CN103700983A - Air conditioner air supply connector - Google Patents
Air conditioner air supply connector Download PDFInfo
- Publication number
- CN103700983A CN103700983A CN201210366963.4A CN201210366963A CN103700983A CN 103700983 A CN103700983 A CN 103700983A CN 201210366963 A CN201210366963 A CN 201210366963A CN 103700983 A CN103700983 A CN 103700983A
- Authority
- CN
- China
- Prior art keywords
- connector
- air
- connector construction
- conditioning
- adapter
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Landscapes
- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
The invention discloses an air conditioner air supply connector. The air conditioner air supply connector comprises a connector structure, a locking device, an adapter, a guy rope and an air cylinder, wherein the connector structure is connected with the wall of the rocket body of a rocket in a sealing way; the locking device is positioned on the connector and used for locking the connector on the rocket body; the adapter is connected with the locking device; the guy rope is connected with the adapter and controls the motion of the adapter; the adapter controls the motion of the locking device; the connector structure is controlled to be locked with or fall off the rocket body through the motion of the locking device controls; and the air cylinder is connected with the guy rope and controls the motion of the guy rope, so that the air conditioner air supply connector can be automatically locked and automatically fall off, and meets requirements of certain carrier rockets.
Description
Technical field
The present invention relates to satellite Temperature and Humidity Control technical field, relate in particular to a kind of air-conditioning connector.
Background technology
Air-conditioning connector is to blow in fairing of launch vehicle, guarantees the important jockey of the humiture of satellite in radome fairing.The air-conditioning connector of tradition model is mainly to adopt the locking of manual 8 lids lock, and at the first five device of taking manually to come off for ten minutes of transmitting.
Yet at present some carrier rockets require air-conditioning connector can adapt to whole rocket body by level to the vertical perpendicular process that rises, and need to satisfiedly launch the requirements such as fast and flexible.These complicated working condition requirements have proposed very high requirement to the reliable lock of connector, Automatic-falling, and traditional air-conditioning connector cannot meet these requirements
In view of above problem, be necessary air-conditioning connector to improve.
Summary of the invention
The object of the present invention is to provide a kind of air-conditioning connector, to solve existing air-conditioning connector, can not meet the difficult problem that reliable lock and Automatic-falling etc. require.
For addressing the above problem, the present invention proposes a kind of air-conditioning connector, for blowing in fairing of launch vehicle, comprising:
Connector construction, is tightly connected with the arrow wall of described rocket rocket body;
Locking device, is positioned on described connector construction, for described connector construction being locked to described rocket rocket body;
Adapter, is connected with described locking device;
Stay cord, is connected with described adapter, and described stay cord is controlled the motion of described adapter, and described adapter is controlled the motion of described locking device, described in the motion control of described locking device the locking of connector construction and described rocket rocket body with come off;
Cylinder, is connected with described stay cord, controls the motion of described stay cord.
Described connector construction is connected with the arrow wall of described rocket rocket body by upper bracket and undersetting, and described upper bracket and described undersetting are arranged on described rocket body.
Described upper bracket and described undersetting are all furnished with two screwed holes and two pin-and-holes, are connected mutually respectively by screw with alignment pin and rocket body.
The quantity of described upper bracket is one, and the quantity of described undersetting is two.
Described connector construction has two supporting legs, described two supporting legs and described two undersettings assembling.
On the supporting leg of described connector construction, guide finger is housed, described undersetting is provided with the gathering sill mating with described guide finger.
Described locking device comprises torsion spring and latch hook, and described torsion spring is connected with described adapter, and described latch hook is connected with described torsion spring, and described torsion spring is controlled described latch hook and hooked or depart from described upper bracket.
On described connector construction, be welded with guide vane end stop, described guide vane end stop limits the motion of described adapter.
Magnet steel head is installed on described upper bracket, on described connector construction, fills magnetic red transducer.
On described arrow wall, post rubber seal with the interface of connector construction.
Six bafflers are set on described connector construction, and described baffler and described connector construction weld together, and become miter angle upwards with connector construction counterface.
Compared with prior art, air-conditioning connector provided by the invention has following advantage and good effect:
(1) by locking device, adapter, stay cord and cylinder are set, thereby make the air-conditioning connector of the present invention can auto lock and come off;
(2), by the U-lag coordinating with the rotating shaft of undersetting is set on two supporting legs of connector construction, can prevents that supporting leg left and right in horizontal plane of connector construction from beating, thereby make air-conditioning connector of the present invention there is anti-jumping design; And on undersetting, leave gathering sill, anti-jumping guide finger is housed on the supporting leg of connector construction, thereby can prevent that rocket body from playing connector in perpendicular process and being subject to the power of upwards beating or vibration force to overcome the release of torsion spring power;
(3) by be welded with guide vane end stop on connector construction, thereby when torsion spring moment of torsion approaches stall torque, the adapter being connected with latch hook is encountered guide vane end stop, thereby protection torsion spring overload destruction makes air-conditioning connector of the present invention have torsion spring reliability design;
(4) consider bearing can with connector accommodation, each bearing of upper undersetting is all furnished with two screwed holes and by screw, is connected mutually with alignment pin and rocket body structure respectively with two pin-and-holes, thereby can accurately locate;
(5) on arrow wall, post a circle rubber seal with the interface of connector construction, during locking, connector compresses rubber seal (decrement 1.5mm during design locking), thereby guarantees to seal between connector construction and rocket body;
(6) mounting magnetic steel head on upper bracket on arrow, fills magnetic red transducer on connector construction, when transducer two parts end face over against, transducer now circuit disconnects; When connector is separated with rocket body, the separation of staggering of transducer two parts, transducer is power on circuitry all, and the connector signal lamp that comes off is bright, thereby has signal feedback design;
(7)by 6 bafflers are set on connector construction, baffler and connector construction weld together, and become miter angle upwards, thereby can prevent that air-conditioning from directly blowing satellite with connector construction counterface.
Accompanying drawing explanation
The structure chart of the air-conditioning connector that Fig. 1 provides for the embodiment of the present invention;
The upper bracket matching design that Fig. 2 provides for the embodiment of the present invention;
The undersetting matching design that Fig. 3 provides for the embodiment of the present invention.
Embodiment
Air-conditioning connector the present invention being proposed below in conjunction with the drawings and specific embodiments is described in further detail.According to the following describes and claims, advantages and features of the invention will be clearer.It should be noted that, accompanying drawing all adopts very the form of simplifying and all uses non-ratio accurately, only for convenient, the object of the aid illustration embodiment of the present invention lucidly.
Core concept of the present invention is, a kind of air-conditioning connector is provided, and comprising: connector construction, is tightly connected with the arrow wall of described rocket rocket body; Locking device, is positioned on described connector construction, for described connector construction being locked to described rocket rocket body; Adapter, is connected with described locking device; Stay cord, is connected with described adapter, and described stay cord is controlled the motion of described adapter, and described adapter is controlled the motion of described locking device, described in the motion control of described locking device the locking of connector construction and described rocket rocket body with come off; Cylinder, is connected with described stay cord, controls the motion of described stay cord; Thereby make the air-conditioning connector provided by the invention can auto lock and come off, meet the requirement of some carrier rocket.
Please refer to Fig. 1 to Fig. 3, wherein, the structure chart of the air-conditioning connector that Fig. 1 provides for the embodiment of the present invention, the upper bracket matching design that Fig. 2 provides for the embodiment of the present invention, the undersetting matching design that Fig. 3 provides for the embodiment of the present invention, as shown in Figure 1 to Figure 3, the air-conditioning connector that the present invention proposes, for blowing in fairing of launch vehicle, comprising:
Locking device, is positioned on described connector construction 12, for described connector construction 12 is locked to described rocket rocket body;
Adapter 9, is connected with described locking device;
Stay cord 11, is connected with described adapter 9, and described stay cord 11 is controlled the motion of described adapter 9, and described adapter 9 is controlled the motion of described locking device, described in the motion control of described locking device the locking of connector construction 12 and described rocket rocket body with come off;
Cylinder, is connected with described stay cord 11, controls the motion of described stay cord 11.
Described connector construction 12 is connected with the arrow wall 1 of described rocket rocket body by upper bracket 2 and undersetting 7, and described upper bracket 2 and described undersetting 7 are arranged on described rocket body.Described upper bracket 2 is all furnished with two screwed holes and two pin-and-holes with described undersetting 7, is connected mutually respectively by screw with alignment pin and rocket body.The quantity of described upper bracket 2 is one, and the quantity of described undersetting 7 is two.Described connector construction 12 has two supporting legs, described two supporting legs and 7 assemblings of described two undersettings.
On the supporting leg of described connector construction 12, guide finger is housed, described undersetting 7 is provided with the gathering sill mating with described guide finger.
Described locking device comprises torsion spring 4 and latch hook 3, and described torsion spring 4 is connected with described adapter 9, and described latch hook 3 is connected with described torsion spring 4, and described torsion spring 4 is controlled described latch hook 3 and hooked or depart from described upper bracket 2.
On described connector construction 12, be welded with guide vane end stop 10, the motion of the described adapter 9 of described guide vane end stop 10 restriction.
On described upper bracket 2, magnet steel head 8 is installed, on described connector construction 12, fills magnetic red transducer 5.
On described arrow wall, post rubber seal with the interface of connector construction 12.
Six bafflers 6 are set on described connector construction 12, and described baffler 6 welds together with described connector construction 12, becomes miter angle upwards with connector construction 12 counterfaces.
Therefore, on the whole, air-conditioning connector provided by the invention is considered the design of following aspect:
1) lock the design that comes off
By torsion spring 4 effects, latch hook 3 is hooked the upper bracket 2 being fixed on arrow, latch hook 3 is locked at connector construction 12 on rocket body.Connector is when locking state, stay cord 11 is not subject to pulling force, Fig. 3 as shown in Figure 1, Figure 2,, under the effect of whole connector upper bracket 2 levels power and deadweight left on arrow, around the moment of flexure balance of the undersetting point of rotation, (on arrow, upper bracket 2 is positioned on same level line with the pivot of latch hook 3, therefore the turning moment of deadweight and torsion spring 4 coupling mechanism forces are irrelevant, only by bearing horizontal pull balance).
During release, by cylinder, pull stay cord, make latch hook 3 releases, connector is separated with rocket body with under Action of Gravity Field at stay cord 11 pulling force.
2) Seal Design
On arrow wall 1, post a circle rubber seal with the interface of connector construction 12, during locking, connector compresses between rubber seal (decrement 1.5mm during design locking) assurance connector construction and rocket body and seals.
3) signal feedback design
On arrow, mounting magnetic steel head 8 on upper bracket 2, fills magnetic red transducer 5 on connector construction 12, transducer two parts end face over against, transducer now circuit disconnect; When connector is separated with rocket body, the separation of staggering of transducer two parts, transducer is power on circuitry all, and the connector signal lamp that comes off is bright.
4) water conservancy diversion form design
For preventing that air-conditioning from directly blowing satellite, 6 bafflers are set on connector construction 12.Baffler and connector construction weld together, and become miter angle upwards with connector construction counterface.
5) anti-jumping design
Two supporting legs at connector construction 12 can prevent from beating about connector supporting leg is in horizontal plane with the U-lag coordinating of the rotating shaft of undersetting 7, as Fig. 3.
On undersetting 7, leave gathering sill, as Fig. 1, anti-jumping guide finger 13 is housed on the supporting leg of connector construction 12, can prevent that rocket body from playing connector in perpendicular process and being subject to the power of upwards beating or vibration force to overcome the release of torsion spring power.
6) torsion spring reliability design
Excessive for preventing stay cord 11 pulling force; if pulling force surpasses the torsion spring limit, can destroy torsion spring 4, on connector construction, be welded with guide vane end stop 10, when torsion spring 4 moments of torsion approach stall torque; the adapter being connected with latch hook 3 is encountered guide vane end stop 10, thereby protection torsion spring 4 overloads are destroyed.
7) connector arrow upper bracket mount scheme design
On connector arrow, part is mainly comprised of a upper bracket 2 and two undersettings 7.Consider bearing can with connector accommodation, each bearing of upper undersetting is all furnished with two screwed holes and two pin-and-holes respectively by screw be connected mutually with alignment pin and rocket body structure (wherein first use screw pre-determined bit, after pre-add-in connectors completes, squeeze into alignment pin and accurately locate).
And the operating process of air-conditioning connector provided by the invention is as follows:
1) upper and lower bearing is installed
First according to drawing requirement drilling screw on rocket body arrow wall 1, the through hole of use is installed, after brill is good, is installed bearing 2, undersetting 7, with screw, assemble; Again two supporting legs of connector construction 12 are aimed to two undersettings 7 and assemble, then promote connector construction and upwards rotate around undersetting 7; Pull stay cord 11, allow latch hook not run into upper bracket 2, when the sealing ring on connector construction 12 and arrow wall 1 is adjacent to, unclamp stay cord 11, latch hook enters in the groove of upper bracket, connector locking; The position of undersetting in inching (screw is installed between through hole and screw and existed gap to finely tune bearing), after having adjusted, joins brill alignment pin location to arrow wall 1 and upper bracket 2, undersetting 7 on request.Then tighten screw, upper undersetting installation.
2) locking
Two supporting legs of connector construction 12 are aimed to two undersettings 7 and assemble, then promote connector construction and upwards rotate around undersetting 7; Pull stay cord 11, allow latch hook not run into upper bracket 2, when the sealing ring on connector construction 12 and arrow wall 1 is adjacent to, unclamp stay cord 11, latch hook enters in the groove of upper bracket, connector locking.Now, magnetic red transducer 5 approaches with magnet steel head 8, and the signal lamp that comes off goes out.
3) come off
Distribution platform by Long-distance Control is to the cylinder air feed that comes off, and cylinder pulls stay cord 11, and stay cord 11 band moveable lock hooks 3 overcome torsion spring 4 torsional moment releases.After release, because latch hook 3 and limited 10 of adapter 9 block, so torsion spring and latch hook no longer rotate, and stay cord 11 pulling force produce and make a concerted effort to make connector separated with undersetting 7 together with connector, pipeline gravity, complete connector and come off.Meanwhile, magnetic red transducer 5 is separated with magnet steel head 8, and the ground signal lamp that comes off is bright.
In sum, the invention provides a kind of air-conditioning connector, comprising: connector construction, is tightly connected with the arrow wall of described rocket rocket body; Locking device, is positioned on described connector construction, for described connector construction being locked to described rocket rocket body; Adapter, is connected with described locking device; Stay cord, is connected with described adapter, and described stay cord is controlled the motion of described adapter, and described adapter is controlled the motion of described locking device, described in the motion control of described locking device the locking of connector construction and described rocket rocket body with come off; Cylinder, is connected with described stay cord, controls the motion of described stay cord; Thereby make the air-conditioning connector provided by the invention can auto lock and come off, meet the requirement of some carrier rocket.
Obviously, those skilled in the art can carry out various changes and modification and not depart from the spirit and scope of the present invention invention.Like this, if within of the present invention these are revised and modification belongs to the scope of the claims in the present invention and equivalent technologies thereof, the present invention is also intended to comprise these changes and modification interior.
Claims (11)
1. an air-conditioning connector, for blowing in fairing of launch vehicle, is characterized in that, comprising:
Connector construction, is tightly connected with the arrow wall of described rocket rocket body;
Locking device, is positioned on described connector construction, for described connector construction being locked to described rocket rocket body;
Adapter, is connected with described locking device;
Stay cord, is connected with described adapter, and described stay cord is controlled the motion of described adapter, and described adapter is controlled the motion of described locking device, described in the motion control of described locking device the locking of connector construction and described rocket rocket body with come off;
Cylinder, is connected with described stay cord, controls the motion of described stay cord.
2. air-conditioning connector as claimed in claim 1, is characterized in that, described connector construction is connected with the arrow wall of described rocket rocket body by upper bracket and undersetting, and described upper bracket and described undersetting are arranged on described rocket body.
3. air-conditioning connector as claimed in claim 2, is characterized in that, described upper bracket and described undersetting are all furnished with two screwed holes and two pin-and-holes, are connected mutually respectively by screw with alignment pin and rocket body.
4. air-conditioning connector as claimed in claim 2, is characterized in that, the quantity of described upper bracket is one, and the quantity of described undersetting is two.
5. air-conditioning connector as claimed in claim 4, is characterized in that, described connector construction has two supporting legs, described two supporting legs and described two undersettings assembling.
6. air-conditioning connector as claimed in claim 5, is characterized in that, on the supporting leg of described connector construction, guide finger is housed, and described undersetting is provided with the gathering sill mating with described guide finger.
7. air-conditioning connector as claimed in claim 2, it is characterized in that, described locking device comprises torsion spring and latch hook, and described torsion spring is connected with described adapter, described latch hook is connected with described torsion spring, and described torsion spring is controlled described latch hook and hooked or depart from described upper bracket.
8. air-conditioning connector as claimed in claim 7, is characterized in that, on described connector construction, is welded with guide vane end stop, and described guide vane end stop limits the motion of described adapter.
9. air-conditioning connector as claimed in claim 2, is characterized in that, magnet steel head is installed on described upper bracket, fills magnetic red transducer on described connector construction.
10. the air-conditioning connector as described in claim 1 to 9 any one, is characterized in that, on described arrow wall, posts rubber seal with the interface of connector construction.
11. air-conditioning connectors as described in claim 1 to 9 any one, is characterized in that, six bafflers are set on described connector construction, and described baffler and described connector construction weld together, and become miter angle upwards with connector construction counterface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210366963.4A CN103700983B (en) | 2012-09-27 | 2012-09-27 | Air-conditioning adapter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210366963.4A CN103700983B (en) | 2012-09-27 | 2012-09-27 | Air-conditioning adapter |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103700983A true CN103700983A (en) | 2014-04-02 |
| CN103700983B CN103700983B (en) | 2016-06-22 |
Family
ID=50362433
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210366963.4A Active CN103700983B (en) | 2012-09-27 | 2012-09-27 | Air-conditioning adapter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103700983B (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104836058A (en) * | 2015-05-26 | 2015-08-12 | 叶吉利 | Circuit board socket component with left and right spacing sensors |
| CN105736113A (en) * | 2014-12-11 | 2016-07-06 | 陕西重型汽车有限公司 | Air protection hood assembly and assembling method thereof |
| CN113324444A (en) * | 2021-04-25 | 2021-08-31 | 上海宇航系统工程研究所 | Flow guide structure of air supply outlet of air conditioner of carrier rocket satellite fairing |
| CN113428057A (en) * | 2021-07-09 | 2021-09-24 | 浙江吉利控股集团有限公司 | Vehicle armrest box |
| CN115218729A (en) * | 2022-07-06 | 2022-10-21 | 蓝箭航天空间科技股份有限公司 | A vent flap for carrier rocket radome |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1040312A1 (en) * | 1997-12-16 | 2000-10-04 | Lockheed Martin Corporation | Separation system |
| CN101665156A (en) * | 2008-09-03 | 2010-03-10 | 北京航空航天大学 | Connecting and unlocking mechanism driven by SMA wire |
| CN201842261U (en) * | 2010-09-17 | 2011-05-25 | 湖北航天技术研究院总体设计所 | Pneumatic executive device used for separating two objects |
| CN102975872A (en) * | 2012-12-25 | 2013-03-20 | 中国科学院长春光学精密机械与物理研究所 | Shock-free wrapping tape type unlocking separation mechanism |
-
2012
- 2012-09-27 CN CN201210366963.4A patent/CN103700983B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1040312A1 (en) * | 1997-12-16 | 2000-10-04 | Lockheed Martin Corporation | Separation system |
| CN101665156A (en) * | 2008-09-03 | 2010-03-10 | 北京航空航天大学 | Connecting and unlocking mechanism driven by SMA wire |
| CN201842261U (en) * | 2010-09-17 | 2011-05-25 | 湖北航天技术研究院总体设计所 | Pneumatic executive device used for separating two objects |
| CN102975872A (en) * | 2012-12-25 | 2013-03-20 | 中国科学院长春光学精密机械与物理研究所 | Shock-free wrapping tape type unlocking separation mechanism |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105736113A (en) * | 2014-12-11 | 2016-07-06 | 陕西重型汽车有限公司 | Air protection hood assembly and assembling method thereof |
| CN105736113B (en) * | 2014-12-11 | 2018-07-24 | 陕西重型汽车有限公司 | Wind shelling cover assembly and its assembly method |
| CN104836058A (en) * | 2015-05-26 | 2015-08-12 | 叶吉利 | Circuit board socket component with left and right spacing sensors |
| CN113324444A (en) * | 2021-04-25 | 2021-08-31 | 上海宇航系统工程研究所 | Flow guide structure of air supply outlet of air conditioner of carrier rocket satellite fairing |
| CN113428057A (en) * | 2021-07-09 | 2021-09-24 | 浙江吉利控股集团有限公司 | Vehicle armrest box |
| CN115218729A (en) * | 2022-07-06 | 2022-10-21 | 蓝箭航天空间科技股份有限公司 | A vent flap for carrier rocket radome |
| CN115218729B (en) * | 2022-07-06 | 2023-06-09 | 蓝箭航天空间科技股份有限公司 | Ventilating port cover for fairing of carrier rocket |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103700983B (en) | 2016-06-22 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103700983A (en) | Air conditioner air supply connector | |
| CN203545532U (en) | Connector device and tower crane provided with same | |
| CN206398160U (en) | A kind of adjustable stop valve for being easy to control | |
| CN204126003U (en) | The comprehensive interim waterworks for firefighting of a kind of packaged type | |
| CN208068090U (en) | A kind of solar wing simulation tooling | |
| CN110588921B (en) | Floating ball device and underwater robot | |
| CN205911711U (en) | Electric wire straining device of being convenient for | |
| CN101723070A (en) | Device for locking and unlocking underwater rope | |
| CN204806961U (en) | Rifle lock | |
| CN107939731A (en) | A kind of axial fan | |
| CN206246424U (en) | A kind of chilled water pump of nuclear power station | |
| CN206309708U (en) | A kind of screw thread fastening type fast assembling disassembling structure for plated film | |
| CN208417637U (en) | A kind of quenching pump house check-valves turnover panel | |
| CN208295384U (en) | A kind of general compensator of combustion gas | |
| CN207906469U (en) | A kind of pipe gallery airtight valve | |
| CN208669613U (en) | Ready-packaged Pulp pump | |
| CN206234165U (en) | A kind of blower fan coupling assembly | |
| CN208831312U (en) | A kind of coupling shield | |
| CN110469518A (en) | It is a kind of with the intelligent deep well pump for automatically powering off protection mechanism | |
| CN206246407U (en) | A kind of nuclear power station chilled water pump rotor part | |
| CN220752848U (en) | Explosion-proof integrated remote controller of combustible gas alarm system | |
| CN221163217U (en) | Anchoring device for wave energy power generation platform | |
| CN214008100U (en) | Novel inserting plate type electromagnetic valve | |
| CN204809575U (en) | Fast gate -type electric connector | |
| CN202946432U (en) | Centrifugal blower sealing nitrogen charge device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |