CN203083451U - Rocket projectile control wing ejection control device - Google Patents
Rocket projectile control wing ejection control device Download PDFInfo
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- CN203083451U CN203083451U CN 201320096291 CN201320096291U CN203083451U CN 203083451 U CN203083451 U CN 203083451U CN 201320096291 CN201320096291 CN 201320096291 CN 201320096291 U CN201320096291 U CN 201320096291U CN 203083451 U CN203083451 U CN 203083451U
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- rocket projectile
- power transmission
- transmission pole
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- power output
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Abstract
The utility model discloses a rocket projectile control wing ejection control device. The rocket projectile control wing ejection control device mainly comprises a rocket projectile wall, a power supply pipe, a power output rod, a power transmission rod, a power output connecting rod, a motor, a wing surface power transmission rod and a wing surface. When a rocket projectile is ignited for launching, a time delay exists; after a rocket flies out from a launching tube, an electronic ignition device in the power supply pipe ignites black powder; and the black powder generates a great amount of gas to push the power output rod to jack upwards so as to push the power transmission rod and the power output connecting rod, so that the wing surface is pushed, and the wing surface and the wing surface power transmission rod are positioned on the same line, the power output rod is perpendicular to the wing surface, the power transmission rod is parallel to the wing surface, and the motor can control the wing surface by rotation. Under the action of external fluid resistance and mechanical self-locking, the wing surface is fixed at a specific position, and the short-time blocking of the motor caused by the vibration of the wing surface is prevented. The ejection of the existing power rocket projectile control wing can be controlled. The rocket projectile control wing ejection control device has the mechanical self-locking capacity and improves the control reliability.
Description
Technical field
The utility model belongs to a kind of rocket projectile control wing and ejects control device, belongs to a kind of controlled rocket projectile control wing in back that ejects especially and ejects control device.
Background technology
At present, it is uncontrollable that the most rocket projectile control wing ejects the back, or based on a kind of motorless rocket projectile control wing, eject the back controllable device, also or a kind of rocket projectile control device that does not have ejection, above-mentioned first kind of uncontrollable wing of ejection is applied in accuracy less demanding mostly, to obtain cheapness, the rocket projectile that large tracts of land is killed and wounded, second kind of precise guidance of unpowered section that is mainly used in rocket projectile, above-mentioned the third is mainly used in does not need often to transport or answer the large rocket bullet, and the above-mentioned ejection control wing cuts both ways, and can't realize the advantage that they are all simultaneously.
Summary of the invention
The purpose of this utility model is to provide a kind of rocket projectile control wing to eject control device, particularly provides a kind of controlled rocket projectile control wing in back that ejects to eject control device.
The technical problems to be solved in the utility model provides a kind of dynamic rocket projectile control wing and ejects control device, and it mainly comprises rocket projectile bullet wall, power supply pipe, power output rod, power transmission pole, power output connecting rod, motor, profile power transmission pole, aerofoil.Rocket projectile bullet wall has four aerofoils to skid off groove, and to cooperate the ejection of aerofoil, the inside of rocket projectile bullet wall is four motor installing ports of distribution evenly, power supply pipe installing port, profile power transmission pole installing port, there is guide groove the centre of rocket projectile bullet wall, so that the parts of rocket projectile power set to be installed; The power supply pipe is installed in the corresponding installing port of rocket projectile bullet wall, power supply pipe one end opening, so that power output rod can be in interior slip, the electronic striking device is arranged at power supply pipe bottom, and an amount of black powder is arranged at the bottom; The external diameter of power output rod is identical with the internal diameter of power supply pipe, and an end has axle, to cooperate the hole on the power transmission pole; The power transmission pole is porose near an end of power output rod, and the other end has one, and axle matches with the hole on the power output connecting rod; Power output connecting rod has the hole that cooperates with it near an end of power transmission pole, and the other end has the hole of matching with aerofoil, so that power output connecting rod can slide on aerofoil; Worm gear is arranged on the motor, be installed in four installing ports of rocket projectile bullet wall, worm gear matches with the worm screw on the profile power transmission pole; Profile power transmission pole one end has worm gear, the other end has one, match with the hole of aerofoil one end, the profile power transmission pole is installed in the installing port of the profile power transmission pole on the rocket projectile bullet wall, so that the profile power transmission pole can not move forward and backward in interior rotation; Aerofoil one end has the hole of matching with the profile power transmission pole, and the other end is used for launching the control air-flow.
When rocket projectile is not launched, power output rod is inserted in the power supply pipe, power output rod thereby be pulled to low side, then hold the power transmission pole, power output connecting rod is held aerofoil, and an angle is arranged between profile power transmission pole and the aerofoil, the uncontrollable motor of motor rotates, and prevents from because of the rotation of aerofoil aerofoil to be ejected.
When rocket projectile when emission igniting, a time delay is arranged, treat that rocket flies out from launching tube after, black powder is lighted in electronic striking device sparking in the power supply pipe, black powder produces a large amount of gases, propulsion power take-off lever make progress jack-up, propulsion power transmission pole then, power output connecting rod, make aerofoil be pushed to the profile power transmission pole on a line, this moment power output rod perpendicular to aerofoil, the power transmission pole is parallel to aerofoil, at this moment, motor can be by rotation control aerofoil; Because the effect and the mechanical self-latching of external fluid resistance make aerofoil be fixed on ad-hoc location, prevent to cause motor stuck in short-term because of the vibrations of aerofoil.
In summary, the utility model has been realized can controlling in the ejection of the dynamic rocket projectile control wing.
In addition, structure of the present utility model also has the ability of mechanical self-latching, makes aerofoil be fixed on a certain location, has improved the reliability of control.
Description of drawings
Fig. 1 arrow bullet control wing ejects the front view of the power supply pipe of control device
This rocket projectile of Fig. 2 control wing ejects the stereogram of the power supply pipe of control device
This rocket projectile of Fig. 3 control wing ejects the front view of the power output rod of control device
This rocket projectile of Fig. 4 control wing ejects the elevation view of the power output rod of control device
This rocket projectile of Fig. 5 control wing ejects the front view of the power transmission pole of control device
This rocket projectile of Fig. 6 control wing ejects the elevation view of the power transmission pole of control device
This rocket projectile of Fig. 7 control wing ejects the front view of the power output connecting rod of control device
This rocket projectile of Fig. 8 control wing ejects the elevation view of the power output connecting rod of control device
This rocket projectile of Fig. 9 control wing ejects the stereogram figure of control device motor
This rocket projectile of Figure 10 control wing ejects the front view of the profile power take-off lever of control device
This rocket projectile of Figure 11 control wing ejects the stereogram of the profile power take-off lever of control device
This rocket projectile of Figure 12 control wing ejects the stereogram of the aerofoil of control device
This rocket projectile of Figure 13 control wing ejects the profile power take-off lever of control device and the installation diagram of aerofoil
This rocket projectile of Figure 14 control wing eject control device rocket projectile bullet wall just wait shaft side figure
This rocket projectile of Figure 15 control wing ejects a certain viewing angles stereogram of the rocket projectile bullet wall of control device
General assembly drawing when this rocket projectile of Figure 16 control wing ejection control device aerofoil is packed up
The master looked cutaway view when this rocket projectile of Figure 17 control wing ejection control device aerofoil was packed up
General assembly drawing when this rocket projectile of Figure 18 control wing ejection control device aerofoil is opened
Master when this rocket projectile of Figure 19 control wing ejection control device aerofoil is opened looks cutaway view
The specific embodiment
Below by example and accompanying drawing thereof the utility model is described in further details;
Referring to Fig. 1-Fig. 2, this rocket projectile control wing ejects the power supply pipe 1 of control device, power supply pipe 1 is installed in the rocket projectile bullet wall 17 corresponding installing ports 20, power supply pipe 1 one end openings, so that power output rod 3 can be in interior slip, electronic striking device 2 is arranged at power supply pipe 1 bottom, and an amount of black powder is arranged at the bottom.
Referring to Fig. 3-Fig. 4, this rocket projectile control wing ejects the power output rod 3 of control device, and the external diameter of power output rod 3 is identical with the internal diameter of power supply pipe 1, and an end has axle 4, to cooperate the hole 6 on the power transmission pole 5.
Referring to Fig. 5-Fig. 6, this rocket projectile control wing ejects the power transmission pole 5 of control device, and power transmission pole 5 is porose 6 near an end of power output rods 3, and the other end has one 7, and axle 7 matches with the hole 8 that power is exported on the connecting rod 9.
Referring to Fig. 7-Fig. 8, this rocket projectile control wing ejects the power output connecting rod 9 of control device, power output connecting rod 9 has the hole 8 that cooperates with it near an end of power transmission pole 5, and the other end has the hole 10 of matching with aerofoil 15, so that power output connecting rod 9 can slide on aerofoil 15.
Referring to Fig. 9, this rocket projectile control wing ejects the motor 12 of control device, and worm gear 11 is arranged on the motor 12, is installed in four installing ports 21 of rocket projectile bullet wall 17, and worm gear 11 matches with the worm screw on the profile power transmission pole 13.
Referring to Figure 10-Figure 11, this rocket projectile control wing ejects the profile power transmission pole 13 of control device, profile power transmission pole 13 1 ends have worm gear, the other end has one 14, match with the hole 16 of aerofoil 15 1 ends, profile power transmission pole 13 is installed in the installing port 23 of the profile power transmission pole 13 on the rocket projectile bullet wall 17, so that profile power transmission pole 13 can not move forward and backward in interior rotation.
Referring to Figure 12, this rocket projectile control wing ejects the aerofoil 15 of control device, and aerofoil 15 1 ends have the hole 16 of matching with profile power transmission pole 13, and the other end is used for launching the control air-flow.
Referring to Figure 14-Figure 15, this rocket projectile control wing ejects the rocket projectile bullet wall 17 of control device, rocket projectile bullet wall 17 has four aerofoils to skid off groove 18, to cooperate the ejection of aerofoil 15, the inside of rocket projectile bullet wall 17 is four motor installing ports 20 of distribution evenly, power supply pipe installing port 21, profile power transmission pole installing port 23, there is guide groove 19 centre of rocket projectile bullet wall, so that the parts of rocket projectile power set to be installed.
Referring to Figure 16-Figure 17, general assembly drawing when this rocket projectile control wing ejection control device aerofoil 15 is packed up, when rocket projectile was not launched, power output rod 3 was inserted in the power supply pipe 1, power output rod 3 thereby be pulled to low side, then hold power transmission pole 5, power output connecting rod 9 is held aerofoil 15, between profile power transmission pole 13 and the aerofoil 15 angle is arranged, motor 12 uncontrollable aerofoils 15 rotate, and prevent from because of the rotation of aerofoil 15 aerofoil 15 to be ejected.
Referring to Figure 18-Figure 19, general assembly drawing when this rocket projectile control wing ejection control device aerofoil 15 is opened, when rocket projectile igniting emission, a time delay is arranged, treat that rocket flies out from launching tube after, black powder is lighted in electronic striking device 2 sparkings in the power supply pipe 1, black powder produces a large amount of gases, and propulsion power take-off lever 3 is jack-up upwards, and the propulsion power transmission pole 5 then, power output connecting rod 9, make aerofoil 15 be pushed to profile power transmission pole 13 on a line, power output this moment connecting rod 9 is perpendicular to profile power transmission pole 13, power transmission pole 5 is parallel to aerofoil 15, at this moment, motor 12 can be by rotation control aerofoil 15; Because the effect and the mechanical self-latching of external fluid resistance make aerofoil 15 be fixed on ad-hoc location, prevent to cause motor 12 stuck in short-term because of the vibrations of aerofoil 15.
The utility model has been realized can controlling in the ejection of the dynamic rocket projectile control wing.
The above only is a kind of embodiment of the present utility model; should be understood that; for the those of ordinary skill in field, the utility model place under the prerequisite that does not break away from the utility model principle; can also make a lot of remodeling; such as, the riding position of plus-minus number of surface or change aerofoil, the kind of drive of adjustment motor and profile power take-off lever; change the length of each bar etc., these also should belong to protection domain of the present utility model.
Claims (1)
1. the rocket projectile control wing ejects control device, and it mainly comprises rocket projectile bullet wall, the power supply pipe, and power output rod, the power transmission pole, power output connecting rod, motor, the profile power transmission pole, aerofoil is characterized in that:
Rocket projectile bullet wall has four aerofoils to skid off groove, and to cooperate the ejection of aerofoil, the inside of rocket projectile bullet wall is four motor installing ports of distribution evenly, power supply pipe installing port, profile power transmission pole installing port, there is guide groove the centre of rocket projectile bullet wall, so that the parts of rocket projectile power set to be installed;
The power supply pipe is installed in the corresponding installing port of rocket projectile bullet wall, power supply pipe one end opening, so that power output rod can be in interior slip, the electronic striking device is arranged at power supply pipe bottom, and an amount of black powder is arranged at the bottom; The external diameter of power output rod is identical with the internal diameter of power supply pipe, and an end has axle, to cooperate the hole on the power transmission pole;
The power transmission pole is porose near an end of power output rod, and the other end has one, and axle matches with the hole on the power output connecting rod;
Power output connecting rod has the hole that cooperates with it near an end of power transmission pole, and the other end has the hole of matching with aerofoil, so that power output connecting rod can slide on aerofoil;
Worm gear is arranged on the motor, be installed in four installing ports of rocket projectile bullet wall, worm gear matches with the worm screw on the profile power transmission pole;
Profile power transmission pole one end has worm gear, the other end has one, match with the hole of aerofoil one end, the profile power transmission pole is installed in the installing port of the profile power transmission pole on the rocket projectile bullet wall, so that the profile power transmission pole can not move forward and backward in interior rotation;
Aerofoil one end has the hole of matching with the profile power transmission pole, and the other end is used for launching the control air-flow.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320096291 CN203083451U (en) | 2013-03-04 | 2013-03-04 | Rocket projectile control wing ejection control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320096291 CN203083451U (en) | 2013-03-04 | 2013-03-04 | Rocket projectile control wing ejection control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203083451U true CN203083451U (en) | 2013-07-24 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320096291 Expired - Lifetime CN203083451U (en) | 2013-03-04 | 2013-03-04 | Rocket projectile control wing ejection control device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203083451U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103134394A (en) * | 2013-03-04 | 2013-06-05 | 丁云广 | Rocket projectile control wing ejection control device |
-
2013
- 2013-03-04 CN CN 201320096291 patent/CN203083451U/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103134394A (en) * | 2013-03-04 | 2013-06-05 | 丁云广 | Rocket projectile control wing ejection control device |
| CN103134394B (en) * | 2013-03-04 | 2014-10-29 | 丁云广 | Rocket projectile control wing ejection control device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20130724 Effective date of abandoning: 20141029 |
|
| RGAV | Abandon patent right to avoid regrant |