CN204767410U - Anti - umbrella formula model rocket recoverable capsule separating mechanism - Google Patents
Anti - umbrella formula model rocket recoverable capsule separating mechanism Download PDFInfo
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- CN204767410U CN204767410U CN201520407126.0U CN201520407126U CN204767410U CN 204767410 U CN204767410 U CN 204767410U CN 201520407126 U CN201520407126 U CN 201520407126U CN 204767410 U CN204767410 U CN 204767410U
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- rocket
- model
- return capsule
- recoverable capsule
- umbrella
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Abstract
The utility model discloses an anti - umbrella formula model rocket recoverable capsule separating mechanism, including recoverable capsule parachute cabin cover, recoverable capsule parachute cabin cover is connected with recoverable capsule and rocket rocket body through the rubber band, and the inside rigid coupling of recoverable capsule has the control steering wheel, is provided with the steel wire on the control steering wheel, and the steel wire is connected with the rubber band, anti - umbrella is installed to rocket rocket body afterbody. The utility model discloses the quickly separating that can make the rocket realize recoverable capsule and rocket rocket body when the whereabouts can improve the success rate of rocket separation greatly, has reduced the internal force of rocket docking mechanism, has reduced the requirement to structural strength, has reduced the rocket cost, is favorable to the popularization of model spacecraft.
Description
Technical field
The utility model belongs to machine control techniques field, is specifically related to a kind of anti-umbrella-type model rocket return capsule separating mechanism.
Background technology
Rocket model is the one in model plane, after the existing separating mechanism launching separate type rocket return capsule adopts and spring-compressed accumulation of energy is arrived specified altitude assignment, control spring releases energy and is separated, this separate mode due to structural internal force large, cause Success rate of virus isolation low, and, to the strength of materials and steering wheel torque requiremnt high, improve manufacture and the launch cost of rocket model.
Utility model content
The purpose of this utility model is to provide anti-umbrella-type model rocket return capsule separating mechanism, which solves existingly to launch the low problem of separate type rocket return capsule its disengagement success rate.
The technical scheme that the utility model adopts is, anti-umbrella-type model rocket return capsule separating mechanism, comprise return capsule parachute hatchcover, return capsule parachute hatchcover is connected with return capsule and rocket rocket body by rubber band, return capsule inside is connected with control steering wheel, control steering wheel is provided with steel wire, steel wire is connected with rubber band; Rocket rocket body afterbody is provided with anti-umbrella.
Feature of the present utility model is also,
Rubber band is laid around return capsule parachute hatchcover, return capsule and rocket rocket body.
The beneficial effects of the utility model are, anti-umbrella-type model rocket return capsule separating mechanism, by laying rubber band around return capsule parachute hatchcover, return capsule and rocket rocket body, reduce the requirement to structural strength and steering wheel torsion, rocket can be made when falling to realize the quick separating of return capsule and rocket rocket body, greatly can improve the success rate of Separation, reduce the internal force of rocket docking mechanism, reduce the requirement to structural strength, reduce rocket cost, be conducive to the universal of model spacecraft.
Accompanying drawing explanation
Fig. 1 is the structural representation of the utility model anti-umbrella-type model rocket return capsule separating mechanism;
Fig. 2 is the structural representation of the utility model anti-umbrella when opening.
In figure, 1. return capsule parachute hatchcover, 2. controls steering wheel, 3. rubber band, 4. return capsule, 5. rocket rocket body, 6. anti-umbrella, 7. steel wire.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the utility model is described in detail.
As depicted in figs. 1 and 2, anti-umbrella-type model rocket return capsule separating mechanism, comprise return capsule parachute hatchcover 1, return capsule parachute hatchcover 1 is connected with return capsule 4 and rocket rocket body 5 by rubber band 3, rubber band 3 is laid along return capsule parachute hatchcover 1, return capsule 4 and rocket rocket body 5 surrounding, return capsule 4 inside is connected with and controls steering wheel 2, controls steering wheel 2 is provided with steel wire 7, and steel wire 7 is connected with rubber band 3; Rocket rocket body 5 afterbody is provided with anti-umbrella 6.
Operation principle of the present utility model is, fire a rocket model time, rubber band 3 is laid along return capsule parachute hatchcover 1, return capsule 4 and rocket rocket body 5 surrounding and strained, then the other end of rubber band 3 is fixed on the steel wire 7 of control steering wheel 2, anti-umbrella 6 is in rounding state; Launch and arrive after specified altitude assignment, control steering wheel 2 rocking arm and rotate, steel wire 7 is retracted, rubber band 3 fast-falling, and anti-umbrella 6 is opened thereupon, and rocket increases due to resistance, and speed sharply reduces, and completes being separated of rocket rocket body 5 and return capsule 4.
Claims (2)
1. anti-umbrella-type model rocket return capsule separating mechanism, it is characterized in that: comprise return capsule parachute hatchcover (1), described return capsule parachute hatchcover (1) is connected with return capsule (4) and rocket rocket body (5) by rubber band (3), return capsule (4) inside is connected with and controls steering wheel (2), control steering wheel (2) is provided with steel wire (7), steel wire (7) is connected with rubber band (3); Rocket rocket body (5) afterbody is provided with anti-umbrella (6).
2. anti-umbrella-type model rocket return capsule separating mechanism according to claim 1, is characterized in that: described rubber band (3) is around laid along return capsule parachute hatchcover (1), return capsule (4) and rocket rocket body (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520407126.0U CN204767410U (en) | 2015-06-12 | 2015-06-12 | Anti - umbrella formula model rocket recoverable capsule separating mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520407126.0U CN204767410U (en) | 2015-06-12 | 2015-06-12 | Anti - umbrella formula model rocket recoverable capsule separating mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204767410U true CN204767410U (en) | 2015-11-18 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520407126.0U Expired - Fee Related CN204767410U (en) | 2015-06-12 | 2015-06-12 | Anti - umbrella formula model rocket recoverable capsule separating mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204767410U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113362692A (en) * | 2021-06-16 | 2021-09-07 | 中国人民解放军国防科技大学 | Teaching aid based on water rocket boosting glider |
-
2015
- 2015-06-12 CN CN201520407126.0U patent/CN204767410U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113362692A (en) * | 2021-06-16 | 2021-09-07 | 中国人民解放军国防科技大学 | Teaching aid based on water rocket boosting glider |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151118 Termination date: 20160612 |