CN2907080Y - Electromagnetic object emission device with energy storage in capacitor - Google Patents
Electromagnetic object emission device with energy storage in capacitor Download PDFInfo
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- CN2907080Y CN2907080Y CN 200620081395 CN200620081395U CN2907080Y CN 2907080 Y CN2907080 Y CN 2907080Y CN 200620081395 CN200620081395 CN 200620081395 CN 200620081395 U CN200620081395 U CN 200620081395U CN 2907080 Y CN2907080 Y CN 2907080Y
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Abstract
The utility model relates to a capacitor energy-storing electromagnetic-object launching device, which is used to launch the local object to the long distance by electromagnetic energy. The utility model utilizes the electromagnetic force to gradually accelerate the object to be launched until the required initial velocity is reached and then the object is to be launched, the launched electromagnetic force comes from the discharge loop which is composed of a multiple acceleration winding and an energy-storing capacitor, the electric energy stored by the energy-storing capacitor is discharged instantaneously to the acceleration winding, the powerful discharge current generates a powerful electromagnetic force to accelerate the object to be launched, the launched object is gradually and orderly accelerated by the multiple acceleration winding until the required initial velocity is reached and then the object is to be launched, the electric energy stored by the energy-storing capacitor of the multiple acceleration winding is more than the dynamic energy that the launched object obtains the initial velocity, so that the launched object is launched to the preset orbit. The capacitor energy-storing electromagnetic-object launching device only can launch the object that needs to be launched, moreover the utility model has the advantages of high-efficiency launch, large launching power, saving launching energy, cleanness, no pollution, no noise and environmental protection.
Description
Technical field
The utility model designs a kind of capacitance energy storage electromagnetism object emitting device, is used for the object of this locality is transmitted at a distance by electromagnetic energy, belongs to the space technology field.
Background technology
At present, known general satellites transmits is by chemical energy, and the carrier rocket combustion fuel arrives track with satellites transmits.Carrier rocket is a means of transportation, is not the purpose that will launch, just finishes when inferior emission and scraps.The weight of carrier rocket will be much larger than the weight of satellite, and is therefore high with the launch an artificial satellite unavailable energy that consumes of carrier rocket, and the chemical fuel of carrier rocket burning causes great pollution to Earth'S atmosphere.
Summary of the invention
The utility model provides a kind of capacitance energy storage electromagnetism object emitting device, and it is to utilize electromagnetic force will launch object acceleration gradually, accelerates to the needed initial velocity of emission always, and object is launched.The electromagnetic force of emission comes from the discharge loop of multipole accelerating coil and storage capacitor formation, the electric energy that storage capacitor stores is instantaneous to discharge to accelerating coil, powerful discharging current produces the object that powerful electromagnetic force acceleration is launched, the object that is launched is accelerated to the required initial velocity of emission orderly gradually by multistage accelerating coil, and object is launched.The electric energy that the storage capacitor of multipole accelerating coil stores just can be transmitted into planned orbit with being launched object greater than being launched the kinetic energy that object obtains initial velocity.
The technical scheme that its technical problem that solves the utility model adopts is: be provided with multistage accelerating coil and magnetic test coil on a launcher, accelerating coil is in parallel with storage capacitor through the high rate discharge switch, the discharge switch of first order accelerating coil is controlled by firing order, controlled by magnetic test coil separately from the second level to the discharge switch of n level accelerating coil, the storage capacitor of accelerating coils at different levels is connected on the high power DC high voltage source by current-limiting resistance and charges.Before the emission, the storage capacitor of accelerating coils at different levels is full of, after receiving firing order, the discharge switch of first order accelerating coil is connected, storage capacitor produces the object that the electromagnetic force pulling is launched to coil discharge, when the movement of objects that is launched arrives the magnetic test coil position, the discharge switch of on-off controller control second level accelerating coil is connected, storage capacitor produces electromagnetic force to second level coil discharge is accelerated the object that is launched once more, and the object that is launched by that analogy constantly is accelerated until reaching the required initial velocity of emission.
The beneficial effects of the utility model are: this capacitance energy storage electromagnetism object emitting device; only emission needs the object of emission, and the emission effciency height is compared with carrier rocket and can be saved emitted energy greatly; because electromagnetic force is used in emission, therefore cleaning, pollution-free, noiseless, protection environment.In addition, the huge instantaneous energy the during emission of this capacitance energy storage electromagnetism object emitting device is from the instantaneous discharge of storage capacitor, and the storage capacitor storage of electrical energy is a power supply long period abundance, does not need the power supply of super high power.This capacitance energy storage electromagnetism object emitting device is simple in structure, transmitting power is big, reliable operation, manufacturing cost are relatively low.
Description of drawings
Below in conjunction with drawings and Examples the utility model is further specified.
Fig. 1 is the utility model structural representation.
Fig. 2 is the utility model fundamental diagram.
Among the figure, 1. first order accelerating coil, 2. second level accelerating coil, 3. third level accelerating coil, n. n level accelerating coil, n-1. n-1 level accelerating coil, L. accelerating coil, Le. magnetic test coil, C. storage capacitor, R. current-limiting resistance, K. high rate discharge switch, Ka. high rate discharge on-off controller, E. high-voltage DC power supply, the object that M. is launched, m. spurs magnetic field, I. discharging current, T. launcher, G. ground.
Embodiment
In Fig. 1, this capacitance energy storage electromagnetism object emitting device is on launcher (T), according to certain intervals, has fixedly mounted first order accelerating coil (1), second level accelerating coil (2) etc. and has fixedly mounted n level accelerating coil and n-1 magnetic test coil (Le) altogether.Magnetic test coil (Le) connects high rate discharge on-off controller (Ka), (Ka) connect high rate discharge switch (K), storage capacitor (C), high rate discharge switch (K), accelerating coil (L) are connected into discharge loop, storage capacitor (C) is connected in parallel on the high-voltage DC power supply (E) through current-limiting resistance (R), has placed the object (M) that is launched in the launcher (T).
In Fig. 1, embodiment shown in Figure 2, this capacitance energy storage electromagnetism object emitting device is in running order.After receiving firing order, high rate discharge switch (K) closure of first order accelerating coil (1), storage capacitor (C) is to accelerating coil (L) discharge generation electromagnetic force, and the object that is launched (M) is spurred by electromagnetic force, on moved on to second level accelerating coil (2) magnetic test coil (Le) locate.Magnetic test coil (Le) detect the object (M) that is launched on move the back and produce detection signal, detection signal is delivered to on-off controller (Ka), (Ka) high rate discharge switch (K) closure of control second level accelerating coil (2), the storage capacitor (C) of second level accelerating coil (2) discharges to accelerating coil (L), produced pulling magnetic field (m), the object that is launched (M) is accelerated once more.The object that is launched by that analogy (M) can be accelerated n time, as long as the progression n of accelerating coil is enough big, the object that is launched (M) can be accelerated to the required initial velocity of high emission.
Claims (3)
1, a kind of capacitance energy storage electromagnetism object emitting device, it is characterized in that on launcher, according to certain intervals, fixedly mounted a n level accelerating coil and n-1 magnetic test coil, magnetic test coil connects the high rate discharge on-off controller, and on-off controller connects, control high rate discharge switch, and storage capacitor, high rate discharge switch, accelerating coil are connected into discharge loop, storage capacitor is connected in parallel on the high-voltage DC power supply through current-limiting resistance, has placed the object that is launched in the launcher.
2, a kind of capacitance energy storage electromagnetism object emitting device according to claim 1 is characterized in that the storage capacitor store electrical energy is: n/2CE
2, the required kinetic energy of the object that is launched is: 1/2MV
2, n/2CE
2＞1/2MV
2, E: the voltage of high-voltage DC power supply, C: the capacity of storage capacitor, M: be launched the quality of object, V: the initial velocity that is launched object.
3, a kind of capacitance energy storage electromagnetism object emitting device according to claim 1, the shell that it is characterized in that being launched object is to be made by the material of the action of a magnetic field.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620081395 CN2907080Y (en) | 2006-03-06 | 2006-03-06 | Electromagnetic object emission device with energy storage in capacitor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620081395 CN2907080Y (en) | 2006-03-06 | 2006-03-06 | Electromagnetic object emission device with energy storage in capacitor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2907080Y true CN2907080Y (en) | 2007-05-30 |
Family
ID=38115725
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200620081395 Expired - Fee Related CN2907080Y (en) | 2006-03-06 | 2006-03-06 | Electromagnetic object emission device with energy storage in capacitor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2907080Y (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103134383A (en) * | 2013-02-01 | 2013-06-05 | 上海交通大学 | Electromagnetic launching device capable of controlling force and electromagnetic launching method thereof |
| CN107860263A (en) * | 2017-11-24 | 2018-03-30 | 广东交通职业技术学院 | A kind of dynamical system and emitter for emitter |
| CN109323618A (en) * | 2017-08-01 | 2019-02-12 | 邓志昌 | A kind of multistage electromagnetic launch system |
| CN110127085A (en) * | 2019-05-16 | 2019-08-16 | 中国科学院电工研究所 | Driven with current sources type electromagnetic launch system |
| CN111964524A (en) * | 2020-08-24 | 2020-11-20 | 孙志强 | Multistage induction type electromagnetic transmitter |
-
2006
- 2006-03-06 CN CN 200620081395 patent/CN2907080Y/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103134383A (en) * | 2013-02-01 | 2013-06-05 | 上海交通大学 | Electromagnetic launching device capable of controlling force and electromagnetic launching method thereof |
| CN103134383B (en) * | 2013-02-01 | 2015-04-22 | 上海交通大学 | Electromagnetic launching device capable of controlling force and electromagnetic launching method thereof |
| CN109323618A (en) * | 2017-08-01 | 2019-02-12 | 邓志昌 | A kind of multistage electromagnetic launch system |
| CN107860263A (en) * | 2017-11-24 | 2018-03-30 | 广东交通职业技术学院 | A kind of dynamical system and emitter for emitter |
| CN110127085A (en) * | 2019-05-16 | 2019-08-16 | 中国科学院电工研究所 | Driven with current sources type electromagnetic launch system |
| CN111964524A (en) * | 2020-08-24 | 2020-11-20 | 孙志强 | Multistage induction type electromagnetic transmitter |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |