CN103662102B - One is load lock tripper out of my cabin - Google Patents
One is load lock tripper out of my cabin Download PDFInfo
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- CN103662102B CN103662102B CN201310583673.XA CN201310583673A CN103662102B CN 103662102 B CN103662102 B CN 103662102B CN 201310583673 A CN201310583673 A CN 201310583673A CN 103662102 B CN103662102 B CN 103662102B
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- cabin
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- installing port
- lock
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Abstract
One is load lock tripper out of my cabin, for load out of my cabin and the mechatronics of load installing port and the unblock out of my cabin of space vehicle; Load comprises out of my cabin: locking roller, is arranged on the rear end of load side out of my cabin; Unlock roller, be arranged on the front end of side; Electric coupler, is arranged on the front side of load out of my cabin; Load installing port comprises out of my cabin: cavity, in order to accommodation chamber external load; Bussing connector, is arranged on the bottom surface of cavity, can be electrically connected with electric coupler; Rotary drive mechanism, is arranged on the side of cavity, the side, place of corresponding locking roller and unblock roller; Locking unlocks driving lever, and center is connected on rotary drive mechanism; Separate lock slide, connect one end that locking unlocks driving lever, separate on lock slide and be provided with one first guiding surface; Lock slider, connects the other end that locking unlocks driving lever, lock slider is provided with one second guiding surface.
Description
Technical field
The present invention relates to replaceable module locking-unlocking device, particularly one load lock tripper out of my cabin.
Background technology
Along with the raising day by day to space vehicle maintainability performance and functions expanding demand in-orbit, especially require at limited load space, weight range, and the operating equipment power output such as mechanical arm less when, load just can overcome connection resistance larger between the associate devices such as connector out of my cabin, realizes load and out of my cabin failure-free mechatronics the locking and unlocking between load installing port out of my cabin.
At present, space vehicle in-orbit maintainable and functions expanding aspects is in the pre research stage at initial stage, not yet there is ideal scheme can realize the mechanical arm relying on power output less, overcome load and larger between load installing port connection resistance out of my cabin out of my cabin, thus realize load and the reliable mechatronics the locking and unlocking out of my cabin between load installing port out of my cabin.Do not find explanation or the report of technology similar to the present invention at present, not yet collect similar data both at home and abroad yet.
Summary of the invention
The present invention is directed to prior art above shortcomings, less in order to solve existing machinery arm end power output, be difficult to overcome the problem of larger between load and space vehicle connection resistance out of my cabin, one load lock tripper is out of my cabin provided; Utilize the present invention, load and larger between load installing port connection resistance out of my cabin can be overcome out of my cabin, thus realize load and the reliable mechatronics the locking and unlocking out of my cabin between load installing port out of my cabin, and be convenient to the operations such as the follow-up secondary of load out of my cabin plug replacing.
The present invention is achieved through the following technical solutions:
One is load lock tripper out of my cabin, for load out of my cabin and the mechatronics of load installing port and the unblock out of my cabin of space vehicle;
Load comprises out of my cabin:
Locking roller, is arranged on the rear end of load side out of my cabin;
Unlock roller, be arranged on the front end of side;
Electric coupler, is arranged on the front side of load out of my cabin;
Load installing port comprises out of my cabin:
Cavity, in order to accommodation chamber external load;
Bussing connector, is arranged on the bottom surface of cavity, is electrically connected with electric coupler;
Rotary drive mechanism, is arranged on the side of cavity, the side, place of corresponding locking roller and unblock roller;
Locking unlocks driving lever, and its medium position is connected on rotary drive mechanism;
Separate lock slide, connect one end that locking unlocks driving lever, separate on lock slide and be provided with one first guiding surface;
Lock slider, connects the other end that locking unlocks driving lever, lock slider is provided with one second guiding surface;
In the locked state, rotary drive mechanism drives lock slider move to described locking roller, and the first guiding surface promotes to lock the internal motion of roller to load installing port out of my cabin, to overcome the connection resistance of electric coupler and Bussing connector and to play fixation;
In the unlocked state, rotary drive mechanism drives to be separated lock slide and move to described unblock roller, and the second guiding surface promotes the external movement of unblock roller to load installing port out of my cabin, to overcome the unblock resistance of electric coupler and Bussing connector.
Preferably, load installing port also comprises some guide-localizations wheel out of my cabin, is arranged on the both sides of load installing port inside out of my cabin, in order to play the guiding role.
Preferably, locking unblock driving lever and solution lock slide, lock slider are connected by finger.
Accompanying drawing explanation
Fig. 1 is the structural representation of the present invention's load lock tripper out of my cabin;
Fig. 2 be the present invention out of my cabin load enter the cutaway view of space vehicle load installing port out of my cabin;
Fig. 3 be the present invention out of my cabin load installing port catch the cutaway view of load out of my cabin;
Fig. 4 be the present invention out of my cabin load installing port lock the cutaway view of load out of my cabin;
Fig. 5 is the cutaway view that the present invention's load installing port preparation out of my cabin unlocks load out of my cabin;
Fig. 6 be the present invention out of my cabin load installing port unlock the cutaway view of load out of my cabin completely.
Detailed description of the invention
Below with reference to accompanying drawing of the present invention; clear, complete description and discussion are carried out to the technical scheme in the embodiment of the present invention; obviously; as described herein is only a part of example of the present invention; it is not whole examples; based on the embodiment in the present invention, the every other embodiment that those of ordinary skill in the art obtain under the prerequisite not making creative work, all belongs to protection scope of the present invention.
For the ease of the understanding to the embodiment of the present invention, be further explained for specific embodiment below in conjunction with accompanying drawing, and each embodiment does not form the restriction to the embodiment of the present invention.
As shown in the illustrated embodiment of fig. 1, the inventive system comprises the installing port of load out of my cabin 5 of load 1 and space vehicle out of my cabin.Load installing port 5 can be arranged on the position set by space vehicle according to demand out of my cabin, out of my cabin load 1 can be arranged in main service is in-orbit provided aircraft on.
As shown in Figure 1, load comprises out of my cabin: locking roller, is arranged on the rear end of load side out of my cabin; Unlock roller, be arranged on the front end of side; Electric coupler, is arranged on the front side of load out of my cabin;
Load installing port 5 comprises out of my cabin: cavity, in order to accommodation chamber external load; Bussing connector 11, is arranged on the bottom surface of cavity, is electrically connected with electric coupler 3; Rotary drive mechanism 9, is arranged on the side of cavity, the side, place of corresponding locking roller 2 and unblock roller 4; Locking unlocks driving lever 8, and its medium position is connected on rotary drive mechanism 9; Separate lock slide 6, connect one end that locking unlocks driving lever 8, separate on lock slide 6 and be provided with one first guiding surface; Lock slider 12, connects the other end that locking unlocks driving lever 8, lock slider 12 is provided with one second guiding surface;
Load 1 will be transferred to out of my cabin above load installing port 5 out of my cabin by the external device such as mechanical arm, and the application force moved downward will be provided;
Above-mentioned load out of my cabin 1 left upper end has locking roller 2, and lower-left end has unblock roller 4, has load electric coupler 3 out of my cabin in the middle of lower end;
In the present embodiment, load installing port 5 left upper end has lock slider 12 out of my cabin, lock slider 12 has lock slider finger 13, and lock slider finger 13 is arranged on locking and unlocks in the upper waist shaped hole of driving lever 8; Locking unlocks driving lever 8 middle part and is arranged on rotary drive mechanism 9; Load installing port 5 lower-left end has solution lock slide 6 out of my cabin, separates on lock slide 6 and has solution lock slide finger 7, separates lock slide finger 7 and is arranged in the lower waist shaped hole of locking unblock driving lever 8; Space vehicle is provided with guide-localization roller 10 in load installing port 5 cavity both sides out of my cabin; Space vehicle is provided with Bussing connector 11 in load installing port 5 cavity lower end out of my cabin.
Below the principle of work of apparatus of the present invention is described below:
When implementing to connect locking, load 1 load installing port 5 out of my cabin will be transferred to out of my cabin by external devices such as mechanical arms, and by the directional tagging of guiding surface be applied to the low-force that load 1 upper end is downward out of my cabin, just can under the guide-localization effect of load installing port 5 cavity both sides guide-localization roller 10 out of my cabin, enter into out of my cabin in load installing port 5 cavity smoothly, then, rotary drive mechanism 9 clickwise, lock slider finger 13 is driven to move right, thus drive lock slider 12 to move right simultaneously, and then under the effect on lock slider 12 inclined-plane, locking roller 2 vertical downward movement, load 1 out of my cabin is finally made to overcome larger between load electric coupler 3 and Bussing connector 11 connection resistance out of my cabin, realize the reliable mechatronics function out of my cabin between load 1 and space vehicle.
When implementing to unlock release, by rotary drive mechanism 9 left-hand revolution, solution lock slide finger 7 is driven to move right, thus drive solution lock slide 6 to move right simultaneously, and then under the effect of separating lock slide 6 inclined-plane, unlock roller 4 upward vertical movement, finally make load 1 out of my cabin overcome larger between load electric coupler 3 and Bussing connector 11 connection resistance out of my cabin, realize the reliable dynamo-electric unlocking function out of my cabin between load 1 and space vehicle.
For a more clear understanding of the present invention, below in conjunction with accompanying drawing, the working process that the invention process connects locking is described.
Fig. 2 is that load enters the cutaway view of space vehicle load installing port out of my cabin out of my cabin; Fig. 3 be space vehicle out of my cabin load installing port catch the cutaway view of load out of my cabin; Fig. 4 be space vehicle out of my cabin load installing port lock the cutaway view of load out of my cabin.
As shown in Figure 2, load 1 load installing port 5 out of my cabin will be transferred to out of my cabin by external devices such as mechanical arms, and by the directional tagging of guiding surface be applied to the low-force that load 1 upper end is downward out of my cabin, just can under the guide-localization effect of load installing port 5 cavity both sides guide-localization roller 10 out of my cabin, enter into out of my cabin in load installing port 5 cavity smoothly; Then, rotary drive mechanism 9 clickwise, drives lock slider finger 13 to move right, thus drives lock slider 12 to move right simultaneously, completes the catching load 1 out of my cabin of load installing port 5 out of my cabin, as shown in Figure 3; And then rotary drive mechanism 9 continues clickwise, and under the effect on lock slider 12 inclined-plane, locking roller 2 vertical downward movement, load 1 out of my cabin is finally made to overcome larger between load electric coupler 3 and Bussing connector 11 connection resistance out of my cabin, realize the reliable mechatronics function out of my cabin between load 1 and space vehicle, as shown in Figure 4.
Below in conjunction with accompanying drawing, the working process that the invention process unlocks release is described.
Fig. 5 is that load installing port prepares to unlock the cutaway view of load out of my cabin out of my cabin; Fig. 6 is that load installing port unlocks the cutaway view of load out of my cabin completely out of my cabin.
When implementing to unlock release, drive to lock by rotary drive mechanism 9 and unlock driving lever 8 left-hand revolution, and then drive solution lock slide finger 7 to move right, thus drive solution lock slide 6 to move right simultaneously, make to separate lock slide 6 and arrive the position preparing to unlock load 1 out of my cabin, as shown in Figure 5; Rotary drive mechanism 9 drives locking unblock driving lever 8 to continue left-hand revolution afterwards, make to separate lock slide 6 to continue to move right, and then under the effect of separating lock slide 6 inclined-plane, unlock roller 4 upward vertical movement, load 1 out of my cabin is finally made to overcome larger between load electric coupler 3 and Bussing connector 11 connection resistance out of my cabin, the reliable electromechanics realized out of my cabin between load 1 and space vehicle unlocks, as shown in Figure 6.Out of my cabin, load 1 detaches out of my cabin after load installing port 5 completely, drives locking to unlock driving lever 8 clickwise, just can realize the reset that lock slider 12 conciliates lock slide 6 by rotary drive mechanism 9, and final in position as shown in Figure 1, completes reset operation.
Owing to adopting technique scheme, load space vehicle load installing port out of my cabin will be transferred to out of my cabin by external devices such as mechanical arms, and by the directional tagging of guiding surface be applied to the low-force that load upper end is downward out of my cabin, just can under the guide-localization effect of space vehicle load installing port cavity both sides guide-localization roller out of my cabin, enter into space vehicle smoothly out of my cabin in load installing port cavity, then, rotary drive mechanism clickwise, lock slider finger is driven to move right, thus drive lock slider to move right simultaneously, and then under the effect on lock slider inclined-plane, locking roller vertical downward movement, load out of my cabin is finally made to overcome larger between load electric coupler and Bussing connector connection resistance out of my cabin, to realize out of my cabin between load with space vehicle reliable is electrically connected and mechanical connection.Simultaneously, rotary drive mechanism left-hand revolution can be passed through, solution lock slide finger is driven to move right, thus drive solution lock slide to move right simultaneously, and then under the effect unlocking slide block inclined-plane, unlock roller upward vertical movement, finally make load out of my cabin overcome larger between load electric coupler and Bussing connector connection resistance out of my cabin, the reliable electromechanics realized out of my cabin between load and space vehicle unlocks.Therefore, the present invention not only can realize reliable out of my cabin between load installing port of load and space vehicle out of my cabin and be electrically connected and mechanical connection, and failure-free electrical connection can be realized and be mechanically connected removing, this device has the beneficial effects such as principle is simple, production and processing is convenient simultaneously.
The above; be only the present invention's preferably detailed description of the invention, but protection scope of the present invention is not limited thereto, is anyly familiar with those skilled in the art in the technical scope that the present invention discloses; the change that can expect easily or replacement, all should be encompassed within protection scope of the present invention.Therefore, protection scope of the present invention should be as the criterion with the protection domain of claim.
Claims (3)
1. a load lock tripper out of my cabin, for load out of my cabin and the mechatronics of load installing port and the unblock out of my cabin of space vehicle, is characterized in that:
Described load out of my cabin comprises:
Locking roller, the rear end of load side out of my cabin described in being arranged on;
Unlock roller, be arranged on the front end of described side;
Electric coupler, the front side of load out of my cabin described in being arranged on;
The described installing port of load out of my cabin comprises:
Cavity, in order to load out of my cabin described in holding;
Bussing connector, is arranged on the bottom surface of described cavity, is electrically connected with described electric coupler;
Rotary drive mechanism, is arranged on the side of described cavity, the side, place of corresponding described locking roller and described unblock roller;
Locking unlocks driving lever, and its medium position is connected on described rotary drive mechanism;
Separate lock slide, connect one end that described locking unlocks driving lever, described solution lock slide is provided with one first guiding surface;
Lock slider, connects the other end that described locking unlocks driving lever, described lock slider is provided with one second guiding surface;
In the locked state, described rotary drive mechanism drives described lock slider to move to described locking roller, described first guiding surface promotes the internal motion of described locking roller to the described installing port of load out of my cabin, to overcome the connection resistance of described electric coupler and described Bussing connector and to play fixation;
In the unlocked state, described rotary drive mechanism drives described solution lock slide to move to described unblock roller, described second guiding surface promotes the external movement of described unblock roller to the described installing port of load out of my cabin, to overcome the unblock resistance of described electric coupler and described Bussing connector.
2. the tripper of load lock out of my cabin according to claim 1, is characterized in that, the described installing port of load out of my cabin also comprises some guide-localizations wheel, and the both sides of load installing port inside out of my cabin described in being arranged on, in order to play the guiding role.
3. the tripper of load lock out of my cabin according to claim 1, is characterized in that, described locking is unlocked driving lever and is connected by finger with described solution lock slide, lock slider.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310583673.XA CN103662102B (en) | 2013-11-20 | 2013-11-20 | One is load lock tripper out of my cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310583673.XA CN103662102B (en) | 2013-11-20 | 2013-11-20 | One is load lock tripper out of my cabin |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103662102A CN103662102A (en) | 2014-03-26 |
| CN103662102B true CN103662102B (en) | 2015-08-12 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201310583673.XA Active CN103662102B (en) | 2013-11-20 | 2013-11-20 | One is load lock tripper out of my cabin |
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Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104058108B (en) * | 2014-05-30 | 2015-12-30 | 北京控制工程研究所 | A kind of satellite is independently annotated in-orbit and is used docking mechanism actuating device |
| CN111196381B (en) * | 2020-01-14 | 2021-08-13 | 中国科学院空间应用工程与技术中心 | Self-positioning load adapter |
| CN112758356B (en) * | 2020-12-28 | 2022-02-22 | 中国科学院长春光学精密机械与物理研究所 | Optical load positioning and locking system |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4971474A (en) * | 1990-03-30 | 1990-11-20 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Quick connect coupling |
| RU2342290C1 (en) * | 2007-06-22 | 2008-12-27 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" | Unit separation mechanism |
| CN103231813A (en) * | 2013-04-16 | 2013-08-07 | 北京航空航天大学 | Shape memory alloy (SMA) group rolling rod type large load releasing mechanism |
-
2013
- 2013-11-20 CN CN201310583673.XA patent/CN103662102B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4971474A (en) * | 1990-03-30 | 1990-11-20 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Quick connect coupling |
| RU2342290C1 (en) * | 2007-06-22 | 2008-12-27 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" | Unit separation mechanism |
| CN103231813A (en) * | 2013-04-16 | 2013-08-07 | 北京航空航天大学 | Shape memory alloy (SMA) group rolling rod type large load releasing mechanism |
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| CN103662102A (en) | 2014-03-26 |
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