articles is achieved, the filling clamp can be used repeatedly, and throwing cost is reduced.
The aim of the invention can be achieved by the following technical scheme:
The utility model provides a cabin formula article throwing device in aircraft, puts in the device and is located the cabin, the cabin includes the cabin main part, and the top of cabin main part is equipped with fills the clamp entry, fills to be equipped with in the clamp entry and dismantle the shell, and the below of cabin main part is equipped with the cabin and throws the mouth.
The cabin body is internally provided with symmetrically distributed supporting frames, and symmetrically distributed supporting rods are arranged between the supporting frames.
The cabin body is internally provided with a supporting plate in array distribution, the supporting plate is provided with a first through hole and a second through hole, and the inner side of the supporting plate is provided with a sliding groove.
The cabin cover opening device is arranged in the cabin body and comprises first motors which are symmetrically distributed, the first motors are fixed on the supporting plates, symmetrically distributed rotating shafts are arranged on the first motors, symmetrically distributed first belt pulleys are arranged on the rotating shafts, second belt pulleys are arranged on the two opposite supporting plates, and the second belt pulleys are connected with the first belt pulleys in a rotating mode through belts.
The cabin cover opening device comprises a symmetrically distributed bottom plate, the bottom plate is located in a cabin throwing port and comprises a bottom plate main body, a symmetrically distributed first connecting block is arranged on the bottom plate main body, a first sliding shaft is arranged on one side of the first connecting block, a symmetrically distributed second connecting block is arranged on the first connecting block, a third through hole is formed in the second connecting block, and a contact shaft is arranged in the third through hole in a rotating mode.
The cabin is internally provided with filling clamps distributed in an array manner, each filling clamp comprises a filling clamp shell, a handle is arranged on each filling clamp, a filling clamp throwing outlet is formed in the lower portion of each filling clamp, two sides of each filling clamp shell are respectively provided with a side plate, and two ends of each side plate are respectively provided with an arc-shaped surface.
Limiting blocks distributed in an array mode are arranged on the side plates, limiting sliding holes are formed in the limiting blocks, first connecting rods are slidably arranged in the limiting sliding holes, fourth through holes and fifth through holes are formed in the first ends of the first connecting rods, and second connecting rods are connected to the other ends of the first connecting rods in a rotating mode.
The opposite side of curb plate is equipped with the spliced pole, and spliced pole one end is equipped with the sliding hole, and the other end is equipped with places the hole, places hole and sliding hole intercommunication.
The side plate is provided with a spring pin, the spring pin comprises a second sliding shaft, one end of the second sliding shaft is provided with a locking block, the other end of the second sliding shaft is provided with a limiting locking block, one end of the limiting locking block is fixedly connected with the second sliding shaft, the other end of the limiting locking block is provided with a first connecting shaft, a sixth through hole is formed in the first connecting shaft, a connecting ring is connected in the sixth through hole, and two connecting rings of the first pair are connected through a safety rope.
An elastic piece is arranged in the placing hole.
The packing clamp is characterized in that a rotary connecting groove is formed in one side of the packing clamp shell, a connecting block is arranged in the rotary connecting groove, a connecting sleeve is arranged on the connecting block, a connecting support ring is arranged on one side of the packing clamp shell, which is provided with the rotary connecting groove, a first connecting hole is formed in the connecting support ring, a connecting shaft is rotationally arranged in the first connecting hole and the connecting sleeve, a first supporting block is rotationally arranged on the connecting shaft and comprises a first supporting block main body, and a seventh through hole and an eighth through hole are formed in the first supporting block main body.
The cabin body is internally provided with a symmetrically-distributed throwing device, the throwing device comprises a throwing box body, the throwing box body comprises a throwing shell, a V-shaped funnel is arranged below the shell, a throwing outlet is arranged below the V-shaped funnel, a symmetrically-distributed supporting connecting plate is arranged below the V-shaped funnel, an accelerating shaft which is symmetrically distributed is rotationally connected to the supporting connecting plate, one end of the accelerating shaft is provided with a second motor, and the second motor is fixed on the supporting connecting plate.
The one end of throwing the box is equipped with first support connecting plate, and the other end is equipped with the second support connecting plate, is equipped with the baffle of array distribution in the throwing the box, and the baffle will throw the box and cut apart the different region of length, baffle one end and first support connecting plate fastening connection, the other end and second support connecting plate fastening connection all are equipped with on the both ends in every region, first support connecting plate and the second support connecting plate with arcwall face complex arc draw-in groove.
The first support connecting plate and the second support connecting plate are provided with arc-shaped movable grooves distributed in an array mode, and the partition plates are provided with square grooves distributed symmetrically.
The first steering engine, the second steering engine, the third steering engine and the fourth steering engine are sequentially arranged on two sides of the second support connecting plate from top to bottom, the first limiting mechanism is arranged on the second steering engine and comprises a third connecting rod, one end of the third connecting rod is fixedly connected with an output shaft of the second steering engine, the other end of the third connecting rod is rotationally connected with the fourth connecting rod, a fifth connecting rod is rotationally connected with a first opposite end of the fourth connecting rod, a control shaft is fixedly connected to the fifth connecting rod, second supporting blocks which are symmetrically distributed are arranged on the control shaft, and the control shaft is rotationally connected with the second support connecting plate and the first support connecting plate.
And a second limiting mechanism is arranged on the fourth steering engine.
And a third limiting mechanism and a fourth limiting mechanism are respectively arranged on the first steering engine and the third steering engine.
Further, the disassembly shell is fixed in the filling clamp inlet through a screw rod.
Further, the rotating shaft is positioned in the second through hole to rotate through a bearing; the second belt pulley is positioned in the first through hole through the fixed shaft to rotate; the bottom plate is positioned in the sliding groove through the first sliding shaft and guided in a sliding manner.
Further, the bottom plate is in contact transmission with the belt through the contact shaft, and the first motor controls the bottom plate to be located on and off in the cabin throwing port.
Further, the elastic piece is sleeved on the second sliding shaft, one end of the elastic piece acts on the inner wall of the placement hole, and the other end acts on the locking piece; the first supporting block is rotationally connected with the connecting shaft through a seventh through hole and is rotationally connected with the second connecting rod through the eighth through hole and the pin shaft.
Further, one end of the second connecting rod is rotationally connected with the first connecting rod, the other end of the second connecting rod is rotationally connected with the first supporting block, and the rotation of the first supporting block is controlled through up-and-down movement of the first connecting rod to limit the thrown objects in the filling clamp shell.
Further, the rotation directions of the two second motors are opposite, and the symmetrically distributed accelerating shafts accelerate and throw the thrown objects; the filling clamps distributed in the array are clamped in the arc-shaped clamping grooves through the arc-shaped surfaces, and the filling clamps are limited and fixed through the support rods distributed in a weighing mode.
Further, the throwing devices which are symmetrically distributed are contacted with each other through the first supporting connecting plates, the first limiting mechanism is identical to the second limiting mechanism, and the second supporting blocks controlled by the first limiting mechanism and the second limiting mechanism are located in the same area where the throwing box body is divided by the partition plate.
Further, the third limiting mechanism and the fourth limiting mechanism have the same structure as the first limiting mechanism, and the difference is that the length of the fourth connecting rod is different, so that the second supporting blocks controlled by the first limiting mechanism and the third limiting mechanism are positioned in different areas of the partition plate for dividing the throwing box body, and the second supporting blocks controlled by the third limiting mechanism and the fourth limiting mechanism are positioned in the same area of the partition plate for dividing the throwing box body.
Further, the second support connecting plate is provided with symmetrically distributed support connecting sleeves, and the support connecting sleeves are matched with the screw rods to fix the throwing device on the support frame.
The invention has the beneficial effects that:
1. according to the throwing device, the safety rope is pulled, so that the locking block is separated from the fifth through hole, the first connecting rod is pushed to move downwards, the first supporting block is in a vertical state, the limit of the throwing outlet of the filling clamp is canceled, at the moment, the throwing objects are placed into the filling clamp from the throwing outlet of the filling clamp, and the bearing of a plurality of throwing objects is realized;
2. according to the throwing device, the throwing objects fall into the V-shaped funnel, the throwing objects are accelerated to be thrown out through the accelerating shaft at the throwing outlet, an initial speed of the throwing objects is set, continuous and stable throwing of a plurality of throwing objects is achieved, the filling clamp can be used repeatedly, and throwing cost is reduced.
Drawings
The invention is further described below with reference to the accompanying drawings.
FIG. 1 is a schematic view of a dispensing apparatus of the present invention;
FIG. 2 is a schematic view of the structure of the throwing device of the present invention;
FIG. 3 is a schematic view of the structure of the dispensing device of the present invention;
FIG. 4 is a schematic view of the structure of the base plate of the present invention;
FIG. 5 is a schematic view of the structure of the filling clip of the present invention;
FIG. 6 is a schematic view of a portion of the fill clip of the present invention;
FIG. 7 is a schematic view of a portion of the fill clip of the present invention;
FIG. 8 is a cross-sectional view of a portion of the structure of the filling clip of the present invention;
FIG. 9 is a schematic view of a portion of the fill clip of the present invention;
FIG. 10 is a schematic view of the structure of the throwing apparatus of the present invention;
FIG. 11 is a schematic view of a part of the structure of the throwing apparatus of the present invention;
fig. 12 is a schematic view of a part of the structure of the throwing apparatus of the present invention.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
The utility model provides a cabin-type article throwing device in aircraft, throwing device is located cabin 1, and as shown in fig. 1, fig. 2, and cabin 1 includes cabin main part 11, and the top of cabin main part 11 is equipped with fills and presss from both sides entry 12, fills and presss from both sides entry 12 in being equipped with and dismantle shell 2, and dismantle shell 2 passes through the screw rod to be fixed in filling and presss from both sides entry 12, and the below of cabin main part 11 is equipped with cabin throwing mouth 15.
The cabin main body 11 is internally provided with symmetrically distributed supporting frames 13, and symmetrically distributed supporting rods 131 are arranged between the supporting frames 13.
The cabin main body 11 is provided with support plates 14 distributed in an array, the support plates 14 are provided with first through holes 141 and second through holes 142, and the inner sides of the support plates 14 are provided with sliding grooves 143, as shown in fig. 3.
The cabin cover opening device 3 is arranged in the cabin main body 11, as shown in fig. 3, the cabin cover opening device 3 comprises a first motor 31 which is symmetrically distributed, the first motor 31 is fixed on the supporting plate 14, a rotating shaft 32 which is symmetrically distributed is arranged on the first motor 31, the rotating shaft 32 is positioned in the second through hole 142 to rotate through a bearing, a first belt pulley 33 which is symmetrically distributed is arranged on the rotating shaft 32, a second belt pulley 34 is arranged on the two opposite supporting plates 14, the second belt pulley 34 is positioned in the first through hole 141 to rotate through a fixed shaft, the second belt pulley 34 is rotatably connected with the first belt pulley 33 through a belt 35, and the belt 35 has toughness.
The hatch cover opening device 3 comprises a symmetrically distributed bottom plate 36, as shown in fig. 4, the bottom plate 36 is positioned in a cabin throwing port 15, the bottom plate 36 comprises a bottom plate main body 361, a symmetrically distributed first connecting block 362 is arranged on the bottom plate main body 361, a first sliding shaft 363 is arranged on one side of the first connecting block 362, the bottom plate 36 is positioned in a sliding chute 143 through the first sliding shaft 363 and guided in a sliding manner, a symmetrically distributed second connecting block 364 is arranged on the first connecting block 362, a third through hole 365 is arranged on the second connecting block 364, a contact shaft 366 is arranged in the third through hole 365 in a rotating manner, the bottom plate 36 is in contact transmission with a belt 35 through the contact shaft 366, and the first motor 31 controls the opening and closing of the bottom plate 36 positioned in the cabin throwing port 15.
The cabin 1 is internally provided with filling clamps 4 distributed in an array manner, as shown in fig. 1, 5, 6 and 7, the filling clamps 4 comprise filling clamp shells 41, handles 42 are arranged on the filling clamps 4, filling clamp throwing outlets 401 are arranged below the filling clamps 4, two sides of the filling clamp shells 41 are respectively provided with side plates 411, and two ends of each side plate 411 are respectively provided with an arc-shaped surface 4111.
The side plate 411 is provided with limit blocks 413 distributed in an array, the limit blocks 413 are provided with limit sliding holes 414, the limit sliding holes 414 are slidably provided with first connecting rods 43, the first ends of the first connecting rods 43 are provided with fourth through holes 431 and fifth through holes 432, and the other ends of the first connecting rods 43 are rotatably connected with second connecting rods 44.
The opposite side of the side plate 411 is provided with a connection post 412, and as shown in fig. 8, one end of the connection post 412 is provided with a sliding hole 4121, and the other end is provided with a placement hole 4122, and the placement hole 4122 communicates with the sliding hole 4121.
The side plate 411 is provided with the spring pin 45, the spring pin 45 comprises a second sliding shaft 451, one end of the second sliding shaft 451 is provided with a locking piece 452, the other end of the second sliding shaft 451 is provided with a limiting locking piece 453, one end of the limiting locking piece 453 is fixedly connected with the second sliding shaft 451, the other end of the limiting locking piece 453 is provided with a first connecting shaft 454, the first connecting shaft 454 is provided with a sixth through hole 455, a connecting ring 47 is connected in the sixth through hole 455, and the two connecting rings 47 of the first pair are connected through a safety rope 48.
The elastic member 46 is provided in the placement hole 4122, the elastic member 46 is fitted over the second sliding shaft 451, one end of the elastic member 46 acts on the inner wall of the placement hole 4122, and the other end acts on the lock piece 452.
The filling clamp shell 41 is provided with a rotary connecting groove 415 on one side, a connecting block 416 is arranged in the rotary connecting groove 415, a connecting sleeve 417 is arranged on the connecting block 416, a connecting support ring 418 is arranged on one side, provided with the rotary connecting groove 415, of the filling clamp shell 41, a first connecting hole 4181 is arranged on the connecting support ring 418, a connecting shaft 419 is rotationally arranged on the first connecting hole 4181 and the connecting sleeve 417, a first supporting block 49 is rotationally arranged on the connecting shaft 419, the first supporting block 49 comprises a first supporting block main body 491, a seventh through hole 493 and an eighth through hole 492 are arranged on the first supporting block main body 491, the first supporting block 49 is rotationally connected with the connecting shaft 419 through the seventh through hole 493, and is rotationally connected with the second connecting rod 44 through the eighth through hole 492 and a pin shaft.
One end of the second link 44 is rotatably connected to the first link 43, and the other end is rotatably connected to the first supporting block 49, and the rotation of the first supporting block 49 is controlled by the up-and-down movement of the first link 43, so that the thrown article in the filling clip case 41 is limited.
The cabin main body 11 is internally provided with a symmetrically-distributed throwing device 5, as shown in fig. 10, the throwing device 5 comprises a throwing box body 51, the throwing box body 51 comprises a throwing shell 511, a V-shaped funnel 512 is arranged below the shell 511, a throwing outlet 514 is arranged below the V-shaped funnel 512, a symmetrically-distributed support connecting plate 513 is arranged below the V-shaped funnel 512, a symmetrically-distributed accelerating shaft 515 is rotationally connected to the support connecting plate 513, one end of the accelerating shaft 515 is provided with a second motor 516, the second motor 516 is fixed on the support connecting plate 513, the rotation directions of the two second motors 516 are opposite, and the symmetrically-distributed accelerating shaft 515 is used for accelerating and throwing out a throwing object.
One end of the throwing box body 51 is provided with a first supporting connecting plate 59, the other end of the throwing box body 51 is provided with a second supporting connecting plate 52, the throwing box body 51 is internally provided with partition plates 50 distributed in an array mode, the partition plates 50 divide the throwing box body 51 into areas with different lengths, one end of each partition plate 50 is fixedly connected with the first supporting connecting plate 59, the other end of each partition plate 50 is fixedly connected with the second supporting connecting plate 52, two ends in each area, the first supporting connecting plate 59 and the second supporting connecting plate 52 are respectively provided with an arc clamping groove 521 matched with an arc surface 4111, filling clamps 4 distributed in an array mode are clamped in the arc clamping grooves 521 through the arc surfaces 4111, and the filling clamps 4 are limited and fixed through support rods 131 distributed in a weighing mode.
The symmetrically distributed throwing apparatuses 5 are in contact with each other through the first support connection plates 59.
The first support connecting plate 59 and the second support connecting plate 52 are provided with arc-shaped moving grooves 522 distributed in an array manner, and the partition plate 50 is provided with square grooves 501 distributed symmetrically.
The first steering engine 523, the second steering engine 524, the third steering engine 525 and the fourth steering engine 526 are sequentially arranged on two sides of the second support connecting plate 52 from top to bottom, as shown in fig. 11 and 12, a first limiting mechanism is arranged on the second steering engine 524, the first limiting mechanism comprises a third connecting rod 53, one end of the third connecting rod 53 is fixedly connected with an output shaft of the second steering engine 524, the other end of the third connecting rod 53 is rotatably connected with a fourth connecting rod 54, a first opposite end of the fourth connecting rod 54, which is rotatably connected with the third connecting rod 53, is rotatably connected with a fifth connecting rod 55, a control shaft 56 is fixedly connected with the fifth connecting rod 55, second supporting blocks 57 which are symmetrically distributed are arranged on the control shaft 56, and the control shaft 56 is rotatably connected with the second support connecting plate 52 and the first support connecting plate 59.
The fourth steering engine 526 is provided with a second limiting mechanism, the first limiting mechanism is identical to the second limiting mechanism, and a second supporting block 57 controlled by the first limiting mechanism and the second limiting mechanism is located in the same area where the partition plate 50 partitions the throwing box 51.
The first steering engine 523 and the third steering engine 525 are respectively provided with a third limiting mechanism and a fourth limiting mechanism, the third limiting mechanism and the fourth limiting mechanism are identical to the first limiting mechanism in structure, and the difference is that the length of the fourth connecting rod 54 is different, so that the second supporting blocks 57 controlled by the first limiting mechanism and the third limiting mechanism are positioned in different areas of the partition 50 for dividing the throwing box 51, and the second supporting blocks 57 controlled by the third limiting mechanism and the fourth limiting mechanism are positioned in the same area of the partition 50 for dividing the throwing box 51.
The second support connecting plate 52 is provided with symmetrically distributed support connecting sleeves 58, and the support connecting sleeves 58 are matched with the screw rods to fix the throwing device 5 on the support frame 13.
When the device is used, the lock piece 452 is separated from the fifth through hole 432 by pulling the safety rope 48, the first connecting rod 43 is pushed to move downwards, the first supporting blocks 49 are in a vertical state, the limit of the filling clamp throwing outlet 401 is canceled, at the moment, a throwing object is placed into the filling clamp 4 from the filling clamp throwing outlet 401, after the filling clamp 4 is filled, the first connecting rod 43 is pulled to move upwards, the spring pin 45 is clamped in the fifth through hole 432 under the action of the elastic piece 46, at the moment, the first supporting blocks 49 are in a horizontal state to limit the throwing object in the filling clamp 4, the filling clamp 4 is placed on the throwing device 5 through the filling clamp inlet 12 by pulling the handle 42, the filling clamps 4 distributed in an array are clamped in the arc-shaped clamping grooves 521 through the arc-shaped surfaces 4111, the safety rope 48 is pulled, at the moment, the first supporting blocks 49 move downwards under the action of the gravity of the throwing object, the safety rope 48 is loosened, the first supporting blocks 49 are fixed in the fourth through the spring pin 45 and clamped in the fourth through the through hole 431, and the filling object is dismounted by the second supporting blocks 57 close to one side of the filling clamp 4.
When the aircraft flies to the appointed position, the steering engine on the second supporting block 57 which is close to one side of the filling clamp 4 below the filling clamp 4 rotates, so that the thrown article falls on the next second supporting block 57, at the moment, the steering engine on the second supporting block 57 which is close to one side of the filling clamp 4 rotates back, the second supporting block 57 is enabled to be vertical to the horizontal state to limit the rest thrown article, at the moment, the steering engine on the second supporting block 57 which is far away from one side of the filling clamp 4 rotates, so that the thrown article falls into the V-shaped funnel 512, the first motor 31 controls the bottom plate 36 to be started, and the thrown article is accelerated to be thrown out through the acceleration shaft 515 at the throwing outlet 514.
In the description of the present specification, the descriptions of the terms "one embodiment," "example," "specific example," and the like, mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present invention. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiments or examples. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The foregoing has shown and described the basic principles, principal features and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present invention, and various changes and modifications may be made without departing from the spirit and scope of the invention, which is defined in the appended claims.
Claims (8)
1. The cabin type article throwing device in the aircraft is arranged in an aircraft cabin (1) and is characterized in that the cabin (1) comprises a cabin main body (11), a filling clamp inlet (12) is arranged above the cabin main body (11), a disassembly shell (2) is arranged in the filling clamp inlet (12), and a cabin throwing port (15) is arranged below the cabin main body (11);
Symmetrically distributed supporting frames (13) are arranged in the cabin main body (11), and symmetrically distributed supporting rods (131) are arranged between the supporting frames (13);
The cabin body (11) is internally provided with support plates (14) distributed in an array manner, the support plates (14) are provided with first through holes (141) and second through holes (142), and the inner sides of the support plates (14) are provided with sliding grooves (143);
The cabin cover opening device (3) is arranged in the cabin main body (11), the cabin cover opening device (3) comprises first motors (31) which are symmetrically distributed, the first motors (31) are fixed on the supporting plates (14), rotating shafts (32) which are symmetrically distributed are arranged on the first motors (31), first belt pulleys (33) which are symmetrically distributed are arranged on the rotating shafts (32), second belt pulleys (34) are arranged on the two opposite supporting plates (14), and the second belt pulleys (34) are rotationally connected with the first belt pulleys (33) through belts (35);
The cabin cover opening device (3) comprises a bottom plate (36) which is symmetrically distributed, the bottom plate (36) is positioned in a cabin throwing port (15), the bottom plate (36) comprises a bottom plate main body (361), first connecting blocks (362) which are symmetrically distributed are arranged on the bottom plate main body (361), a first sliding shaft (363) is arranged on one side of each first connecting block (362), second connecting blocks (364) which are symmetrically distributed are arranged on each first connecting block (362), a third through hole (365) is formed in each second connecting block (364), and a contact shaft (366) is rotationally arranged in each third through hole (365);
Filling clamps (4) distributed in an array are arranged in the cabin (1), each filling clamp (4) comprises a filling clamp shell (41), a handle (42) is arranged on each filling clamp (4), a filling clamp throwing outlet (401) is arranged below each filling clamp (4), side plates (411) are arranged on two sides of each filling clamp shell (41), and arc-shaped surfaces (4111) are arranged at two ends of each side plate (411);
Limiting blocks (413) distributed in an array are arranged on the side plates (411), limiting sliding holes (414) are formed in the limiting blocks (413), first connecting rods (43) are arranged in the limiting sliding holes (414) in a sliding mode, fourth through holes (431) and fifth through holes (432) are formed in the first ends of the first connecting rods (43), and second connecting rods (44) are connected to the other ends of the first connecting rods in a rotating mode;
The opposite sides of the side plates (411) are provided with connecting columns (412), one end of each connecting column (412) is provided with a sliding hole (4121), the other end of each connecting column is provided with a placing hole (4122), and the placing holes (4122) are communicated with the sliding holes (4121);
the side plate (411) is provided with a spring pin (45), the spring pin (45) comprises a second sliding shaft (451), one end of the second sliding shaft (451) is provided with a locking block (452), the other end of the second sliding shaft is provided with a limiting locking block (453), one end of the limiting locking block (453) is fixedly connected with the second sliding shaft (451), the other end of the limiting locking block is provided with a first connecting shaft (454), the first connecting shaft (454) is provided with a sixth through hole (455), a connecting ring (47) is connected in the sixth through hole (455), and the two opposite connecting rings (47) are connected through a safety rope (48);
an elastic piece (46) is arranged in the placing hole (4122);
One side of the filling clamp shell (41) is provided with a rotating connecting groove (415), a connecting block (416) is arranged in the rotating connecting groove (415), a connecting sleeve (417) is arranged on the connecting block (416), one side of the filling clamp shell (41) provided with the rotating connecting groove (415) is provided with a connecting support ring (418), the connecting support ring (418) is provided with a first connecting hole (4181), the first connecting hole (4181) and the connecting sleeve (417) are rotationally provided with a connecting shaft (419), the connecting shaft (419) is rotationally provided with a first supporting block (49), the first supporting block (49) comprises a first supporting block main body (491), and the first supporting block main body (491) is provided with a seventh through hole (493) and an eighth through hole (492);
The cabin body (11) is internally provided with symmetrically-distributed throwing devices (5), each throwing device (5) comprises a throwing box body (51), each throwing box body (51) comprises a throwing shell (511), a V-shaped funnel (512) is arranged below each shell (511), a throwing outlet (514) is arranged below each V-shaped funnel (512), symmetrically-distributed support connecting plates (513) are arranged below each V-shaped funnel (512), symmetrically-distributed accelerating shafts (515) are rotatably connected to the support connecting plates (513), a second motor (516) is arranged at one end of each accelerating shaft (515), and the second motors (516) are fixed on the support connecting plates (513);
One end of the throwing box body (51) is provided with a first supporting connecting plate (59), the other end of the throwing box body is provided with a second supporting connecting plate (52), the throwing box body (51) is internally provided with partition plates (50) distributed in an array, the partition plates (50) divide the throwing box body (51) into different areas, one end of each partition plate (50) is fixedly connected with the first supporting connecting plate (59), the other end of each partition plate is fixedly connected with the second supporting connecting plate (52), and arc clamping grooves (521) matched with arc surfaces (4111) are formed in two ends in each area, the first supporting connecting plate (59) and the second supporting connecting plate (52);
Arc-shaped movable grooves (522) distributed in an array manner are formed in the first support connecting plate (59) and the second support connecting plate (52), and square grooves (501) distributed symmetrically are formed in the partition plate (50);
The two sides of the second support connecting plate (52) are sequentially provided with a first steering engine (523), a second steering engine (524), a third steering engine (525) and a fourth steering engine (526) up and down, the second steering engine (524) is provided with a first limiting mechanism, the first limiting mechanism comprises a third connecting rod (53), one end of the third connecting rod (53) is fixedly connected with an output shaft of the second steering engine (524), the other end of the third connecting rod is rotationally connected with a fourth connecting rod (54), the opposite end of the fourth connecting rod (54) which is rotationally connected with the third connecting rod (53) is rotationally connected with a fifth connecting rod (55), a control shaft (56) is fixedly connected with the fifth connecting rod (55), the control shaft (56) is provided with second supporting blocks (57) which are symmetrically distributed, and the control shaft (56) is rotationally connected with the second support connecting plate (52) and the first support connecting plate (59);
a second limiting mechanism is arranged on the fourth steering engine (526);
a third limiting mechanism and a fourth limiting mechanism are respectively arranged on the first steering engine (523) and the third steering engine (525);
the rotating shaft (32) is positioned in the second through hole (142) to rotate through a bearing; the second belt pulley (34) is positioned in the first through hole (141) to rotate through the fixed shaft; the bottom plate (36) is positioned in the sliding groove (143) through a first sliding shaft (363) and guided in a sliding way;
the bottom plate (36) is in contact transmission with the belt (35) through the contact shaft (366), and the first motor (31) controls the opening and closing of the bottom plate (36) in the cabin throwing port (15).
2. An aircraft interior compartment item delivery device according to claim 1, wherein the disassembly housing (2) is secured in the filling clip inlet (12) by means of a screw.
3. An aircraft interior compartment type article dispensing device according to claim 1, wherein the elastic member (46) is fitted over the second sliding shaft (451), one end of the elastic member (46) acts on the inner wall of the placement hole (4122), and the other end acts on the lock piece (452); the first supporting block (49) is rotatably connected with the connecting shaft (419) through a seventh through hole (493), and is rotatably connected with the second connecting rod (44) through the eighth through hole (492) and the pin shaft.
4. The aircraft interior compartment type article dispensing device according to claim 1, wherein one end of the second link (44) is rotatably connected to the first link (43), and the other end is rotatably connected to the first support block (49), and the rotation of the first support block (49) is controlled by the up-and-down movement of the first link (43), so that the article to be thrown in the filling clip case (41) is limited.
5. An aircraft interior compartment type article dispensing device according to claim 1, wherein the rotation directions of the two second motors (516) are opposite, and symmetrically distributed acceleration shafts (515) are used for accelerating and ejecting the articles to be thrown; filling clamp (4) that the array distributes is blocked in arc draw-in groove (521) through arcwall face (4111), carries out spacing fixed to filling clamp (4) through bracing piece (131) that scale was distributed.
6. The aircraft interior compartment type article throwing device according to claim 1, wherein the throwing devices (5) which are symmetrically distributed are contacted with each other through a first supporting connection plate (59), the first limiting mechanism is identical to the second limiting mechanism, and a second supporting block (57) controlled by the first limiting mechanism and the second limiting mechanism is positioned in the same area where the throwing box body (51) is divided by the partition plate (50).
7. The device for throwing articles into an aircraft interior cabin according to claim 1, wherein the third and fourth limiting mechanisms are identical in structure to the first limiting mechanism, and the difference is that the fourth connecting rod (54) is different in length, so that the second supporting blocks (57) controlled by the first limiting mechanism and the third limiting mechanism are located in different areas of the partition plate (50) for dividing the throwing box (51), and the second supporting blocks (57) controlled by the third limiting mechanism and the fourth limiting mechanism are located in the same area of the partition plate (50) for dividing the throwing box (51).
8. An aircraft interior compartment article dispensing device according to claim 1, characterized in that the second support connection plate (52) is provided with symmetrically distributed support connection sleeves (58), and the support connection sleeves (58) are matched with screws to fix the dispensing device (5) on the support frame (13).
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910665505.2A CN110239717B (en) | 2019-07-23 | 2019-07-23 | Cabin type article throwing device in aircraft |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910665505.2A CN110239717B (en) | 2019-07-23 | 2019-07-23 | Cabin type article throwing device in aircraft |
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| CN110239717A CN110239717A (en) | 2019-09-17 |
| CN110239717B true CN110239717B (en) | 2024-05-07 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201910665505.2A Active CN110239717B (en) | 2019-07-23 | 2019-07-23 | Cabin type article throwing device in aircraft |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN111025984B (en) * | 2019-12-23 | 2021-02-26 | 中国科学院光电研究院 | Near space ball carries control device that jettisonings |
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| CN106184757A (en) * | 2016-07-15 | 2016-12-07 | 杭州迅蚁网络科技有限公司 | A kind of unmanned plane goods loads and jettison system automatically |
| 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 |
| US9676481B1 (en) * | 2015-03-27 | 2017-06-13 | Amazon Technologies, Inc. | Tether compensated airborne delivery |
| CN107000843A (en) * | 2016-11-18 | 2017-08-01 | 深圳市大疆创新科技有限公司 | Survival aids delivery device and unmanned vehicle |
| 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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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2965794A1 (en) * | 2010-10-07 | 2012-04-13 | France Etat | SOLIDARIZATION DEVICE / DESOLIDARIZATION DEVICE AND RELATIVE DEVICE |
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|---|---|---|---|---|
| US9676481B1 (en) * | 2015-03-27 | 2017-06-13 | Amazon Technologies, Inc. | Tether compensated airborne delivery |
| CN106184757A (en) * | 2016-07-15 | 2016-12-07 | 杭州迅蚁网络科技有限公司 | A kind of unmanned plane goods loads and jettison system automatically |
| 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 |
| CN107000843A (en) * | 2016-11-18 | 2017-08-01 | 深圳市大疆创新科技有限公司 | Survival aids delivery device and unmanned vehicle |
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| CN110239717A (en) | 2019-09-17 |
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