WO2013040847A1 - Through-flow air suspension platform - Google Patents
Through-flow air suspension platform Download PDFInfo
- Publication number
- WO2013040847A1 WO2013040847A1 PCT/CN2012/000852 CN2012000852W WO2013040847A1 WO 2013040847 A1 WO2013040847 A1 WO 2013040847A1 CN 2012000852 W CN2012000852 W CN 2012000852W WO 2013040847 A1 WO2013040847 A1 WO 2013040847A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- cross
- flow
- fan
- suspension platform
- air suspension
- Prior art date
Links
- 239000000725 suspension Substances 0.000 title claims abstract description 75
- 230000005540 biological transmission Effects 0.000 claims description 9
- 241000886569 Cyprogenia stegaria Species 0.000 abstract description 3
- 238000010276 construction Methods 0.000 abstract description 3
- 238000007599 discharging Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 3
- FGRBYDKOBBBPOI-UHFFFAOYSA-N 10,10-dioxo-2-[4-(N-phenylanilino)phenyl]thioxanthen-9-one Chemical compound O=C1c2ccccc2S(=O)(=O)c2ccc(cc12)-c1ccc(cc1)N(c1ccccc1)c1ccccc1 FGRBYDKOBBBPOI-UHFFFAOYSA-N 0.000 description 1
- 241001465754 Metazoa Species 0.000 description 1
- 230000004323 axial length Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/16—Combinations of two or more pumps ; Producing two or more separate gas flows
- F04D25/166—Combinations of two or more pumps ; Producing two or more separate gas flows using fans
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/02—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
- F04D17/04—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal of transverse-flow type
Definitions
- the invention belongs to the field of flying devices, and in particular relates to a cross flow air suspension platform.
- the above four methods are capable of achieving vertical takeoff and landing and air hovering, but they cannot be effectively applied to flying cars and urban traffic due to both principle and structural problems. Let's take a look at their shortcomings in this respect: A: Jet: The temperature of the jet is too high, the noise is very large and the energy consumption is huge. The above disadvantages can be seen from the British fighter jets.
- Flapping Wing Many animals have the first to develop a perfect flight structure, and it carries the original dream of human flight, but for thousands of years people have not developed it to carry people to fly, but also because of structural constraints If you need to carry people, then the wings will be too large to fly freely in the city.
- Hot air balloon and airship type aircraft Although it can achieve smooth take-off and landing, its volume is even more amazing. It is impossible to walk through small city streets, and it is difficult to adapt to urban life due to slow take-off and landing. Rapid and efficient requirements.
- the present invention provides a cross-flow air suspension platform, which can solve the difficulties encountered by the foregoing four methods in urban flight traffic in a completely new way, and realizes the built-in thrust suspension device. And miniaturization and flattening, the most important thing is that it replaces the chassis driving system of the car and the huge propeller take-off and landing mechanism of the helicopter in a completely new way. It can be said that it is the hovering and taking off and landing of the future helicopter and flying vehicle foundation. Device.
- the invention adopts a structure formed by a cross-flow fan and an engine, and the force is used for mutual use, and the principle of the force and the reaction force is utilized, and the counter-thrust obtained by the cross-flow fan to promote the one-way flow of the air is fully utilized, and the platform is realized in the air. Suspended flight device.
- the impeller and the outer casing of the cross-flow fan form a structure in which the air moves in one direction, and the impeller of the cross-flow fan rotates at a high speed under the driving of the engine.
- the impeller rotates at a high speed
- the air is sucked by the impeller, and a thrust is given to the air, and the air is supplied to the impeller.
- the force is applied, the air also gives the impeller a counter force to give the fan a lift.
- the impeller and the engine shaft are arranged in parallel, and can also be installed at right angles through the transmission mechanism and the engine shaft.
- the cross flow fan is also called a cross flow fan, and the impeller is multi-leaf type, long cylindrical shape, and has a forward multi-wing blade.
- the airflow enters the cascade from the open end of the impeller, passes through the interior of the impeller, and is discharged into the volute from the other side of the cascade to form a working airflow.
- the flow of the airflow in the impeller is complex, the velocity field of the airflow is unsteady, and there is a vortex in the impeller, centered near the volute tongue.
- the existence of the vortex causes a circulating flow at the output end of the impeller. Outside the vortex, the flow line of the airflow in the impeller is arc-shaped. Therefore, the flow velocity at each point on the outer circumference of the impeller is inconsistent. The closer to the vortex core, the greater the velocity, and the closer to the volute, the smaller the velocity.
- the airflow speed and pressure at the fan outlet are not uniform, so the flow coefficient and pressure coefficient of the fan are average.
- the position of the vortex has a great influence on the performance of the cross-flow fan.
- the center of the vortex is close to the inner circumference of the impeller and close to the volute tongue.
- the performance of the fan is better.
- the cross-flow fan is mainly composed of three parts: impeller, air duct and electric motor. It has the following characteristics:
- the axial length is not limited, and the length of the impeller can be arbitrarily selected according to different use requirements;
- the cross flow air suspension platform is characterized in that it comprises at least two cross flow fans, the cross flow fans are disposed in the same plane, and the cross flow fan comprises a cylindrical fan shell, a fan The opposite sides of the shell are respectively provided with an air inlet and an air outlet, and the air outlet is arranged downward, and the fan shaft of the cross flow fan is connected with the rotating shaft of the engine.
- the cross-flow air suspension platform is characterized in that the air inlet and the air outlet of the fan casing are strip-shaped ports which are disposed along the longitudinal direction of the fan casing cylinder and have the same length as the cylinder.
- the tubular air suspension platform is characterized in that the width of the air inlet is wider than the width of the air outlet.
- the cross-flow air suspension platform is characterized in that the width of the air inlet is three times the width of the air outlet.
- the cross-flow air suspension platform is characterized in that a fan-shaped fan impeller is arranged in the fan casing, and the fan impeller is composed of strip-shaped blades arranged along the length of the cylinder and having the same length as the cylinder The strip blade is disposed obliquely to the circumferential section of the cylinder.
- the tubular air suspension platform is characterized in that the strip blades are disposed at an angle of 45° to the circumferential section of the cylinder.
- the cross-flow air suspension platform is characterized in that: two rotating shafts are respectively arranged on the two sides of the engine, the rotating shafts are respectively connected with one driving shaft, and the main bevel gears are symmetrically arranged on the driving shafts, and each main cone Two cross-flow fans are respectively arranged on both sides of the gear, the fan shaft of the cross-flow fan is vertically arranged with the transmission shaft, the auxiliary bevel gear is arranged on the fan shaft, and the main bevel gear and the auxiliary bevel gear are vertically meshed with each other.
- the tubular air suspension platform is characterized in that the cross flow fan is disposed between two mutually parallel side beams, and the engine is staggered outside the side beams.
- the cross-flow air suspension platform is characterized in that it comprises an outer ring and a support plate, the support plate is arranged at the center of the outer ring, the engine is arranged on the support plate, and the fan shaft on one side of the cross flow fan is connected with the engine shaft.
- the other side of the cross-flow fan is connected to the outer ring, and the engine and the cross-flow fan are symmetrically arranged in the outer ring.
- the cross-flow air suspension platform is characterized in that a cross-flow fan disposed parallel to or perpendicular to the cross-flow air suspension platform and disposed downstream of the air outlet is disposed on the rear side of the cross-flow air suspension platform.
- the left and right sides of the flow air suspension platform are respectively connected with a cross flow fan which is perpendicular to the cross flow air suspension platform and which is arranged forwardly from the air outlet.
- the fan shaft of the cross flow fan is connected with the rotating shaft of the engine.
- the cross-flow air suspension platform is characterized in that it comprises an outer frame, a cross-flow fan of a pair of shared engines is laterally disposed on the upper and lower sides of the outer frame, and a pair of shared engines are vertically disposed inside the outer frame Flow fan.
- the cross-flow air suspension platform is characterized in that it comprises an inner frame, an outer frame is arranged around the inner frame, a cross-flow fan is arranged in the outer frame, and the cross-flow fan is clockwise or reverse In the hour hand arrangement, the fan shaft of the cross flow fan is connected to the rotating shaft of the engine.
- the cross-flow air suspension platform is characterized in that a set of fixing plates are fixedly arranged in the inner frame.
- the cross-flow air suspension platform is characterized in that: an outer frame is arranged, and a cross-flow fan is fixedly disposed on four circumferential corners of the outer frame, and the fan shaft of the cross-flow fan is connected to the gearbox, The engine is connected to the gearbox.
- the tubular air suspension platform is characterized in that a steering gear is connected to the cross flow fan.
- the tubular air suspension platform is characterized in that the gearbox and the engine are provided with a control port for connecting an external control system.
- the function and effect of the invention 1. It can make the real flying car appear, and the life of most helicopters and a part of the car; 2. Realize the rapid traffic in the huge area and volume city in the future; 3. Reduce the urban road construction And the construction of peripheral highways to maximize the protection of the land to protect the natural environment; 4.
- the flight device has an emergency fault in the air, because of its small structure and no external high-speed rotating device, it can use the parachute to land when the high altitude fails.
- the entire aircraft can be protected by a honeycomb airbag, thereby maximizing the safety of the internal passengers, and avoiding the fact that the existing aircraft is in flight or not, and the vast majority of the survivors have no terrible situation, in special circumstances.
- It can also be used for aerodynamic suspension stretchers in the battle of rugged mountains to transport combat wounded, and can also be applied to high-efficiency transport of small quantities of battlefield materials and supplies in the field.
- FIG. 1 is a schematic structural view of a cross flow fan of a cross flow air suspension platform of the present invention
- FIG. 2 is a schematic structural view of a first embodiment of a through-flow air suspension platform of the present invention
- FIG. 3 is a schematic structural view of a second embodiment of a tubular air suspension platform of the present invention
- FIG. 5 is a schematic structural view of a third embodiment of a through-flow air suspension platform
- FIG. 5 is a schematic structural view of a set forward and brake power device of the tubular air suspension platform of the present invention
- FIG. 6 is a schematic structural view of a fourth embodiment of the throughflow air suspension platform of the present invention
- FIG. 7 is a schematic structural view of a fifth embodiment of the throughflow air suspension platform of the present invention
- Figure 9 is a schematic structural view of a seventh embodiment of the through-flow air suspension platform of the present invention
- Figure 10 is a schematic structural view of an eighth embodiment of the tubular air suspension platform of the present invention
- 2 fan shell
- 3 fan impeller
- 4 consistent flow fan 5
- 6 one support plate
- 7 side beam
- 8 main bevel gear
- 9 one transmission shaft
- 10-outer frame Inner frame
- 12- fixed plate 13-transmission; 14-rudder; 15-control port.
- the basic assembly of the tubular air suspension platform of the present invention is a cross flow fan 4 connected to an engine 1.
- the cross flow fan 4 comprises a cylindrical fan casing 2, and two opposite sides of the fan casing 2 are respectively provided with strip-shaped air inlets and outlets of the same length as the cylinder along the length of the cylinder casing 2 At the tuyere, the width of the air inlet is wider than the air outlet, which is roughly three times the width of the air outlet, and the air outlet is facing downward.
- the fan casing 2 is provided with a cylindrical fan impeller 3, and the fan impeller 3 is composed of strip-shaped blades provided along the length of the cylinder and having the same length as the cylinder, and the strip-shaped blades are inclined with respect to the circumferential section of the cylinder. It is approximately at an angle of 45° to the circumferential section of the cylinder.
- the fan shaft of the cross flow fan 4 is connected to the shaft of the engine 1.
- a rotating shaft is respectively arranged on both sides of the engine 1, and each of the rotating shafts is connected with a transmission shaft 9, and the main bevel gear is symmetrically arranged on the transmission shaft 9 respectively.
- Two cross-flow fans 4 are respectively disposed on two sides of each main bevel gear 8.
- the fan shaft of the cross-flow fan 4 is vertically disposed with the transmission shaft 9, and the auxiliary bevel gear, the main bevel gear 8 and the auxiliary bevel gear are disposed on the fan shaft. Vertically meshed with each other.
- the number of bevel gears and cross-flow fan 4 can be set as needed. As shown in Fig.
- each main drive shaft 9 is provided with four main bevel gears 8, each of which has two cross-flow fans respectively. 4 connections, a total of 8 cross-flow fans 4.
- the engine 1 in the middle works to drive the drive shaft. 9 rotation, the drive shaft 9 drives the main bevel gear 8 to rotate, the main bevel gear 8 drives the auxiliary bevel gear to rotate, thereby driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, and discharging from the lower air outlet.
- Give the air a thrust, and the air also gives the platform a counter-force to allow the platform to gain a lift and float in the air.
- the engine suspension below the platform. This type of platform is generally suitable for use in flying cars and can be used to replace the chassis of an ordinary car to suspend the car in the air.
- a second embodiment of the tubular air suspension platform of the present invention is provided.
- the cross flow fan 4 of the platform is disposed between two mutually parallel side beams 7, and the engine 1 is staggered outside the side beam 7.
- the fan shaft of each cross flow fan 4 is connected to the rotating shaft of one engine 1.
- the number of cross-flow fan 4 and the corresponding engine 1 can be set as required.
- four cross-flow fans 4 are arranged in the middle of the side beam 7, and four engines 1 are staggered on the outer side of the side beam 7.
- the engine 1 works, driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, discharging from the lower air outlet, giving the air a thrust, and the air also giving the platform a counteracting force to make the platform Get a lift and float in the air.
- This platform can be used in a flying car, instead of the chassis of an ordinary car, so that the car can be suspended in the air, or a stretcher plate can be placed on it for a pneumatic suspension stretcher.
- the platform includes an outer ring 5 and a support plate 6.
- the support plate 6 is disposed at the center of the outer ring 5, and the engine 1 is disposed at
- the fan shaft on the side of the cross flow fan 4 is connected to the shaft of the engine 1, and the other side of the cross flow fan 4 is connected to the outer ring 5, and the engine 1 and the cross flow fan 4 are symmetrically arranged in the outer ring 5.
- the number of the cross flow fan 4 and the engine 1 can be set as needed. In Fig.
- the support plate 6 is square, and an engine 1 is disposed in the middle of the four sides of the square, and each of the engines 1 is connected to a cross flow fan 4 , A total of 4 cross-flow fans 4, the outer ring is divided into 4 equal parts.
- the engine 1 works, driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, discharging from the lower air outlet, giving the air a thrust, and the air also giving the platform a counter force to make the platform Get a lift and float in the air. This platform is suitable for use in new round aircraft.
- the through-flow air suspension platform of the present invention can be provided with a power device for forward and brake, and the power device for forward and brake is also composed of a cross flow fan 4, which is connected at the rear side of the cross flow air suspension platform.
- the cross-flow fan 4 disposed parallel to or perpendicular to the cross-flow air suspension platform and disposed at the left and right sides of the cross-flow air suspension platform is disposed perpendicular to the cross-flow air suspension platform.
- the cross flow fan 4 provided with the tuyere forward, and the fan shaft of the cross flow fan 4 is connected to the rotating shaft of the engine 1.
- the engine 1 drives the fan shaft of the cross-flow fan 4 on the rear side to rotate, sucking air from the front air inlet, discharging it from the rear air outlet, giving the air a thrust, and the air also gives the platform a counter force.
- the engine works to drive the fan shaft of the cross-flow fan 4 on the left and right sides to rotate, and the air is sucked from the rear air inlet, and is discharged from the front air outlet to give the air a thrust, and the air also gives the platform a reverse Acting to reduce the speed of the platform forward until it stops.
- This forward and brake power unit can be mounted on a variety of cross-flow air suspension platforms for propelling and braking the platform.
- FIG. 6 is a fourth embodiment of the through-flow air suspension platform of the present invention.
- the platform includes an outer frame 10 of a rectangular structure, and a cross-flow fan 4 of the shared engine 1 is laterally disposed on the upper and lower sides of the outer frame 10, A pair of cross-flow fans 4 sharing the engine 1 are longitudinally disposed inside the outer frame 10, and preferably four pairs of cross-flow fans 4 are longitudinally disposed inside the outer frame 10, and each pair of cross-flow fans 4 shares an engine 1.
- the engine 1 is operated to drive the fan shaft of the cross flow fan 4 to rotate, and the air is taken from the air inlet above. Inhalation, discharged from the lower air outlet, gives the air a thrust, and the air also gives the platform a counter-force to allow the platform to gain a lift and float in the air.
- FIG. 7 is a fifth embodiment of the through-flow air suspension platform of the present invention, the platform includes an inner frame 11 of a rectangular or square structure, and four outer frames 10 of a rectangular structure are disposed around the inner frame 11
- a cross flow fan 4 is fixedly disposed in the outer frame 10, and the cross flow fan 4 is arranged in a clockwise or counterclockwise direction.
- the fan shaft of each cross flow fan 4 is connected to the shaft of the engine 1.
- the engine 1 works, driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, discharging from the lower air outlet, giving the air a thrust, and the air also giving the platform a counter force to make the platform Get a lift and float in the air.
- FIG. 8 is a sixth embodiment of the through-flow air suspension platform of the present invention.
- the platform includes an inner frame 11 of a rectangular or square structure, and a set of fixing plates 12 are disposed in the inner frame 11, and the inner frame 11 is disposed outside.
- a circular outer frame 10 having a rectangular structure and a square structure, a cross flow fan 4 is disposed in the outer frame 10 of the rectangular structure, and an engine 1 connected to the cross flow fan 4 is disposed in the outer frame 10 of the square structure, and The flow fan 4 is arranged in a clockwise or counterclockwise direction.
- the engine 1 works, driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, discharging from the lower air outlet, giving the air a thrust, and the air also giving the platform a counter force to make the platform Get a lift and float in the air.
- FIG. 9 is a seventh embodiment of the through-flow air suspension platform of the present invention.
- the platform includes an outer frame 10 of a rectangular structure, and the four corners of the outer frame 10 are respectively divided into rectangular frames, each of which is rectangular. frame A pair of cross flow fans 4 are disposed, and the fan shafts of each pair of cross flow fans 4 are disposed at the center of the outer frame 10.
- a steering gear 14 is coupled to the fan casing 2 of the cross flow fan 4, and a gearbox 13 is connected to the fan shaft of the cross flow fan 4, the engine 1 is connected to the gearbox 13, and an external unit is provided on the gearbox 13 and the engine 1.
- the control port 15 to which the control system is connected.
- FIG. 10 is an eighth embodiment of the through-flow air suspension platform of the present invention.
- one cross-flow fan 4 is reduced in each rectangular frame, and other structures are the same as the embodiment. 7 is the same.
Abstract
Description
Claims
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011203548626U CN202279234U (en) | 2011-09-21 | 2011-09-21 | Tubular air suspension platform |
CN201110281430.1 | 2011-09-21 | ||
CN201110281430.1A CN102358423B (en) | 2011-09-21 | 2011-09-21 | Through-flow air suspension platform |
CN201120354862.6 | 2011-09-21 |
Publications (1)
Publication Number | Publication Date |
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WO2013040847A1 true WO2013040847A1 (en) | 2013-03-28 |
Family
ID=47913804
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/CN2012/000852 WO2013040847A1 (en) | 2011-09-21 | 2012-06-19 | Through-flow air suspension platform |
Country Status (1)
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WO (1) | WO2013040847A1 (en) |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3065928A (en) * | 1960-07-16 | 1962-11-27 | Dornier Werke Gmbh | Multiple drive for aircraft having wings provided with transverse flow blowers |
US3082976A (en) * | 1960-07-02 | 1963-03-26 | Dornier Werke Gmbh | Aircraft with ground effect landing gear |
US3178131A (en) * | 1963-10-03 | 1965-04-13 | Laing Nikolaus | Aircraft wing structure |
US3212735A (en) * | 1956-12-07 | 1965-10-19 | Laing Nikolaus | Thrust means for powering aircraft |
US4194707A (en) * | 1977-12-16 | 1980-03-25 | Sharpe Thomas H | Lift augmenting device for aircraft |
US6016992A (en) * | 1997-04-18 | 2000-01-25 | Kolacny; Gordon | STOL aircraft |
CN101405182A (en) * | 2006-03-31 | 2009-04-08 | 范文有限公司 | Aircraft with aerodynamic lift generating device |
CN201679737U (en) * | 2010-05-25 | 2010-12-22 | 宁波丽辰电器有限公司 | Cross-flow fan |
CN102358423A (en) * | 2011-09-21 | 2012-02-22 | 陈晓春 | Through-flow air suspension platform |
CN202279234U (en) * | 2011-09-21 | 2012-06-20 | 陈晓春 | Tubular air suspension platform |
-
2012
- 2012-06-19 WO PCT/CN2012/000852 patent/WO2013040847A1/en active Application Filing
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3212735A (en) * | 1956-12-07 | 1965-10-19 | Laing Nikolaus | Thrust means for powering aircraft |
US3082976A (en) * | 1960-07-02 | 1963-03-26 | Dornier Werke Gmbh | Aircraft with ground effect landing gear |
US3065928A (en) * | 1960-07-16 | 1962-11-27 | Dornier Werke Gmbh | Multiple drive for aircraft having wings provided with transverse flow blowers |
US3178131A (en) * | 1963-10-03 | 1965-04-13 | Laing Nikolaus | Aircraft wing structure |
US4194707A (en) * | 1977-12-16 | 1980-03-25 | Sharpe Thomas H | Lift augmenting device for aircraft |
US6016992A (en) * | 1997-04-18 | 2000-01-25 | Kolacny; Gordon | STOL aircraft |
CN101405182A (en) * | 2006-03-31 | 2009-04-08 | 范文有限公司 | Aircraft with aerodynamic lift generating device |
CN201679737U (en) * | 2010-05-25 | 2010-12-22 | 宁波丽辰电器有限公司 | Cross-flow fan |
CN102358423A (en) * | 2011-09-21 | 2012-02-22 | 陈晓春 | Through-flow air suspension platform |
CN202279234U (en) * | 2011-09-21 | 2012-06-20 | 陈晓春 | Tubular air suspension platform |
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