CN103419945A - Impact injection type star soil diving device with escapement mechanism - Google Patents
Impact injection type star soil diving device with escapement mechanism Download PDFInfo
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- CN103419945A CN103419945A CN2013103869461A CN201310386946A CN103419945A CN 103419945 A CN103419945 A CN 103419945A CN 2013103869461 A CN2013103869461 A CN 2013103869461A CN 201310386946 A CN201310386946 A CN 201310386946A CN 103419945 A CN103419945 A CN 103419945A
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Abstract
The invention provides an impact injection type star soil diving device with an escapement mechanism. The impact injection type star soil diving device is characterized in that the diving device mainly consists of a diving shell, an impact counterweight, an energy storage spring, a buffer spring, the escapement mechanism and a driving unit. The diving device has the beneficial effects of exquisite structure, reasonable design, automatic control operation and smooth and steady working process and is specially designed for star surface detection to be used.
Description
Technical field:
The present invention relates to celestial body detecting devices technical field, refer in particular to a kind of impact penetration type star earth of escapement that utilizes and slip into device.
Background technology:
Through the development of 51 years, China's aerospace industry formed six abilities---enter ability, satellite R&D capability, manned space flight ability, survey of deep space ability, space flight basis and the supportability in space, and the satellite application ability.The ability of survey of deep space, implementing moon exploration project is the first step that China steps to survey of deep space.This engineering divides three phases to implement.At first stage, be transmitted in the moonik of 200 kilometers orbital motions of the moon---Chang'e 1, its task is to take the menology 3-d photographs, analyzes the distribution of multiple element on the moon, surveys lunar soil thickness, surveys the cislunar space environment.After completing the first stage engineering, will implement second, third stage engineering, and about 2013, complete the lunar surface soft landing and survey; Before the year two thousand twenty, launch small-sized sampling recoverable module, gather moon sample Returning ball, carry out in-depth study.This just needs a kind of instrument that the surface injection is surveyed for celestial body.
Summary of the invention:
The present invention aims to provide a kind of can the realization and surveys and automatically slip into the injection submersible that carries out detection mission below catalog of celestial bodies number of plies rice and automatically slip into device for objects outside Earth, specifically refers to that a kind of impact penetration type star earth of escapement that utilizes slips into device.
The objective of the invention is to realize as follows:
A kind of impact penetration type star earth of escapement that utilizes slips into device, and it is characterized in that: this slips into device and mainly is comprised of dive shell, impact weights, energy stroage spring, recoil spring, escapement, driver element;
The dive shell is closure casing, and head is taper, is conducive to the injection dive; Impact weights, under driver element and energy stroage spring effect, is controlled the hoisting depth energy storage and is thrown off realization shock housing by escapement; Energy stroage spring is the impact weights stored energy; Escapement is comprised of the nut of snap hook, wedge-shaped catch and special shape, to realize that nut and snap hook are chimeric and to disconnect; Driver element mainly is comprised of reducing motor, coupler, screw rod, for slipping into device, provides power; This slips into the required electric energy of device and signal transmits by the cable that slips into the device tail end;
The dive shell is comprised of conical head, lower case, central enclosure, upper body, slideway and upper cover, and the whole mechanism that slips into all is wrapped in housing;
Impact weights and snap hook are fixed together, and the symmetrical sliding tray of twice is arranged, and are limited in the slideway of housing, can only prolong slideway and slide up and down; Center has the rectangle slotted hole, and stop nut slides up and down in hole, and when screw rod rotates, nut moves up and down, thereby pulls the energy storage of impact weights lifting implementation;
Energy stroage spring compressed and energy storage when impact weights promotes, clashing into conehead for impact weights provides kinetic energy;
The collision time that recoil spring delays driver element while upwards impacting, the impact that reducing mechanism makes progress greatly;
Escapement is core of the present invention, mainly wedge-shaped catch, snap hook, special shape nut, stop nut part, consists of, and realizes the chimeric of nut and snap hook and throws off along with nut moves up and down, thereby complete weight energy storage and shock;
Driver element mainly is comprised of reducing motor, coupler, screw rod, and for the whole device that slips into provides power resources, this unit can only limit in certain position and move up and down, with the impulsive force slowed down under the recoil spring combined action upwards.
The invention has the beneficial effects as follows: delicate structure, reasonable in design, running is controlled in automation, and working process is steadily smooth, for the design of celestial body probing surface, uses specially.
The accompanying drawing explanation:
Fig. 1 is structural representation of the present invention;
In figure: slip into 1, weight 2, stop nut 3, lower case 4, snap hook 5, slideway 6, centre housing 7, coupler 8, upper body 9, upper cover 10, reducing motor 11, block 12, nut 13, screw rod 14.
The specific embodiment:
With reference to accompanying drawing, a kind of impact penetration type star earth of escapement that utilizes slips into device, and it is characterized in that: this slips into device and mainly is comprised of dive shell, impact weights, energy stroage spring, recoil spring, escapement, driver element;
The dive shell is closure casing, and head is taper, is conducive to the injection dive; Impact weights 2, under driver element and energy stroage spring effect, is controlled the hoisting depth energy storage and is thrown off realization shock housing by escapement; Energy stroage spring is impact weights 2 stored energy; Escapement is comprised of the nut 13 of snap hook 5, wedge-shaped catch 12 and special shape, to realize that nut 13 and snap hook 5 are chimeric and to disconnect; Driver element mainly is comprised of reducing motor 11, coupler 8, screw rod 14, for slipping into device, provides power; This slips into the required electric energy of device and signal transmits by the cable that slips into the device tail end;
The dive shell is comprised of conical head, lower case 4, central enclosure 7, upper body 9, slideway 6 and upper cover 10, and the whole mechanism that slips into all is wrapped in housing.
Impact weights 2 is fixed together with snap hook 5, and the symmetrical sliding tray of twice is arranged, and is limited in the slideway 6 of housing, can only prolong slideway 6 and slide up and down; Center has the rectangle slotted hole, and stop nut 3 slides up and down in hole, and when screw rod 14 rotation, nut 13 moves up and down, thereby pulls the energy storage of impact weights lifting implementation;
Energy stroage spring compressed and energy storage when impact weights promotes, clashing into conehead for impact weights provides kinetic energy;
The collision time that recoil spring delays driver element while upwards impacting, the impact that reducing mechanism makes progress greatly;
Escapement mainly is comprised of wedge-shaped catch 12, snap hook 5, special shape nut 13, stop nut 3 parts, realizes nut 13 and the chimeric of snap hook 5 and disengagement along with nut 13 moves up and down, thereby completes weight energy storage and shock;
Driver element mainly is comprised of reducing motor 11, coupler 8, screw rod 14, and for the whole device that slips into provides power resources, this unit can only limit in certain position and move up and down, with the impulsive force slowed down under the recoil spring combined action upwards.
This invention motion flow is as follows:
1, the right biography of reducing motor 11, connecting screw rod 14 rotations, nut 13 moves up, and snap hook 5 is chimeric with nut, drives weight 2 and moves up.The compressed energy storage of energy stroage spring.
When 2, weight rises to wedge-shaped catch 12, snap hook 5 outwards push open with nut 13 throw off make weight 2 under energy stroage spring promotes rapidly down sliding with slip into 1 and clash into a dive.Reducing motor 11, screw rod 14 etc. move up under reaction force acts simultaneously, and recoil spring is compressed.
3, motor loses load, and winding current reduces rapidly, and control unit is controlled motor commutation and turned left, and nut 13 moves down.Reducing motor 11 is got back to initial position under the recoil spring effect simultaneously.
When 4, nut moves to certain position, the inclined-plane, lower end starts gradually snap hook 5 outwards to be pushed open, then continues to move down inclined-plane and snap hook 5 disengagements, and snap hook 5 resets, chimeric with nut 13.Nut 13 is subject to stop nut 3 to be stopped, motor load increases sharply, and winding current increases rapidly, and control unit is controlled motor commutation and turned right, and carries out next working cycle.
Claims (1)
1. one kind is utilized the impact penetration type star earth of escapement to slip into device, and it is characterized in that: this slips into device and mainly is comprised of dive shell, impact weights, energy stroage spring, recoil spring, escapement, driver element;
The dive shell is closure casing, and head is taper, is conducive to the injection dive; Impact weights (2), under driver element and energy stroage spring effect, is controlled the hoisting depth energy storage and is thrown off realization shock housing by escapement; Energy stroage spring is impact weights (2) stored energy; Escapement is comprised of the nut (13) of snap hook (5), wedge-shaped catch (12) and special shape, to realize that nut (13) and snap hook (5) are chimeric and to disconnect; Driver element mainly is comprised of reducing motor (11), coupler (8), screw rod (14), for slipping into device, provides power; This slips into the required electric energy of device and signal transmits by the cable that slips into the device tail end;
The dive shell is comprised of conical head, lower case (4), central enclosure (7), upper body (9), slideway (6) and upper cover (10), and the whole mechanism that slips into all is wrapped in housing;
Impact weights (2) is fixed together with snap hook (5), and the symmetrical sliding tray of twice is arranged, and is limited in the slideway (6) of housing, can only prolong slideway (6) and slide up and down; Center has the rectangle slotted hole, and stop nut (3) slides up and down in hole, and when screw rod (14) rotates, nut (13) moves up and down, thereby pulls the energy storage of impact weights lifting implementation;
Energy stroage spring compressed and energy storage when impact weights promotes, clashing into conehead for impact weights provides kinetic energy;
The collision time that recoil spring delays driver element while upwards impacting, the impact that reducing mechanism makes progress greatly;
Escapement mainly is comprised of wedge-shaped catch (12), snap hook (5), special shape nut (13), stop nut (3) part, realize nut (13) and the chimeric of snap hook (5) and disengagement along with nut (13) moves up and down, thereby complete weight energy storage and shock;
Driver element mainly is comprised of reducing motor (11), coupler (8), screw rod (14), and for the whole device that slips into provides power resources, this unit can only limit in certain position and move up and down, with the impulsive force slowed down under the recoil spring combined action upwards.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310386946.1A CN103419945B (en) | 2013-08-30 | 2013-08-30 | A kind of impact penetration type star earth of escapement that utilizes slips into device |
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| CN201310386946.1A CN103419945B (en) | 2013-08-30 | 2013-08-30 | A kind of impact penetration type star earth of escapement that utilizes slips into device |
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| CN103419945A true CN103419945A (en) | 2013-12-04 |
| CN103419945B CN103419945B (en) | 2016-01-20 |
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Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104149993A (en) * | 2014-08-06 | 2014-11-19 | 哈尔滨工业大学 | Biomimetic wriggle tunneling type planetary exploration submergence device |
| CN105929140A (en) * | 2016-07-11 | 2016-09-07 | 中国科学院沈阳自动化研究所 | High-speed impacting penetrator structure for detecting lunar soil |
| CN106428654A (en) * | 2016-11-17 | 2017-02-22 | 上海卫星工程研究所 | Small-sized split type survivable deep space impactor |
| CN106516178A (en) * | 2016-11-17 | 2017-03-22 | 上海卫星工程研究所 | Series module combining type common impactor configuration |
| CN106742078A (en) * | 2016-11-23 | 2017-05-31 | 上海卫星工程研究所 | One kind inflation allosteric type has air celestial body impact probing device from outside deceleration ground |
| CN107826272A (en) * | 2017-10-30 | 2018-03-23 | 哈尔滨工业大学 | One kind impact penetration type slips into device |
| CN108750150A (en) * | 2018-06-19 | 2018-11-06 | 上海卫星工程研究所 | It is a kind of to invade deep small-sized shock penetration device greatly towards super thick ice sheet |
| CN109131957A (en) * | 2018-06-19 | 2019-01-04 | 上海卫星工程研究所 | A kind of deployable objects outside Earth penetration limiting device |
| CN109187072A (en) * | 2018-09-26 | 2019-01-11 | 哈尔滨工业大学 | A kind of impact penetration type star earth section flexibility stock rod |
| CN111547269A (en) * | 2020-04-21 | 2020-08-18 | 哈尔滨工业大学 | Asteroid exploration bomb spin-on release device |
| CN111731511A (en) * | 2020-07-31 | 2020-10-02 | 北京控制与电子技术研究所 | Data rescue system applied to extraterrestrial celestial body detector |
| CN113267367A (en) * | 2020-02-17 | 2021-08-17 | 哈尔滨工业大学 | Two-side clamping type impact actuating device |
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Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104149993A (en) * | 2014-08-06 | 2014-11-19 | 哈尔滨工业大学 | Biomimetic wriggle tunneling type planetary exploration submergence device |
| CN105929140A (en) * | 2016-07-11 | 2016-09-07 | 中国科学院沈阳自动化研究所 | High-speed impacting penetrator structure for detecting lunar soil |
| CN105929140B (en) * | 2016-07-11 | 2018-11-02 | 中国科学院沈阳自动化研究所 | A kind of high-speed impact penetration device structure for lunar soil detection |
| CN106428654A (en) * | 2016-11-17 | 2017-02-22 | 上海卫星工程研究所 | Small-sized split type survivable deep space impactor |
| CN106516178A (en) * | 2016-11-17 | 2017-03-22 | 上海卫星工程研究所 | Series module combining type common impactor configuration |
| CN106742078A (en) * | 2016-11-23 | 2017-05-31 | 上海卫星工程研究所 | One kind inflation allosteric type has air celestial body impact probing device from outside deceleration ground |
| CN107826272A (en) * | 2017-10-30 | 2018-03-23 | 哈尔滨工业大学 | One kind impact penetration type slips into device |
| CN107826272B (en) * | 2017-10-30 | 2020-06-30 | 哈尔滨工业大学 | Impact penetration type submersible diving device |
| CN109131957A (en) * | 2018-06-19 | 2019-01-04 | 上海卫星工程研究所 | A kind of deployable objects outside Earth penetration limiting device |
| CN108750150A (en) * | 2018-06-19 | 2018-11-06 | 上海卫星工程研究所 | It is a kind of to invade deep small-sized shock penetration device greatly towards super thick ice sheet |
| CN109187072A (en) * | 2018-09-26 | 2019-01-11 | 哈尔滨工业大学 | A kind of impact penetration type star earth section flexibility stock rod |
| CN109187072B (en) * | 2018-09-26 | 2020-04-24 | 哈尔滨工业大学 | Impact injection type star soil profile flexible stock rod |
| CN113267367A (en) * | 2020-02-17 | 2021-08-17 | 哈尔滨工业大学 | Two-side clamping type impact actuating device |
| CN111547269A (en) * | 2020-04-21 | 2020-08-18 | 哈尔滨工业大学 | Asteroid exploration bomb spin-on release device |
| CN111547269B (en) * | 2020-04-21 | 2021-06-15 | 哈尔滨工业大学 | Asteroid exploration bomb spin-on release device |
| CN111731511A (en) * | 2020-07-31 | 2020-10-02 | 北京控制与电子技术研究所 | Data rescue system applied to extraterrestrial celestial body detector |
| CN111731511B (en) * | 2020-07-31 | 2020-11-17 | 北京控制与电子技术研究所 | Data rescue system applied to extraterrestrial celestial body detector |
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