JP5039738B2 - Air carrier and method - Google Patents

Description

  The present invention relates to an air carrier used for an air transportation facility and an air transportation method using the air carrier.

  One facility for transporting goods to a destination is an air transportation facility that uses the flow of airflow in a pipe. In the air-feeding facility, a container for storing articles therein and transporting them to a remote place is called an air-feeder.

  For example, in the nuclear power plant, the air transportation facility is used as a facility for transporting a sample collected for inspection (for example, a radioactive object such as a spent fuel rod dissolved in a strong acid) to a destination. ing.

  FIG. 11 (A) is a front view of an example of a conventional pneumatic feeder, and FIG. 11 (B) is a side view of the pneumatic carrier shown in FIG. 11 (A).

  An air carrier 90 shown in FIG. 11A has a cylindrical body portion 91 and circular collar portions 92 and 93 having the same central axis as the body portion 91 at a location away from the body portion 91. Further, the body portion 91 has a tapered end portion 911 on the side of the collar portion 92, and the other end portion 912 has an opening 95 in the space 98 for storing the article BP in the air carrier inside the main body. Has been. The opening 95 has a cap 94 for closing the opening 95. The air carrier 90 is a rotating body around the shaft 9c.

  The movement of the pneumatic carrier 90 in the pipe P will be described.

  The air feed element 90 disposed in the pipe P is pressed by the air flow 96 or the air flow 97 in the pipe generated by a blower or an exhaust fan (not shown) provided at the end of the pipe. The pipe P moves in the same direction as the directions of the airflows 96 and 97. The diameters of the collar portions 92 and 93 are the same.

  In the pneumatic carrier 90, the diameters 9e of the collar portions 92 and 93 are set to a size that allows the airflows 96 and 97 in the pipe to effectively act on the pneumatic carrier 90. If the diameter 9e is the same as the pipe inner diameter d, the airflows 96 and 97 most effectively act on the air carrier 90. However, a frictional force is generated between the pipe P and the collar portions 92 and 93, and in the worst case, The air carrier 90 cannot move in the pipe P. Moreover, even if the movement is barely possible, problems such as the inability to move the bending portion occur. Therefore, it is necessary to make the flange portion diameter 9e smaller than the pipe inner diameter d and provide a gap 9f. However, if the flange diameter 9e is too smaller than the pipe inner diameter d, in other words, if the gap 9f is too large, the area of the air carrier 90 that receives the air currents 96 and 97 is reduced, and the air current acting on the air carrier 90 is reduced. As a result, the moving speed of the pneumatic carrier 90 decreases.

  Further, by providing the gap 9f, an air flow is generated in the gap 9f, and it is possible to generate a so-called gas bearing effect that prevents contact friction between the pipe P and the collar portions 92 and 93. In the gap 9f, there is an air flow at substantially the same speed although there is a slight fluctuation. The airflow acts on the air carrier 90 with the same or substantially equal pressure, and as a result, the pressure applied to the air carrier is balanced.

  Accordingly, the diameter 9e of the collar portions 92 and 93 is optimally selected based on the moving speed of the pneumatic feeder, the inner diameter of the pipe, the air flow rate, the weight of the pneumatic feeder, the curvature of the pipe line, and the like.

  Moreover, not only the thing which has the collar parts 92 and 93 like the above-mentioned Example but the air carrier which does not have a collar part is also considered. In that case, the diameter of the body part of the air carrier approaches the inner diameter of the pipe.

JP 2002-12322 A

  However, even with an airliner with the diameter of the collar set optimally for the moving speed of the airliner, the ribs on the pipe pipe joint, small irregularities on the inner wall surface of the pipe, such as defective internal processing, etc. The parts touch and decelerate. At this time, the gap 9f becomes a contact portion and the gap becomes small, the flow velocity of the airflow flowing through the gap 9f increases, and the moving direction of the air feeder toward the air feeder at the contact portion with the pipe inner wall of the outer peripheral surface of the air carrier A force perpendicular to is generated. The posture of the air carrier changes due to a slight change in the local fluid pressure applied to the air carrier.

  FIGS. 12A and 12B schematically show the situation of this posture change. The pneumatic carrier 90 is moved in the direction of the arrow, and the posture shown in FIG. 12A and the posture shown in FIG. It becomes a state.

  When the air carrier starts to vibrate, the air flow in the pipe is disturbed, and the moving speed of the air carrier decreases, and in some cases, it does not move along the pipe and keeps vibrating in one place. It is possible.

  Further, speed reduction and movement stop due to vibration frequently occur when the pipeline is horizontal or vertical and straight.

  When the air carrier vibrates, problems such as breakage of articles stored inside, breakage of the air carrier itself, breakage of pipes, and the like occur.

  In view of such a problem, an object of the present invention is to provide an air carrier capable of conveying an article while maintaining a predetermined speed without causing vibration in a pipeline.

  Another object of the present invention is to provide an air carrier capable of transporting an article without causing damage to the article, the air carrier, a pipe or the like due to vibration.

In order to achieve the above object, the present inventor conducted research and obtained the following knowledge.
The pneumatic carrier moves in the pipe while maintaining its posture with a delicate balance of radial force. Once the balance of force is broken, vibration tends to occur. However, it was found that when a part of the air carrier has a different shape, the air carrier moves in a stable posture.

Therefore, the present invention is an air carrier that moves inside the transport pipeline along the flow of air current inside the circular pipe, and is formed in a cylindrical shape so that articles can be stored inside, The cross-sectional shape perpendicular to the axis is characterized in that it has an outer shape in which two flat portions of two semi-cylinders having different radii are bonded to each other while being radially displaced from each central axis.
In addition, the present invention is an air carrier that moves inside the transport pipeline along the flow of air current inside the circular pipe, and is formed in a cylindrical shape so that articles can be stored inside, is the cross-sectional shape perpendicular to the central axis, the flat portion of the two half cylinder each having the same radius, have a bonded contour in a state shifted in the radial directions from the respective central axes, said in outer shape A step due to a radial deviation gradually decreases in the axial direction of the central axis, and the two half-cylinders are smoothly connected to each other at an end in the axial direction. To do.
According to this configuration, the streamlines of the airflow generated in the moving direction are different at one or more places, and different portions of the streamlines are biased.

By doing in this way, the fluid pressure differs in the different part of the said streamline compared with another part. When airflow flows in the direction of movement of Kiokuko, to move the pipe in a state in which the force biased the gas Okuko is applied.

  As a result, even if the flow velocity of the air flow around the air carrier changes, the force due to the fluid pressure is applied to the air child in advance, and the inclination of the air carrier is unlikely to occur. Generation of vibration can be suppressed.

That is, since the streamlines of the airflow flowing on the surface are different from each other, the speed is changed and the fluid pressure is different. The force due to the difference in fluid pressure continues to act on the pneumatic feeder. The pneumatic feeder moves stably, and vibration of the pneumatic feeder can be prevented.

Further, in the pneumatic feeding method in which the pneumatic carrier is transported inside the circular pipe by the flow of the air current inside the circular pipe, the above pneumatic carrier is used as the pneumatic carrier.

  According to the present invention, it is possible to provide an air carrier that can convey an article while maintaining a predetermined speed without being vibrated in a pipeline.

  In addition, according to the present invention, it is possible to provide an air carrier capable of transporting the article without causing damage to the article, the air carrier, a pipe or the like due to vibration.

Fig. (A) is a front view of a first reference example of the pneumatic carrier according to the present invention, Fig. (B) is a side view, and Fig. (C) is a front view showing an inclined state. It is a front view of the modification of the 1st reference example of an air carrier shown in FIG. It is a front view of the 2nd reference example of an air carrier concerning the present invention. It is a front view of the modification of the 2nd reference example of an air carrier shown in FIG. It is a front view of the further third reference example of the pneumatic carrier according to the present invention. It is a side view of the modification of the 3rd reference example shown in FIG. It is the front view and left view of the 4th reference example of an air carrier concerning the present invention. It is the front view and left view of the 5th reference example of the pneumatic carrier which concerns on this invention. It is a positive plane view and a left side view of the pneumatic tube carrier according to the present invention. It is the front view and left view of the 6th reference example of the pneumatic carrier which concerns on this invention. It is the front view and left view which show an example of the conventional pneumatic feeder . It is the figure which showed the condition of the attitude | position change of a pneumatic carrier typically, Comprising: It is the figure which showed the self-excited vibration state of the pneumatic carrier.

( First Reference Example )
FIG. 1 shows a front view of a first reference example of an air carrier according to the present invention.

  An air carrier A shown in FIG. 1 includes a body 1 formed in a cylindrical shape, a first collar 2 formed on one end 11 side of the body 1, and the other end of the body 1. It has the 2nd collar part 3 formed in 12 side.

  As for the trunk | drum 1, one edge part 11 is formed in the taper surface, and the other edge part 12 is formed with the opening part for accommodating articles | goods. A cap 4 for covering the opening is provided. The body part 1 is a rotating body around the axis c.

  The first collar portion 2 has a cutout portion 21 obtained by removing a part (upper side in the drawing) of the rotating body centering on the axis c in the same manner as the body portion 1 in a planar shape.

  Although the shortest distance from the central axis c of the notch part 21 is not limited to it, it is the same as the radius h of the trunk | drum 1 here.

  Similarly to the body portion, the second collar portion 3 is a rotating body centered on the axis c, and a radius e1 of a portion excluding the notch portion 21 of the first collar portion 2 and a radius of the second collar portion 3. e2 is the same here, but may be different. Any of the radii e1 and e2 that can sufficiently receive the flow of the air flow FL in the pipe P and can move the air carrier A at a sufficient speed can be widely employed.

  The air carrier A reciprocates inside the pipe P to both the one end 11 side and the other end 12 side, but is not limited to this, for example, it moves only to the other end 12 side. It is good also as what to do.

  The air carrier A shown in FIG. 1 shows an example in which an airflow is flowing from one end portion 11 side to the other end portion 12 side, and an arrow indicates the flow of the airflow FL.

  The air flow FL flows into the gap f between the first flange portion 11 and the inner wall of the pipe P at the same time as the first flange portion 2 is pushed. The airflow FL1 flowing into the gap f flows along the pipe as it is, and flows into the gap g between the second collar portion 3 and the pipe P. Since the areas of the gaps f and g are very small compared to the area inside the pipe P, the flow velocity of the air flow FL1 is very fast compared to the flow velocity of the air flow FL. Moreover, in the notch part 21, the notch part 21 and the pipe P inner surface form the clearance gap f1.

  Since the areas of the gap f and the gap f1 are different, the flow velocity of the airflow flowing through the gaps f and f1 is also different, and as a result, the fluid pressure acting on the gaps f and f1 is also different. Further, since the flow velocity flowing through the gaps f and f1 is fast, the flow velocity changes greatly even if the area changes slightly, and therefore the fluid pressure also changes greatly.

Due to the difference in the speed of the air flow FL1, a force M due to fluid pressure acts on the notch 21 of the air carrier A as shown in FIG. As a result, Kiokuko A is a force M, moves within the pipe P in an inclined position (see FIG. 1 (C)).

  In the state where the fluid pressure is applied in advance, the posture is maintained and the inside of the pipe P is moved, so that it is difficult to be affected by the pressure change due to the turbulence of the air flow FL1.

FIG. 2 shows a front view of an air carrier of a modified example of the first reference example .

The pneumatic carrier A2 shown in FIG. 2 is substantially the same as the pneumatic carrier A of the first reference example except for the first collar portion and the second collar portion. Substantially the same parts are denoted by the same reference numerals.

  The air carrier A2 includes a first collar portion 2a that is a rotating body centered on the axis c as in the body portion 1, and a part of the rotating body that is centered on the axis c as in the body portion (in the drawing, It has the 2nd collar part 3a which has the notch part 31 which removed the upper side in planar shape.

  The shortest distance from the central axis c of the notch 31 is not limited to this, but here is the same as the radius h of the body 1.

Unlike the pneumatic carrier A shown in the first reference example , the pneumatic carrier A2 has a notch 31 in the second collar portion 3a, so that the inclination of the pneumatic carrier A shown in FIG. Tilt to the opposite side. Although the inclination is different, it is the same that the inside of the pipe P can be moved in an inclined posture .

In the above reference example , the notch 31 is notched to the same height as the body part 1, but is not limited thereto, and sufficient airflow is provided to portions other than the notch 31 and the notch. Those that cause a difference in speed can be widely adopted.

  The cutout portions 21 and 31 are provided in the first collar portion 2 and the second collar portion 3a, respectively, but are not limited thereto, and the force to the air feed caused by the fluid pressure is around the axis. It is possible to use a wide range of things that are not balanced.

( Second reference example )
FIG. 3 shows a front view of a second reference example of the pneumatic carrier according to the present invention.

The pneumatic carrier B shown in FIG. 3 is the same as the pneumatic carrier A shown in the first reference example except for the first collar portion and the second collar portion, and the same parts are denoted by the same reference numerals.

  The first collar 2b of the air carrier B is provided with a notch 21b, and the notch 31b is also formed in the second collar 3b. The notches 21b and 31b are formed at the same position as viewed from the traveling direction of the air carrier B (on the upper side of the air carrier B in the drawing).

The sizes of the notches 21b and 31b are the same (the collars 2b and 3b are notched so as to have the same height as the body 1 in a front view), and forces due to equal fluid pressure are generated. As a result, the air carrier B is pushed toward the notches 21b and 31b and moves inside the pipe P while being in contact with the pipe P.

In this reference example , the cutout portion 21b and the cutout portion 31b have the same size, but may have different sizes. At that time, since the fluid force acting on the notch is different, the posture is inclined.

Further, in this reference example , the notches 21b and 31b are provided at the same position when viewed from the traveling direction of the air carrier B, but one of the notches is at a position rotated around the axis c. A thing (refer FIG. 4) is also employable. Since the pulled in the direction notched Again, taking the inclined posture. In the above examples, the sizes of the notches 21b and 31b are the same, but they may be different.

( Third reference example )
FIG. 5 shows a front view of a third reference example of the pneumatic carrier according to the present invention .

  An air carrier C shown in FIG. 5 includes a cylindrical body portion 1c and a cap 4c that is detachably attached to the body portion 1c.

  The body portion 1c has a hollow inside, and can store articles therein, and can be covered with a cap 4c so as not to fall off. Further, a notch 41c is formed at the end of the body 1c opposite to the side where the cap 4c is attached.

When the air flow is in the air flow, the air feed element C changes the speed of the air flow at the notch 11c, and the fluid pressure changes due to the speed change. A force is applied to the notch 41c due to a change in fluid pressure, resulting in a tilted posture .

In the above reference example , the notch portion 11c is provided at the end portion of the body portion 1c, but is not limited thereto, and is provided over the entire length of the body portion 1c, or an intermediate portion other than the end portion. A material that can generate a difference in fluid pressure due to a change in airflow, such as a material having a notch, can be widely used. The notch need not necessarily include the end.

In the pneumatic carrier C of the above reference example, the notch portion 11c is cut in a straight line, but the invention is not limited thereto, and for example, a cross-sectional shape V-shaped like the pneumatic carrier C2 shown in FIG. Those having a notch 111c or the like, and those having a change in air flow and a difference in fluid pressure can be widely employed.

( 4th reference example )
FIG. 7 (A) shows a front view of a fourth reference example of an air carrier according to the present invention, and FIG. 7 (B) shows a left side view of the air carrier shown in FIG. 7 (A).

  An air carrier D shown in FIGS. 7A and 7B includes a cylindrical body 1d and a cap 4d that is detachably attached to the body 1d.

  A resistance portion 8d for changing the flow of the airflow is attached to the outer peripheral surface of the body portion 1d. The resistance portion 8d is airtightly connected along the outer peripheral surface of the body portion 1d. The resistance portion 8d is formed so as to cover a part of the body portion 1d in the circumferential direction. Moreover, it has the shape of the extent which covers a part also in the full length direction.

  By attaching the resistance portion 8d to the body portion 1d, the flow velocity of the airflow changes in the portion where the resistance portion 8d is attached, and the fluid pressure changes compared to the other portions, and the direction of travel of the air carrier D in that portion A vertical force acts on the. As a result, the air carrier D maintains its posture while being inclined with respect to the pipe P.

By maintaining the posture in an inclined state, vibration due to the fluid pressure due to the change in the velocity of the airflow can be prevented.

Although the resistance part 8d used for this reference example was the shape which covers only a part of trunk | drum 1d, it may cover over the full length. A wide variety of fluid pressure differences can be used due to changes in airflow.
Moreover, the front-end | tip of the trunk | drum 1d may be formed in the taper shape.

( 5th reference example )
FIG. 8 (A) shows a front view of a fifth reference example of the pneumatic carrier according to the present invention, and FIG. 8 (B) shows a left side view.

  An air carrier E shown in FIGS. 8A and 8B has a front end portion 11e and a rear end portion 12e, and includes a cap 4e that covers an opening of the air carrier E. As shown in FIGS. 8A and 8B, the centers of the front end portion 11e and the rear end portion 12e are shifted by α. And the front-end | tip part 11e and the rear-end part 12e have the taper shape where the axis | shaft with which it connected smoothly was bent.

  Since the airflow flows around the air carrier E, the lengths of the streamlines on the upper side 2e and the lower side 3e of the air carrier E differ from each other, and therefore, the flow rates of the air currents flowing through the portions 2e and 3e are different. Different flow velocities cause a difference in fluid pressure, resulting in a force. Since the force is applied in advance, it is possible to prevent the air feed E from vibrating due to a change in the fluid pressure due to the turbulence of the airflow.

(Embodiment of the present invention)
FIG. 9 (A) shows a front view of the pneumatic carrier according to the present invention, and FIG. 9 (B) shows a left side view.

  The body portion 1f of the air carrier F shown in FIGS. 9A and 9B is bonded with the semi-cylindrical first member 13f and the second member 14f having the same radius in a state where the central axes cf1 and cf2 are shifted by β. It has a combined shape. Moreover, the cap 4f which covers a hollow part is provided.

  In the case of the pneumatic carrier F shown in FIGS. 9 (A) and 9 (B), the flow velocity of the gaps 131f and 141f generated by the deviation between the first member 13f and the second member 14f changes compared to the other parts. Therefore, a change in fluid pressure occurs, and a force due to the pressure difference is applied to the body portion 1f. Thereby, the air carrier F can move stably.

( Sixth reference example )
FIG. 10A is a front view of a sixth reference example according to the present invention, and FIG. 10B is a left side view.

The pneumatic carrier G shown in FIGS. 10A and 10B has a radius R portion on the upper right side in FIG. 10B and a radius r portion on the left side in FIG. 10B. . The radius is R> r, so that when inserted into the circular pipe P, the size of the gap can be different, and the flow velocity is different. As a result, a difference occurs in the fluid pressure, and the force resulting from the fluid pressure acts on the air feed G, and the posture is maintained to move inside the pipe.

  From this, the air feed G is always subjected to a force due to a difference in fluid pressure, and can suppress vibration due to a change in air flow.

A, B, C, D, E, F, G Air transport element 1 Body part 2 First collar part 21 Notch part 3 Second collar part 31 Notch part 4 Cap P Pipe

Claims (3)

An airliner that moves inside the transport pipeline along the airflow inside the circular pipe,
It is formed in a cylindrical shape so that articles can be stored inside,
A pneumatic structure characterized in that the cross-sectional shape perpendicular to the central axis has an outer shape in which two flat portions of two semi-cylinders having different radii are bonded to each other while being radially displaced from each central axis. Child. An airliner that moves inside the transport pipeline along the airflow inside the circular pipe,
It is formed in a cylindrical shape so that articles can be stored inside,
Is the cross-sectional shape perpendicular to the central axis, the flat portion of the two half cylinder each having the same radius, have a bonded contour in a state shifted in the radial directions from the respective central axes,
A step due to the radial shift in the outer shape gradually decreases in the axial direction of the central axis, and the two half-cylinders are smoothly connected to each other at the end in the axial direction. An airy child characterized by that. In the air feeding method of conveying the air carrier inside the circular pipe by the air flow inside the circular pipe,
A pneumatic method using the pneumatic carrier according to claim 1 or 2 as the pneumatic carrier.

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