EP4405225A1 - Vacuum transportation system - Google Patents

Vacuum transportation system

Info

Publication number
EP4405225A1
EP4405225A1 EP22869559.9A EP22869559A EP4405225A1 EP 4405225 A1 EP4405225 A1 EP 4405225A1 EP 22869559 A EP22869559 A EP 22869559A EP 4405225 A1 EP4405225 A1 EP 4405225A1
Authority
EP
European Patent Office
Prior art keywords
tube
transportation system
vacuum
platform
vacuum transportation
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
EP22869559.9A
Other languages
German (de)
French (fr)
Other versions
EP4405225A4 (en
Inventor
Satyanarayanan Raghuraman Chakravarthy
Thiruchengode Mahalingam Muruganandam
Vibhor Jain
Rajaraman Sasisekaran
Anurag Patil
Dhalpe Abhishek Jayant
Vemireddy Sri Rishitha
Kishan Thakkar
Neel Balar
Siddhant Sagar Patole
Lokesh Kabdal
Chokkasamudram Anish
Ankit Bansal
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Indian Institute of Technology Madras
Original Assignee
Indian Institute of Technology Madras
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Indian Institute of Technology Madras filed Critical Indian Institute of Technology Madras
Publication of EP4405225A1 publication Critical patent/EP4405225A1/en
Publication of EP4405225A4 publication Critical patent/EP4405225A4/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B61RAILWAYS
    • B61BRAILWAY SYSTEMS; EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR
    • B61B13/00Other railway systems
    • B61B13/10Tunnel systems
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES, PROFILES OR LIKE SEMI-MANUFACTURED PRODUCTS OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C37/00Manufacture of metal sheets, rods, wire, tubes, profiles or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape
    • B21C37/06Manufacture of metal sheets, rods, wire, tubes, profiles or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape of tubes or metal hoses; Combined procedures for making tubes, e.g. for making multi-wall tubes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L13/00Electric propulsion for monorail vehicles, suspension vehicles or rack railways; Magnetic suspension or levitation for vehicles
    • B60L13/04Magnetic suspension or levitation for vehicles
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T30/00Transportation of goods or passengers via railways, e.g. energy recovery or reducing air resistance

Definitions

  • the present invention relates to the field of vacuum systems, and specifically relates to a vacuum transportation system.
  • High-speed transportation systems such as aircrafts have been contemplated for reducing overall time for commuting between places.
  • transportation systems contribute to enormous greenhouse gas emissions.
  • traditional transportation systems are responsible for major share of environmental pollution.
  • One way to reduce the environmental pollution caused through the aircrafts without compromising the performance, is by using a highspeed vacuum transportation system for travelling.
  • a high-speed vacuum transportation system requires a continuous tube infrastructure that is maintained at low pressures.
  • the high-speed vacuum transportation system has support structures that enable hyperloop pods/maglev vacuum trains to run at extremely high speeds.
  • the tube has to be robust, stiff, capable of holding vacuum, and long-lasting.
  • the tube needs to be thick for resisting loads acting on the tube from different sources.
  • An overall weight of the tube and a cost of manufacturing of the tube is increased due to increase in thickness of the tube. Since the tube is a major part of the vacuum transportation system, it is vital to decrease the cost of manufacturing of the tube.
  • Still another object of the present invention to reduce an overall weight of the vacuum transportation system.
  • the vacuum transportation system may include a tube, a platform, and a track.
  • the tube may hold a vacuum within.
  • the tube may comprise a skin and a framework.
  • the skin may be made of a metallic sheet and may resist load acting on the tube from one or more sources.
  • the one or more sources may comprise at least one of the vacuum inside the tube, wind outside the tube, and weight of the object moving inside the tube.
  • the framework may provide support to the skin.
  • the framework may comprise a plurality of formers, a plurality of flanges, and a plurality of longerons.
  • the plurality of formers may be separated from each other by a first predefined distance and positioned beneath the skin in a longitudinal direction of the tube.
  • the plurality of flanges may be separated from each other by a second predefined distance and positioned outside the skin in the longitudinal direction of the tube.
  • the plurality of longerons may connect consecutive formers of the plurality of formers with each other.
  • the platform may pass through and over a bottom area of the tube.
  • the platform may rest over a plurality of pylons placed longitudinally.
  • the track may be placed longitudinally on the platform. The track may enable movement of objects inside the tube.
  • the plurality of formers, the plurality of flanges, and the plurality of longerons may be made of one or more of stainless steel, aluminium, carbon fiber composite, and mild steel.
  • a layer of foam may be present between the tube and the plurality of pylons.
  • the plurality of pylons may be separated by a third predefined distance in the longitudinal direction of the tube.
  • the platform may be supported by a plurality of pillars over each pylon of the plurality of pylons for transferring loads of the objects moving inside the tube (204) to ground.
  • one or more vacuum pumps may be connected with the tube to maintain the vacuum.
  • the platform and the plurality of pylons may be made of concrete.
  • a plurality of rebars may arranged linearly within the platform for providing structural reinforcement to the platform.
  • FIG. 1 illustrates a perspective front view of a vacuum transportation system, in accordance with an embodiment of the present invention
  • FIG. 2A illustrates a perspective side view of a framework of the vacuum transportation system, in accordance with an embodiment of the present invention
  • Fig. 2B illustrates a perspective side view of a tube of the vacuum transportation system, in accordance with an embodiment of the present invention
  • FIG. 3 illustrates a perspective front view of the tube, in accordance with an embodiment of the present invention
  • FIG. 4 illustrates an exemplary perspective view of the platform of the vacuum transportation system, in accordance with an embodiment of the present invention
  • Fig. 5A illustrates von Mises equivalent stress plot obtained during simulation of a symmetric model of the vacuum transportation system, in accordance with an embodiment of the present invention.
  • Fig. 5B illustrates a factor of safety plot obtained during simulation of the vacuum transportation system, in accordance with an embodiment of the present invention.
  • Fig. 1 illustrates a perspective front view of a vacuum transportation system 100, in accordance with an embodiment of the present invention.
  • the vacuum transportation system 100 may include a skin 102, a plurality of formers 104, a plurality of flanges 106, a plurality of longerons 108, a platform 110, and a track 112.
  • the plurality of formers 104, the plurality of flanges 106, and the plurality of longerons 108 may contribute to a framework of the vacuum transportation system 100.
  • a structure of the framework has been described successively with reference to Fig. 2A.
  • Fig. 2A illustrates a perspective side view of a framework 202 of the vacuum transportation system 100, in accordance with an embodiment of the present invention.
  • the framework 202 may include stiffeners, such as the plurality of formers 104, the plurality of flanges 106, and the plurality of longerons 108.
  • the plurality of formers 104 may be used as circular stiffeners separated from each other by a first predefined distance in a longitudinal direction of the framework 202.
  • the plurality of flanges 106 may be used as circular stiffeners separated from each other by a second predefined distance in the longitudinal direction of the framework 200.
  • the first predefined distance and the second predefined distance may be determined on the basis of buckling of the plurality of longerons 108, a manufacturing method for the platform 110, requirements to maintain a leak proof environment, and a total cost of manufacturing of the vacuum transportation system 100.
  • the plurality of longerons 108 may connect consecutive formers of the plurality of formers 104 with each other. In one implementation, a longeron may be welded with two consecutive formers.
  • the plurality of formers 104, the plurality of flanges 106, and the plurality of longerons 108 may be made of a material like stainless steel, aluminium, carbon fiber composite, and mild steel. Tensile strength of the material may range from 100 MPa to 5000 MPa.
  • the framework 202 may provide a lightweight and safe supportive assembly for positioning the skin 102, to form a tube.
  • Fig. 2B illustrates a perspective side view of a tube 204 of the vacuum transportation system 100, in accordance with an embodiment of the present invention.
  • the plurality of formers 104 may be positioned beneath the skin 102 and the plurality of flanges 106 may be positioned outside the skin 102, as shown in Fig. 3 illustrating a perspective front view of the tube 204.
  • the skin 102 may be held between the plurality of formers 104 and the plurality of flanges 106.
  • the skin 102 may be supported from inside and outside by the plurality of formers 104 and the plurality of flanges 106 respectively.
  • buckling of the skin 102 may be prevented and stability of the tube 204 may be ensured by the plurality of formers 104 and the plurality of flanges 106.
  • the plurality of formers 104 and the plurality of flanges 106 may be present at same location in the longitudinal direction of the framework 200, and thus the first predefined distance may be equal to the second predefined distance.
  • the plurality of formers 104 and the plurality of flanges 106 may be present at different locations in the longitudinal direction of the framework 200, and thus the first predefined distance may not be equal to the second predefined distance.
  • the tube 204 may hold a vacuum within.
  • a shape of the tube 204 may be defined by a shape of the framework 202.
  • the shape of the tube 204 may be designed based on operational requirements.
  • the tube 204 may be present in a circular shape.
  • the tube 204 may be present in other shapes, such as rectangle, square, and hexagon.
  • the skin 102 may be made of a high strength material, such as a metallic material.
  • the skin 102 may resist load acting on the tube 204 from one or more sources.
  • the one or more sources may comprise at least one of the vacuum inside the tube 204, wind outside the tube 204, and weight of an object moving inside the tube 204.
  • Examples of the object may include, but not limited to, hyperloop pods, maglev trains, or any other vehicle capable of travelling through the vacuum transportation system 100.
  • Fig. 4 illustrates an exemplary perspective view of the platform 110 of the vacuum transportation system 100, in accordance with an embodiment of the present invention.
  • the platform 110 may rest over a plurality of pylons 114 placed longitudinally.
  • the platform 110 and the plurality of pylons 114 may be made of concrete.
  • a plurality of rebars 120 may be arranged linearly within the platform 110 for providing structural reinforcement to the platform 110.
  • the plurality of pylons 114 may act as a supporting member mounted on a foundation, such as earth’s surface for providing support to the tube 204 and the platform 110.
  • the plurality of pylons 114 may be present as rectangular blocks having an arch-like structure in center for accommodating the tube 204 of circular shape.
  • the plurality of pylons 114 may carry load exerted by the platform 110, the tube 204, and other components of the vacuum transportation system 100.
  • the plurality of pylons 114 may transfer the load to the foundation.
  • the plurality of pylons 114 may be separated from each other by a third predefined distance in the longitudinal direction of the tube 204. The third predefined distance may be determined by constraints on deflection of the tube 204 and the platform 110.
  • the platform 110 may be supported by a plurality of pillars 116 present over each pylon of the plurality of pylons 114.
  • the plurality of pillars 116 may provide a vertical support embedded in each of the plurality of pylons 114.
  • the plurality of pillars 116 may be made of a material like stainless steel, Aluminium, a carbon fiber composite, and a mild steel. Tensile strength of the material may ranges from 100 MPa to 5000 MPa.
  • the plurality of pillars may withhold dynamic loads exerted by weight of the platform 110 and the objects in motion. Thus, the plurality of pillars 116 may act as a reinforcement to the plurality of pylons 114 by handling a substantial part of compressive and tensile load transferred to the plurality of pylons 114.
  • the plurality of pillars 116 may transfer the load exerted the object and the platform 110 directly to the foundation, via the plurality of pylons 114. The load exerted by the object and the platform 110 may not couple with the tube 204 as the platform 110 does not remain in contact with the tube 204.
  • the plurality of pillars 116 may ensure that there does not remain a direct contact between the plurality of pylons 114 and the platform 110.
  • the plurality of pillars 116 may further ensure a minimum contact of the plurality of pylons 114 and the platform 110 with other components of the vacuum transportation system 100. Thus, stress concentration areas generated at edges of the tube 204 may be minimized.
  • a layer of foam 118 may be present between the tube 204 and the plurality of pylons 114 for avoiding stress concentrations in the tube 204 and the plurality of pylons 114.
  • the foam 118 may be made of a soft material ensuring smooth contact between the skin 102 and the plurality of pylons 114, without causing any damage to the skin 102.
  • the track 112 may be placed longitudinally on the platform 110 for enabling movement of the objects inside the tube 204.
  • the track 112 may be present as solid channels over which the objects may travel.
  • the track 112 may be mounted on the platform 110 using bolts.
  • the platform 110 may withstand most of the dynamic loads exerted due to the object running on the track 112. Maximum stress may be generated near a bottom and a top part of the platform 110.
  • the platform 110 may be placed on the plurality of pillars 116 embedded in each pylon of the plurality of pylons 114. Thus, load exerted due to the object may be transferred directly to the foundation via the plurality of pylons 114.
  • a computer- based simulation modelling may be used.
  • An Analysis Software (ANSYS) may be used for simulating the vacuum transportation system 100.
  • ANSYS may provide a dynamic environment for analysis of models using programmed algorithms and equations and also allow the possibility of inspecting the processes running in visual 2D or 3D manner. Constant optimization of a model may be obtained by varying the design parameters like dimensions and sectioned parameters of previously mentioned components, until the model with desired performance is obtained.
  • simulation was performed entirely in ANSYS Workbench 2020 Rl. Individual components of the vacuum transportation system 100 were modelled separately through Autodesk Fusion software. The modelled components were individually meshed and finally assembled to form the vacuum transportation system 100 in the ANSYS Workbench. Adequate mesh convergence studies were performed to ensure robustness of simulation results. Material properties for various components were obtained through an ANSYS Granta module.
  • the material properties were assigned to various individual entities appropriately.
  • a half model of the vacuum transportation system 100 was considered for simulations and symmetrical boundary conditions were applied.
  • fixed boundary conditions were introduced to a pylon-ground interface.
  • a vacuum pressure difference, a load of an object, and the selfweight of the individual entities were duly considered in the simulations.
  • 2x of the static load was taken during the simulations.
  • Figs. 5A illustrates von Mises equivalent stress plot obtained during simulation of a symmetric model of the vacuum transportation system 100, in accordance with an embodiment of the present invention.
  • a maximum stress occurs in the circular region of the tube 204 from where the plurality of pillars 116 are connected.
  • Fig. 5B illustrates a factor of safety plot obtained during simulation of the vacuum transportation system 100, in accordance with an embodiment of the present invention. The simulations were performed on a half symmetric model of the vacuum transportation system 100 designed according to the present invention, using the ANSYS workbench.
  • the one or more embodiment of the present invention described above provides the technical advantages mentioned henceforth. Cost of manufacturing the vacuum transportation system designed according to present invention is reduced to almost one-fourth as compared to a vacuum transportation system designed according to conventional approach. Further, buckling of a skin is prevented and stability of a tube is ensured by different components such as formers, flanges, and longerons of a framework of the vacuum transportation system. In addition, regions with high- stress concentrations are minimized and a safety factor of the vacuum transportation system is enhanced by a foam introduced in between the skin and the pylon. Foam being the comparatively soft material ensures smooth contact with the skin without causing any damage to skin.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Power Engineering (AREA)
  • Devices Affording Protection Of Roads Or Walls For Sound Insulation (AREA)
  • Pressure Vessels And Lids Thereof (AREA)

Abstract

The present invention relates to a vacuum transportation system (100) comprising a tube (204), a platform (110), and a track (112). The tube (204) may comprise a skin (102) and a framework (202). The framework (202) may comprise formers (104), flanges (106), and longerons (108). The formers (104) may be separated from each other by a first predefined distance and positioned beneath the skin (102) in a longitudinal direction of the framework (202). The flanges (106) may be separated from each other by a second predefined distance and positioned outside the skin (102) in the longitudinal direction. The longerons (108) may connect consecutive formers with each other. The platform (110) may pass through and over a bottom area of the tube (204). The platform (110) may rest over pylons (114) placed longitudinally. The track (112) may be placed longitudinally on the platform (110) for enabling movement of objects inside the tube (204).

Description

“VACUUM TRANSPORTATION SYSTEM”
TECHNICAU FIELD
[0001] The present invention relates to the field of vacuum systems, and specifically relates to a vacuum transportation system.
BACKGROUND OF THE INVENTION
[0002] Background description includes information that may be useful in understanding the present invention. It is not an admission that any of the information provided herein is prior art or relevant to the presently claimed invention, or that any publication specifically or implicitly referenced is prior art.
[0003] Traditional transportation modes operating over water, land, rail, and air provide quick and convenient movement of persons and objects. The adverse environmental, societal, and economic impacts of these traditional modes of transportation, however, resulted into the need to find alternative modes of transportation that take advantage of the significant improvements in transportation technology, so as to efficiently move objects and persons between locations.
[0004] High-speed transportation systems such as aircrafts have been contemplated for reducing overall time for commuting between places. However, such transportation systems contribute to enormous greenhouse gas emissions. Thus, traditional transportation systems are responsible for major share of environmental pollution. One way to reduce the environmental pollution caused through the aircrafts without compromising the performance, is by using a highspeed vacuum transportation system for travelling.
[0005] A high-speed vacuum transportation system requires a continuous tube infrastructure that is maintained at low pressures. The high-speed vacuum transportation system has support structures that enable hyperloop pods/maglev vacuum trains to run at extremely high speeds. The tube has to be robust, stiff, capable of holding vacuum, and long-lasting. The tube needs to be thick for resisting loads acting on the tube from different sources. An overall weight of the tube and a cost of manufacturing of the tube is increased due to increase in thickness of the tube. Since the tube is a major part of the vacuum transportation system, it is vital to decrease the cost of manufacturing of the tube.
[0006] There is therefore a need to develop a vacuum transportation system capable of allowing high-speed transportation while optimizing cost without compromising overall performance of the vacuum transportation system.
OBJECTS OF THE INVENTION
[0007] It is an object of the present invention to provide a vacuum transportation system capable of allowing high-speed transportation while optimizing cost without compromising overall performance of the vacuum transportation system.
[0008] It is another object of the present invention to provide a vacuum transportation system manufactured seamlessly without requiring an advanced manufacturing machinery.
[0009] Still another object of the present invention to reduce an overall weight of the vacuum transportation system.
SUMMARY OF THE INVENTION
[00010] The summary is provided to introduce aspects related to a vacuum transportation system, and the aspects are further described below in the detailed description. This summary is not intended to identify essential features of the claimed subject matter nor is it intended for use in determining or limiting the scope of the claimed subject matter. [00011] The present invention relates to a vacuum transportation system, for instance, for transportation of people and/or materials from one place to another. In one embodiment, the vacuum transportation system may include a tube, a platform, and a track. The tube may hold a vacuum within. The tube may comprise a skin and a framework. The skin may be made of a metallic sheet and may resist load acting on the tube from one or more sources. The one or more sources may comprise at least one of the vacuum inside the tube, wind outside the tube, and weight of the object moving inside the tube. The framework may provide support to the skin. The framework may comprise a plurality of formers, a plurality of flanges, and a plurality of longerons. The plurality of formers may be separated from each other by a first predefined distance and positioned beneath the skin in a longitudinal direction of the tube. The plurality of flanges may be separated from each other by a second predefined distance and positioned outside the skin in the longitudinal direction of the tube. The plurality of longerons may connect consecutive formers of the plurality of formers with each other. The platform may pass through and over a bottom area of the tube. The platform may rest over a plurality of pylons placed longitudinally. The track may be placed longitudinally on the platform. The track may enable movement of objects inside the tube.
[00012] In an aspect, the plurality of formers, the plurality of flanges, and the plurality of longerons may be made of one or more of stainless steel, aluminium, carbon fiber composite, and mild steel.
[00013] In an aspect, a layer of foam may be present between the tube and the plurality of pylons. The plurality of pylons may be separated by a third predefined distance in the longitudinal direction of the tube. The platform may be supported by a plurality of pillars over each pylon of the plurality of pylons for transferring loads of the objects moving inside the tube (204) to ground.
[00014] In an aspect, one or more vacuum pumps may be connected with the tube to maintain the vacuum. The platform and the plurality of pylons may be made of concrete. A plurality of rebars may arranged linearly within the platform for providing structural reinforcement to the platform.
[00015] Other aspects and advantages of the invention will become apparent from the following description, taken in conjunction with the accompanying drawings, illustrating by way of example the principles of the invention.
BRIEF DESCRIPTION OF ACCOMPANYING DRAWINGS
[00016] The accompanying drawings constitute a part of the description and are used to provide further understanding of the present invention. Such accompanying drawings illustrate the embodiments of the present invention which are used to describe the principles of the present invention. In the figures, similar components and/or features may have the same reference label. Further, various components of the same type may be distinguished by following the reference label with a second label that distinguishes among the similar components. If only the first reference label is used in the specification, the description is applicable to any one of the similar components having the same first reference label irrespective of the second reference label.
[00017] The embodiments are illustrated by way of example and not by way of limitation in the figures of the accompanying drawings in which like references indicate similar elements. It should be noted that references to “an” or “one” embodiment in this invention are not necessarily to the same embodiment, and they mean at least one. In the drawings:
[00018] Fig. 1 illustrates a perspective front view of a vacuum transportation system, in accordance with an embodiment of the present invention;
[00019] Fig. 2A illustrates a perspective side view of a framework of the vacuum transportation system, in accordance with an embodiment of the present invention; [00020] Fig. 2B illustrates a perspective side view of a tube of the vacuum transportation system, in accordance with an embodiment of the present invention;
[00021] Fig. 3 illustrates a perspective front view of the tube, in accordance with an embodiment of the present invention;
[00022] Fig. 4 illustrates an exemplary perspective view of the platform of the vacuum transportation system, in accordance with an embodiment of the present invention;
[00023] Fig. 5A illustrates von Mises equivalent stress plot obtained during simulation of a symmetric model of the vacuum transportation system, in accordance with an embodiment of the present invention; and
[00024] Fig. 5B illustrates a factor of safety plot obtained during simulation of the vacuum transportation system, in accordance with an embodiment of the present invention.
DETAILED DESCRIPTION OF THE INVENTION
[00025] The detailed description set forth below in connection with the appended drawings is intended as a description of various embodiments of the present invention and is not intended to represent the only embodiments in which the present invention may be practiced. Each embodiment described in this disclosure is provided merely as an example or illustration of the present invention, and should not necessarily be construed as preferred or advantageous over other embodiments. The detailed description includes specific details for the purpose of providing a thorough understanding of the present invention. However, it will be apparent to those skilled in the art that the present invention may be practiced without these specific details. [00026] As used in the description herein and throughout the claims that follow, the meaning of “a,” “an,” and “the” includes plural reference unless the context clearly dictates otherwise. Also, as used in the description herein, the meaning of “in” includes “in” and “on” unless the context clearly dictates otherwise.
[00027] If the specification states a component or feature “may”, “can”, “could”, or “might” be included or have a characteristic, that particular component or feature is not required to be included or have the characteristic.
[00028] The present invention relates to a vacuum transportation system for high-speed transportation of people and/or objects. Fig. 1 illustrates a perspective front view of a vacuum transportation system 100, in accordance with an embodiment of the present invention. The vacuum transportation system 100 may include a skin 102, a plurality of formers 104, a plurality of flanges 106, a plurality of longerons 108, a platform 110, and a track 112. The plurality of formers 104, the plurality of flanges 106, and the plurality of longerons 108 may contribute to a framework of the vacuum transportation system 100. A structure of the framework has been described successively with reference to Fig. 2A.
[00029] Fig. 2A illustrates a perspective side view of a framework 202 of the vacuum transportation system 100, in accordance with an embodiment of the present invention. The framework 202 may include stiffeners, such as the plurality of formers 104, the plurality of flanges 106, and the plurality of longerons 108. The plurality of formers 104 may be used as circular stiffeners separated from each other by a first predefined distance in a longitudinal direction of the framework 202. The plurality of flanges 106 may be used as circular stiffeners separated from each other by a second predefined distance in the longitudinal direction of the framework 200. The first predefined distance and the second predefined distance may be determined on the basis of buckling of the plurality of longerons 108, a manufacturing method for the platform 110, requirements to maintain a leak proof environment, and a total cost of manufacturing of the vacuum transportation system 100.
[00030] The plurality of longerons 108 may connect consecutive formers of the plurality of formers 104 with each other. In one implementation, a longeron may be welded with two consecutive formers. The plurality of formers 104, the plurality of flanges 106, and the plurality of longerons 108 may be made of a material like stainless steel, aluminium, carbon fiber composite, and mild steel. Tensile strength of the material may range from 100 MPa to 5000 MPa.
[00031] The framework 202 may provide a lightweight and safe supportive assembly for positioning the skin 102, to form a tube. Fig. 2B illustrates a perspective side view of a tube 204 of the vacuum transportation system 100, in accordance with an embodiment of the present invention. The plurality of formers 104 may be positioned beneath the skin 102 and the plurality of flanges 106 may be positioned outside the skin 102, as shown in Fig. 3 illustrating a perspective front view of the tube 204. As illustrated in Fig. 3, the skin 102 may be held between the plurality of formers 104 and the plurality of flanges 106. In such manner, the skin 102 may be supported from inside and outside by the plurality of formers 104 and the plurality of flanges 106 respectively. Thus, buckling of the skin 102 may be prevented and stability of the tube 204 may be ensured by the plurality of formers 104 and the plurality of flanges 106. In one implementation, the plurality of formers 104 and the plurality of flanges 106 may be present at same location in the longitudinal direction of the framework 200, and thus the first predefined distance may be equal to the second predefined distance. In another implementation, the plurality of formers 104 and the plurality of flanges 106 may be present at different locations in the longitudinal direction of the framework 200, and thus the first predefined distance may not be equal to the second predefined distance.
[00032] The tube 204 may hold a vacuum within. A shape of the tube 204 may be defined by a shape of the framework 202. Importantly, the shape of the tube 204 may be designed based on operational requirements. In one implementation, the tube 204 may be present in a circular shape. In other implementations, the tube 204 may be present in other shapes, such as rectangle, square, and hexagon.
[00033] The skin 102 may be made of a high strength material, such as a metallic material. The skin 102 may resist load acting on the tube 204 from one or more sources. The one or more sources may comprise at least one of the vacuum inside the tube 204, wind outside the tube 204, and weight of an object moving inside the tube 204. Examples of the object may include, but not limited to, hyperloop pods, maglev trains, or any other vehicle capable of travelling through the vacuum transportation system 100.
[00034] Fig. 4 illustrates an exemplary perspective view of the platform 110 of the vacuum transportation system 100, in accordance with an embodiment of the present invention. The platform 110 may rest over a plurality of pylons 114 placed longitudinally. The platform 110 and the plurality of pylons 114 may be made of concrete. A plurality of rebars 120 may be arranged linearly within the platform 110 for providing structural reinforcement to the platform 110. The plurality of pylons 114 may act as a supporting member mounted on a foundation, such as earth’s surface for providing support to the tube 204 and the platform 110. The plurality of pylons 114 may be present as rectangular blocks having an arch-like structure in center for accommodating the tube 204 of circular shape.
[00035] The plurality of pylons 114 may carry load exerted by the platform 110, the tube 204, and other components of the vacuum transportation system 100. The plurality of pylons 114 may transfer the load to the foundation. The plurality of pylons 114 may be separated from each other by a third predefined distance in the longitudinal direction of the tube 204. The third predefined distance may be determined by constraints on deflection of the tube 204 and the platform 110. [00036] The platform 110 may be supported by a plurality of pillars 116 present over each pylon of the plurality of pylons 114. The plurality of pillars 116 may provide a vertical support embedded in each of the plurality of pylons 114. In one implementation, the plurality of pillars 116 may be made of a material like stainless steel, Aluminium, a carbon fiber composite, and a mild steel. Tensile strength of the material may ranges from 100 MPa to 5000 MPa. The plurality of pillars may withhold dynamic loads exerted by weight of the platform 110 and the objects in motion. Thus, the plurality of pillars 116 may act as a reinforcement to the plurality of pylons 114 by handling a substantial part of compressive and tensile load transferred to the plurality of pylons 114. The plurality of pillars 116 may transfer the load exerted the object and the platform 110 directly to the foundation, via the plurality of pylons 114. The load exerted by the object and the platform 110 may not couple with the tube 204 as the platform 110 does not remain in contact with the tube 204.
[00037] The plurality of pillars 116 may ensure that there does not remain a direct contact between the plurality of pylons 114 and the platform 110. The plurality of pillars 116 may further ensure a minimum contact of the plurality of pylons 114 and the platform 110 with other components of the vacuum transportation system 100. Thus, stress concentration areas generated at edges of the tube 204 may be minimized.
[00038] Referring back to Fig. 1, a layer of foam 118 may be present between the tube 204 and the plurality of pylons 114 for avoiding stress concentrations in the tube 204 and the plurality of pylons 114. The foam 118 may be made of a soft material ensuring smooth contact between the skin 102 and the plurality of pylons 114, without causing any damage to the skin 102.
[00039] The track 112 may be placed longitudinally on the platform 110 for enabling movement of the objects inside the tube 204. In one implementation, the track 112 may be present as solid channels over which the objects may travel. The track 112 may be mounted on the platform 110 using bolts. The platform 110 may withstand most of the dynamic loads exerted due to the object running on the track 112. Maximum stress may be generated near a bottom and a top part of the platform 110. The platform 110 may be placed on the plurality of pillars 116 embedded in each pylon of the plurality of pylons 114. Thus, load exerted due to the object may be transferred directly to the foundation via the plurality of pylons 114.
[00040] For validating performance of the vacuum transportation system 100 designed according to one of the embodiments of the present invention, a computer- based simulation modelling may be used. An Analysis Software (ANSYS) may be used for simulating the vacuum transportation system 100. ANSYS may provide a dynamic environment for analysis of models using programmed algorithms and equations and also allow the possibility of inspecting the processes running in visual 2D or 3D manner. Constant optimization of a model may be obtained by varying the design parameters like dimensions and sectioned parameters of previously mentioned components, until the model with desired performance is obtained.
[00041] In one scenario, simulation was performed entirely in ANSYS Workbench 2020 Rl. Individual components of the vacuum transportation system 100 were modelled separately through Autodesk Fusion software. The modelled components were individually meshed and finally assembled to form the vacuum transportation system 100 in the ANSYS Workbench. Adequate mesh convergence studies were performed to ensure robustness of simulation results. Material properties for various components were obtained through an ANSYS Granta module.
[00042] Further, the material properties were assigned to various individual entities appropriately. To optimize computational cost and efforts, a half model of the vacuum transportation system 100 was considered for simulations and symmetrical boundary conditions were applied. In addition to the symmetrical boundary conditions, fixed boundary conditions were introduced to a pylon-ground interface. Further, a vacuum pressure difference, a load of an object, and the selfweight of the individual entities were duly considered in the simulations. For accounting dynamic moving loads, 2x of the static load was taken during the simulations.
[00043] Figs. 5A illustrates von Mises equivalent stress plot obtained during simulation of a symmetric model of the vacuum transportation system 100, in accordance with an embodiment of the present invention. As illustrated in Fig. 5A, a maximum stress occurs in the circular region of the tube 204 from where the plurality of pillars 116 are connected. Fig. 5B illustrates a factor of safety plot obtained during simulation of the vacuum transportation system 100, in accordance with an embodiment of the present invention. The simulations were performed on a half symmetric model of the vacuum transportation system 100 designed according to the present invention, using the ANSYS workbench.
[00044] The one or more embodiment of the present invention described above provides the technical advantages mentioned henceforth. Cost of manufacturing the vacuum transportation system designed according to present invention is reduced to almost one-fourth as compared to a vacuum transportation system designed according to conventional approach. Further, buckling of a skin is prevented and stability of a tube is ensured by different components such as formers, flanges, and longerons of a framework of the vacuum transportation system. In addition, regions with high- stress concentrations are minimized and a safety factor of the vacuum transportation system is enhanced by a foam introduced in between the skin and the pylon. Foam being the comparatively soft material ensures smooth contact with the skin without causing any damage to skin. Load exerted by an object travelling through a platform of the vacuum transportation system is not coupled with the tube as the platform does not remain in contact with the tube. A skin of the tube does not carry the load exerted by the object and leads to reduction in thickness of the skin. [00045] Although a form of the invention has been described herein, it will be obvious to those skilled in the art that variations may be made in the construction and relation of parts and method without departing from the spirit and scope of the invention described herein. While embodiments of the present disclosure have been illustrated and described, it will be clear that the disclosure is not limited to these embodiments only. Numerous modifications, changes, variations, substitutions, and equivalents will be apparent to those skilled in the art, without departing from the scope of the disclosure.

Claims

CLAIMS:
1. A vacuum transportation system (100) comprising: a tube (204) for holding a vacuum within, the tube (204) comprising: a skin (102) for resisting load acting on the tube (204) from one or more sources; and a framework (202) for providing support to the skin (102), the framework (202) comprising: a plurality of formers (104) separated from each other by a first predefined distance and positioned beneath the skin (102) in a longitudinal direction of the framework (202); a plurality of flanges (106) separated from each other by a second predefined distance and positioned outside the skin (102) in the longitudinal direction of the framework (202); and a plurality of longerons (108) for connecting consecutive formers of the plurality of formers (104) with each other; a platform (110) passing through and over a bottom area of the tube (204), wherein the platform (110) rests over a plurality of pylons (114) placed longitudinally; and a track (112) placed longitudinally on the platform (110) for enabling movement of objects inside the tube (204).
2. The vacuum transportation system (100) as claimed in claim 1, wherein the skin (102) is made of a metallic sheet.
3. The vacuum transportation system (100) as claimed in claim 1, wherein the one or more sources comprise at least one of the vacuum inside the tube (102), wind outside the tube (102), and weight of the object moving inside the tube (102).
4. The vacuum transportation system (100) as claimed in claim 1, wherein the plurality of formers (104), the plurality of flanges (106), and the plurality of longerons are made of one or more of stainless steel, aluminium, carbon fiber composite, and mild steel. The vacuum transportation system (100) as claimed in claim 1, wherein a layer of foam is present between the tube (102) and the plurality of pylons (114). The vacuum transportation system (100) as claimed in claim 1, wherein the plurality of pylons (114) are separated by a third predefined distance in the longitudinal direction of the framework (202). The vacuum transportation system (100) as claimed in claim 1, wherein the platform (110) is supported by a plurality of pillars (116) over each pylon of the plurality of pylons (114) for transferring loads of the objects moving inside the tube (204) to ground. The vacuum transportation system (100) as claimed in claim 1, wherein one or more vacuum pumps are connected with the tube (102) to maintain the vacuum. The vacuum transportation system (100) as claimed in claim 1, wherein the platform (110) and the plurality of pylons (114) are made of concrete. The vacuum transportation system (100) as claimed in claim 1, wherein a plurality of rebars (120) are arranged linearly within the platform (110) for providing structural reinforcement to the platform (110).
EP22869559.9A 2021-09-20 2022-09-16 VACUUM TRANSPORT SYSTEM Pending EP4405225A4 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IN202141042501 2021-09-20
PCT/IN2022/050829 WO2023042223A1 (en) 2021-09-20 2022-09-16 Vacuum transportation system

Publications (2)

Publication Number Publication Date
EP4405225A1 true EP4405225A1 (en) 2024-07-31
EP4405225A4 EP4405225A4 (en) 2025-08-13

Family

ID=85602555

Family Applications (1)

Application Number Title Priority Date Filing Date
EP22869559.9A Pending EP4405225A4 (en) 2021-09-20 2022-09-16 VACUUM TRANSPORT SYSTEM

Country Status (4)

Country Link
EP (1) EP4405225A4 (en)
AU (1) AU2022346281A1 (en)
CA (1) CA3232337A1 (en)
WO (1) WO2023042223A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT202300028350A1 (en) * 2023-12-29 2025-06-29 Aeronautical Service S R L PIPE FOR HIGH-SPEED TRANSPORT OF GOODS AND PASSENGERS IN A LOW-PRESSURE ENVIRONMENT AND PROCEDURE FOR ITS CONSTRUCTION

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
YU47775B (en) * 1990-07-23 1996-01-09 Savićević, Milorad TRANSPORT SYSTEM WITH AT LEAST TWO BOTTOM POINTS DISTRIBUTED ON OVERHAUL SIDE OF INTERRUPTED RINGS
CN105253150A (en) * 2014-07-16 2016-01-20 征先管联运输科技研究院(北京)有限公司 Transportation pipeline for pipe traffic system
US9566987B2 (en) * 2015-02-08 2017-02-14 Hyperloop Technologies, Inc. Low-pressure environment structures
WO2020249677A1 (en) * 2019-06-13 2020-12-17 Tata Steel Nederland Technology B.V. Double walled tube segment and method for producing said tube segment
CN114423665B (en) * 2019-09-18 2024-09-27 塔塔钢铁荷兰科技有限责任公司 Tube sections for evacuated tube transport systems

Also Published As

Publication number Publication date
AU2022346281A1 (en) 2024-04-04
EP4405225A4 (en) 2025-08-13
CA3232337A1 (en) 2023-03-23
WO2023042223A1 (en) 2023-03-23

Similar Documents

Publication Publication Date Title
EP4405225A1 (en) Vacuum transportation system
CN114919710B (en) A grid-type box floating raft structure and design method thereof
CN103866890B (en) Space ultra-large type opening-closing type roof system rail system and design thereof, mounting method
CN107697080A (en) A kind of vacuum high-speed transit pipeline
CN105667836B (en) A kind of satellite pole structure
CN201922912U (en) Electric pile mounting support for cars adopting hydrogen fuel cells
CN210943151U (en) Oil tank floating roof unit
CN114955015B (en) Mars exploration landing platform structure with complex and heavy loads
CN112441256A (en) System and method for testing structural strength of bottom of seaplane
US20250154735A1 (en) Method for erecting a transportation structure
US20250188691A1 (en) Method for erecting a transportation structure
CN104878856B (en) The laminated steel plate coupling beam and its construction method being placed in building structure between shear wall
CN114239368B (en) Angle section optimization design method in typical airtight top plate connection
CN114139422B (en) Optimal design method for wing spar of central wing box made of composite material
US20250163657A1 (en) Method for erecting a transportation structure
CN205168510U (en) Roof structure and train
CN215405664U (en) Anti-destabilization supporting device of SPMT module vehicle
CN110469721A (en) A kind of assembled anti-knock suspension and support
CN109778606B (en) Large-span combined bridge structure of straddle type monorail and setting method of large-span combined bridge structure in curve section
CN219468008U (en) Air-tight floor mounting structure of embedded seat slide rail
CN208545777U (en) A vibration isolation device
Awall et al. Improvement effects of bottom lateral bracings on dynamic performance of curved steel twin I-girder bridges under running vehicles
CN218726004U (en) Packing box strength test anchor clamps
CN223856447U (en) A composite reinforced curved wall panel support device
CN105887651B (en) A kind of arch hexagon steel box-girder preparation method

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20240319

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
REG Reference to a national code

Ref country code: DE

Ref legal event code: R079

Free format text: PREVIOUS MAIN CLASS: B61B0013080000

Ipc: B61B0013100000

A4 Supplementary search report drawn up and despatched

Effective date: 20250710

RIC1 Information provided on ipc code assigned before grant

Ipc: B61B 13/10 20060101AFI20250704BHEP

Ipc: B60L 13/04 20060101ALI20250704BHEP

Ipc: F16L 9/18 20060101ALI20250704BHEP

Ipc: B21C 37/00 20060101ALI20250704BHEP