CN102442526A - Potential energy transporting system - Google Patents
Potential energy transporting system Download PDFInfo
- Publication number
- CN102442526A CN102442526A CN2010105037964A CN201010503796A CN102442526A CN 102442526 A CN102442526 A CN 102442526A CN 2010105037964 A CN2010105037964 A CN 2010105037964A CN 201010503796 A CN201010503796 A CN 201010503796A CN 102442526 A CN102442526 A CN 102442526A
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- potential energy
- impact
- bracing frame
- power valve
- impact bead
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Abstract
The invention relates to a device system for quick transporting with potential energy. The potential energy transporting system comprises a potential energy source generation system, an impact system and a launching system, wherein the potential energy source generation system comprises a potential energy column (1), a pulley (2), a winching rope (3) and a winch (4), the impact system comprises an impact ball (6), an impact ball support (9) and a pendulum rope (8), and the launching system comprises a launching tube (11), a launching tube support (12) and a transporting cabin (15). The impact ball (6) is lifted to a required height by the winch (4), then descends by the aid of gravitational acceleration, is aligned to and violently impacts an impact point of the tail of the transporting cabin, and the transporting cabin is launched like a cannonball so as to reach a scheduled goods yard. The potential energy transporting system is fast in transportation and long in distance without fuel, and meets the requirements of environmental protection and low-carbon economy.
Description
Technical field
The present invention relates to transport field, particularly a kind of apparatus system that utilizes potential energy to carry out fast traffic.
Background technology
Existing transportation means is generally automobile, train, steamer or aircraft, and the speed of automobile, train, steamer is lower, can not make to transport goods and materials and arrive the destination rapidly.Air speed is very fast, but because various condition costs such as cost of aircraft own and airport are very high, transportation means that neither be desirable.Above-mentioned in addition various forms of transport all need fuel, also are unfavorable for environmental protection.
Summary of the invention
The objective of the invention is to overcome the deficiency of existing transportation means, providing a kind of can not need the energy-saving and environmental protection type transportation means of fuel again with the goods and materials fast traffic.
Technical scheme of the present invention is such.This potential energy transport systems comprises that source of potential energy produces system, impact system and emission coefficient.Source of potential energy generation system comprises potential energy post, pulley, lift rope, winch; Impact system comprises impact bead, impact bead bracing frame, pendulum rope; Emission coefficient comprises power valve, power valve bracing frame and transport pod.With the impact bead bracing frame firm be fixed on ground, the upper end of pendulum rope is connected with the frame pipe of bracing frame, its lower end is connected with impact bead through pinning; Power valve is through the firm the place ahead that is placed in impact bead of bracing frame, and transport pod is placed in the power valve.Install at the rear of impact bead bracing frame, a fixing potential energy post, and the top of potential energy post is equipped with pulley, and the electromagnet handgrip is connected with winch through lift rope.
Use when of the present invention, at first utilize the potential energy physical principle to calculate the transport pod range ability, earlier lift rope is connected with the electromagnet handgrip through potential energy post pulley; Handgrip is caught impact bead through the suspension ring on the impact bead, through electric winch impact bead is risen to needed height, makes the electromagnet handgrip break away from impact bead through remote control equipment (RCE) again; Impact bead descends with acceleration due to gravity, and the rum point of aiming at the transportation storehouse afterbody that is arranged in power valve clashes, and transport pod is launched as shell; According to the arc trajectory high-speed flight; When land soon in cabin to be transported,, automatically the deceleration pack of transport pod afterbody is opened through the photosensitive sensor components that transport pod is settled; The open deceleration parachute speed that makes reduces very soon, transport pod safety drop to predetermined goods yard.
The present invention has following effect:
1, travelling speed of the present invention is fast, and speed per hour can reach the 1000-500 kilometer;
2, transportation range is far away in the specific time scope, and transportation range arrives in the several hundred kilometers scope at several kilometers as required;
3, the present invention can be provided with many group potential energy conveying arrangements according to the needs of transportation volume;
4, use the present invention not need fuel, meet environmental protection, low-carbon economy requirement;
5, the present invention does not have complex mechanical structures such as driving engine, and is cheap, greatly reduces cost of transportation.
Description of drawings
Fig. 1 is that source of potential energy of the present invention produces the system architecture scheme drawing.
Fig. 2 is an impact system structural representation of the present invention.
Fig. 3 is an emission coefficient structural representation of the present invention.
The specific embodiment
The specific embodiment of the present invention combines accompanying drawing explanation.
Like Fig. 1, Fig. 2 and shown in Figure 3,1-potential energy post 2-pulley 3-lift rope 4-winch 5-electromagnet handgrip 6-impact bead 7-suspension ring 8-pendulum rope 9-impact bead bracing frame 10-pin 11-power valve 12-power valve bracing frame 13-bumper 14-thermal insulation tile 15-transportation storehouse 16-rum point 17-deceleration pack
The present invention includes source of potential energy and produce system, impact system and emission coefficient, source of potential energy generation system comprises potential energy post (1), pulley (2), lift rope (3) and winch (4); Impact system comprises impact bead (6), impact bead bracing frame (9) and pendulum rope (8); Emission coefficient comprises power valve (11), power valve bracing frame (12) and transport pod (15); With impact bead bracing frame (9) firm be fixed on ground; The upper end of pendulum rope (8) is connected with the frame pipe of bracing frame (9), and its lower end is connected with impact bead (6) through pin (10), and power valve (11) is through the firm the place ahead that is placed in impact bead bracing frame (9) of power valve bracing frame (12); Transport pod (15) is placed in the power valve (11); Install at the rear of impact bead bracing frame (9), a fixing potential energy post (1), and the top of potential energy post (1) is equipped with pulley (2), and electromagnet handgrip (5) is connected with winch (4) through lift rope (3).The afterbody of transport pod (15) is equipped with bumper (13) and deceleration pack (17).Power valve is overheated in order to prevent to launch, and the inwall of power valve has one deck thermal insulation tile (14), simultaneously, on the bulkhead of transport pod, scribbles lubricating oil.The elevation angle of power valve (11) is between the 20-45 degree.
But the present invention through structural improvement, also can be used as the fast traffic instrument of shipper except shipping goods.
Claims (4)
1. the potential energy transport systems is characterized in that this system comprises that source of potential energy produces system, impact system and emission coefficient, and source of potential energy generation system comprises potential energy post (1), pulley (2), lift rope (3) and winch (4); Impact system comprises impact bead (6), impact bead bracing frame (9) and pendulum rope (8); Emission coefficient comprises power valve (11), power valve bracing frame (12) and transport pod (15); With impact bead bracing frame (9) firm be fixed on ground; The upper end of pendulum rope (8) is connected with the frame pipe of bracing frame (9), and its lower end is connected with impact bead (6) through pin (10), and power valve (11) is through the firm the place ahead that is placed in impact bead bracing frame (9) of power valve bracing frame (12); Transport pod (15) is placed in the power valve (11); Install at the rear of impact bead bracing frame (9), a fixing potential energy post (1), and the top of potential energy post (1) is equipped with pulley (2), and electromagnet handgrip (5) is connected with winch (4) through lift rope (3).
2. potential energy transport systems according to claim 1 is characterized in that the afterbody of transport pod (15) is equipped with bumper (13) and deceleration pack (17).
3. potential energy transport systems according to claim 1 is characterized in that impact bead (6) upper end is equipped with suspension ring (7).
4. potential energy transport systems according to claim 1, the elevation angle that it is characterized in that power valve (11) is between the 20-45 degree.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010105037964A CN102442526A (en) | 2010-10-12 | 2010-10-12 | Potential energy transporting system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010105037964A CN102442526A (en) | 2010-10-12 | 2010-10-12 | Potential energy transporting system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102442526A true CN102442526A (en) | 2012-05-09 |
Family
ID=46005547
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010105037964A Pending CN102442526A (en) | 2010-10-12 | 2010-10-12 | Potential energy transporting system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102442526A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2036439U (en) * | 1988-07-30 | 1989-04-26 | 方继明 | Ejection return type aircraft toy |
| CN1447091A (en) * | 2002-03-26 | 2003-10-08 | 拉菲尔军械发展公司 | Low characteristic shooting system and method for bullet |
| CN101013017A (en) * | 2005-12-28 | 2007-08-08 | 毛若虚 | Troops and munitions battlefield rapid transportation system device |
| CN201016666Y (en) * | 2006-10-11 | 2008-02-06 | 冯景亮 | Parachute bullet |
| CN201218693Y (en) * | 2008-05-27 | 2009-04-08 | 保定维特瑞交通设施工程有限责任公司 | Environment-friendly anti-riot fire arms |
| CN201343147Y (en) * | 2008-12-03 | 2009-11-11 | 北京航天发射技术研究所 | Emitting system for ejecting aircraft in pneumatic track |
| CN201817064U (en) * | 2010-10-12 | 2011-05-04 | 杨礼诚 | Potential energy transportation system |
-
2010
- 2010-10-12 CN CN2010105037964A patent/CN102442526A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2036439U (en) * | 1988-07-30 | 1989-04-26 | 方继明 | Ejection return type aircraft toy |
| CN1447091A (en) * | 2002-03-26 | 2003-10-08 | 拉菲尔军械发展公司 | Low characteristic shooting system and method for bullet |
| CN101013017A (en) * | 2005-12-28 | 2007-08-08 | 毛若虚 | Troops and munitions battlefield rapid transportation system device |
| CN201016666Y (en) * | 2006-10-11 | 2008-02-06 | 冯景亮 | Parachute bullet |
| CN201218693Y (en) * | 2008-05-27 | 2009-04-08 | 保定维特瑞交通设施工程有限责任公司 | Environment-friendly anti-riot fire arms |
| CN201343147Y (en) * | 2008-12-03 | 2009-11-11 | 北京航天发射技术研究所 | Emitting system for ejecting aircraft in pneumatic track |
| CN201817064U (en) * | 2010-10-12 | 2011-05-04 | 杨礼诚 | Potential energy transportation system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20120509 |