CN104034213B - A kind of rocket projectile reliably opens the cabin mechanism - Google Patents
A kind of rocket projectile reliably opens the cabin mechanism Download PDFInfo
- Publication number
- CN104034213B CN104034213B CN201410233959.XA CN201410233959A CN104034213B CN 104034213 B CN104034213 B CN 104034213B CN 201410233959 A CN201410233959 A CN 201410233959A CN 104034213 B CN104034213 B CN 104034213B
- Authority
- CN
- China
- Prior art keywords
- connector
- key
- connecting hole
- key connecting
- front connector
- 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.)
- Active
Links
Landscapes
- Vibration Dampers (AREA)
Abstract
The present invention relates to a kind of rocket projectile reliably to open the cabin mechanism, belong to rocket projectile technical field.Mechanism of opening the cabin of the present invention, comprises front connector, rear connector, screw, cushion block, key; Be connected with the syndeton of rear connector by " screw thread adds key " at front connector, in the duties processes such as transport at ordinary times, carrying, axial attachment force is born by the thread segment between front connector and rear connector; The circumferential shearing force that body High Rotation Speed produces in transmit state is born by bond structure; When carrying out lock out operation, separation medicine only need destroy the connecting thread between front connector and rear connector, can realize opening the cabin.Mechanism structure of opening the cabin of the present invention is simple, easy to assembly, while the enough bonding strengths of guarantee, can ensure again the reliable separation of front and back connector, have important popularizing application prospect.
Description
Technical field
The present invention relates to a kind of rocket projectile reliably to open the cabin mechanism, belong to rocket projectile technical field.
Background technology
When cabin, the front and back body of rocket projectile docks, the helicitic texture that conventional method adopts usually connects, this screw connection structure, for the relatively light rocket projectile of weight, both can meet bonding strength during rotary motion, can realize again being separated reliable separation between the two cabin bodies that need.But for the rocket projectile that cabin, front and back body weight is larger, learn through test, the axial shearing force that cabin, front and back body connecting portion is subject under accumulating and emission state is less, only can meet the demands by the shorter section of being threaded; And the circumferential shearing force of body High Rotation Speed generation is larger in transmit state, adopting the single screw connection structure of tradition just must increase bonding strength by the length extending the section of being threaded, disintegrating in advance when not reaching the predetermined area to avoid cabin, front and back body connecting portion; But the longer section of being threaded, opening the cabin to operate to body also been proposed higher requirement, is separated dose very few, cannot realizes effective separation; Separation dose is too much, can take more body space, and also can damage the miscellaneous part of body when being separated medicine effect, affects the normal work of rocket projectile.
Summary of the invention
The object of the invention is cabin body before and after the large weight in order to solve the traditional single helicitic texture connection of employing, there are the technological difficulties that cannot meet bonding strength simultaneously and effectively be separated, and a kind of " screw thread adds key " formula connection isolating construction is provided.
The object of the invention is to be achieved through the following technical solutions:
A kind of rocket projectile of the present invention reliably opens the cabin mechanism, comprises front connector, rear connector, screw, cushion block, key;
The rear end inwall of front connector inwardly has annular link slot, the leading portion of this annular link slot is processed with internal thread, the thread segment rear end of this annular link slot has the key connecting hole of a screwed hole and an axial aperture, this screwed hole is not communicated with the forward end of this key connecting hole, and the end, rear end of this key connecting hole is not communicated with the rear end end face of front connector;
The front end outer wall of rear connector is processed with the annular link slot matched with front connector rear end inwall, this annular link slot leading portion is processed with the external screw thread matched with front connector annular link slot leading portion internal thread, the thread segment rear end of this annular link slot has the key connecting hole of an axial aperture, this key connecting hole is consistent with the key connecting hole width on front connector, and the end face distance at two ends, key bottom is greater than the length of key connecting hole on front connector;
The width of key is consistent with the width of key connecting hole on front connector and rear connector, on the height of key and front connector and rear connector, the degree of depth sum of key connecting hole matches, the top, two ends of key all has the step trough matched with the key connecting hole degree of depth on front connector, and the bottom, two ends, front end of key is all processed as the inclined-plane of restraining to the inside;
The width of cushion block is consistent with the width of key connecting hole on front connector and rear connector, on the height of cushion block and rear connector, the degree of depth of key connecting hole matches, and on the length of cushion block and the end face distance sum at two ends, key bottom and rear connector, the length of key connecting hole matches;
The front end of rear connector insert before connector annular link slot in and be threaded, and the key connecting hole on front connector and the key connecting hole circumference on rear connector are aligned; By the key connecting hole of the lower front part of key through front connector, and connector key connecting hole front end after inserting, make the rear end of key put into the key connecting hole of rear connector, promote key backward, make the occlusion part screens of key connecting hole rear end on the cascaded surface of key rear end and front connector; Screwed hole on cushion block in the past connector is inserted, and is placed on the front end of the key bottom on rear connector in key connecting hole, make axial location in the key connecting hole of key on rear connector; Screw thread is connected in the screwed hole of front connector, and scribbles fastening glue between screw and this screwed hole.
Operation principle: in the duties processes such as transport at ordinary times, carrying, axial attachment force is born by the thread segment between front connector and rear connector; The circumferential shearing force that body High Rotation Speed produces in transmit state is born by bond structure; When carrying out lock out operation, separation medicine only need destroy the connecting thread between front connector and rear connector, can realize opening the cabin.
Beneficial effect:
Mechanism structure of opening the cabin of the present invention is simple, easy to assembly, the conventional thinking that length that conventional method can only extend connecting thread simply increases bonding strength has been evaded by the syndeton of " screw thread adds key ", before and after effective solution, connector is to bonding strength and the design contradiction be effectively separated, while the enough bonding strengths of guarantee, the reliable separation of front and back connector can be ensured again, there is important popularizing application prospect.
Accompanying drawing explanation
Fig. 1 is that the present invention opens the cabin the connection diagram of mechanism;
Fig. 2 is that the present invention opens the cabin the generalized section of connector before in mechanism;
Fig. 3 is the top view of Fig. 2;
Fig. 4 is that the present invention opens the cabin the front view of key in mechanism;
Fig. 5 is the top view of Fig. 4;
Wherein: connector before 1-; Connector after 2-; 3-screw; 4-cushion block; 5-key.
Detailed description of the invention
Below in conjunction with accompanying drawing, preferred example of the present invention is further described:
Embodiment
A kind of rocket projectile of the present invention reliably opens the cabin mechanism, as shown in Figure 1, comprises front connector 1, rear connector 2, screw 3, cushion block 4, key 5;
As shown in Figure 2,3, the rear end inwall of front connector 1 inwardly has annular link slot, the leading portion of this annular link slot is processed with internal thread, the thread segment rear end of this annular link slot has the key connecting hole of a screwed hole and an axial aperture, this screwed hole is not communicated with the forward end of this key connecting hole, and the end, rear end of this key connecting hole is not communicated with the rear end end face of front connector 1;
The front end outer wall of rear connector 2 is processed with the annular link slot matched with front connector 1 rear end inwall, this annular link slot leading portion is processed with the external screw thread matched with front connector 1 annular link slot leading portion internal thread, the thread segment rear end of this annular link slot has the key connecting hole of an axial aperture, this key connecting hole is consistent with the key connecting hole width on front connector 1, and the end face distance at two ends, key 5 bottom is greater than the length of key connecting hole on front connector 1;
As shown in Figure 4,5, the width of key 5 is consistent with the width of key connecting hole on front connector 1 and rear connector 2, on the height of key 5 and front connector 1 and rear connector 2, the degree of depth sum of key connecting hole matches, the top, two ends of key 5 all has the step trough matched with the key connecting hole degree of depth on front connector 1, and the bottom, two ends, front end of key 5 is all processed as the inclined-plane of restraining to the inside;
The width of cushion block 4 is consistent with the width of key connecting hole on front connector 1 and rear connector 2, on the height of cushion block 4 and rear connector 2, the degree of depth of key connecting hole matches, and on the length of cushion block 4 and the end face distance sum at two ends, key 5 bottom and rear connector 2, the length of key connecting hole matches;
The front end of rear connector 2 insert before connector 1 annular link slot in and be threaded, and the key connecting hole on front connector 1 and the key connecting hole circumference on rear connector 2 are aligned; By the key connecting hole of the lower front part of key 5 through front connector 1, and connector 2 key connecting hole front end after inserting, make the rear end of key 5 put into the key connecting hole of rear connector 2, promote key 5 backward, make the occlusion part screens of key connecting hole rear end on the cascaded surface of key 5 rear end and front connector 1; Screwed hole on cushion block 4 in the past connector 1 is inserted, and is placed on the front end of key 5 bottom on rear connector 2 in key connecting hole, make axial location in the key connecting hole of key 5 on rear connector 2; Screw 3 is threaded in the screwed hole of front connector 1, and scribbles fastening glue between screw 3 and this screwed hole.
Operation principle: in the duties processes such as transport at ordinary times, carrying, axial attachment force is born by the thread segment between front connector 1 and rear connector 2; The circumferential shearing force that body High Rotation Speed produces in transmit state is born by bond structure; When carrying out lock out operation, separation medicine only need destroy the connecting thread between front connector 1 and rear connector 2, can realize opening the cabin.
Claims (1)
1. rocket projectile reliably opens the cabin a mechanism, it is characterized in that: comprise front connector, rear connector, screw, cushion block, key;
The rear end inwall of front connector inwardly has annular link slot, the leading portion of this annular link slot is processed with internal thread, the thread segment rear end of this annular link slot has the key connecting hole of a screwed hole and an axial aperture, this screwed hole is not communicated with the forward end of this key connecting hole, and the end, rear end of this key connecting hole is not communicated with the rear end end face of front connector;
The front end outer wall of rear connector is processed with the annular link slot matched with front connector rear end inwall, this annular link slot leading portion is processed with the external screw thread matched with front connector annular link slot leading portion internal thread, the thread segment rear end of this annular link slot has the key connecting hole of an axial aperture, this key connecting hole is consistent with the key connecting hole width on front connector, and the end face distance at two ends, key bottom is greater than the length of key connecting hole on front connector;
The width of key is consistent with the width of key connecting hole on front connector and rear connector, on the height of key and front connector and rear connector, the degree of depth sum of key connecting hole matches, the top, two ends of key all has the step trough matched with the key connecting hole degree of depth on front connector, and the bottom, two ends, front end of key is all processed as the inclined-plane of restraining to the inside;
The width of cushion block is consistent with the width of key connecting hole on front connector and rear connector, on the height of cushion block and rear connector, the degree of depth of key connecting hole matches, and on the length of cushion block and the end face distance sum at two ends, key bottom and rear connector, the length of key connecting hole matches;
The front end of rear connector insert before connector annular link slot in and be threaded, and the key connecting hole on front connector and the key connecting hole circumference on rear connector are aligned; By the key connecting hole of the lower front part of key through front connector, and connector key connecting hole front end after inserting, make the rear end of key put into the key connecting hole of rear connector, promote key backward, make the occlusion part screens of key connecting hole rear end on the cascaded surface of key rear end and front connector; Screwed hole on cushion block in the past connector is inserted, and is placed on the front end of the key bottom on rear connector in key connecting hole, make axial location in the key connecting hole of key on rear connector; Screw thread is connected in the screwed hole of front connector, and scribbles fastening glue between screw and this screwed hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410233959.XA CN104034213B (en) | 2014-05-28 | 2014-05-28 | A kind of rocket projectile reliably opens the cabin mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410233959.XA CN104034213B (en) | 2014-05-28 | 2014-05-28 | A kind of rocket projectile reliably opens the cabin mechanism |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104034213A CN104034213A (en) | 2014-09-10 |
| CN104034213B true CN104034213B (en) | 2015-10-21 |
Family
ID=51465082
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410233959.XA Active CN104034213B (en) | 2014-05-28 | 2014-05-28 | A kind of rocket projectile reliably opens the cabin mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104034213B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104501665B (en) * | 2014-12-11 | 2017-02-08 | 晋西工业集团有限责任公司 | Stepwise shearing type orienting knob automatic releasing device |
| CN110749249A (en) * | 2019-10-30 | 2020-02-04 | 河南北方红阳机电有限公司 | Bullet bottom sealing structure of gun projectile and bonding method |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5131610A (en) * | 1990-07-11 | 1992-07-21 | Aerospatiale Societe Nationale Industrielle | Front end structure of a booster rocket mounted on the main body of a launcher |
| CN102494565A (en) * | 2011-11-11 | 2012-06-13 | 中国航天科技集团公司第四研究院第四十一研究所 | Separation mechanism of oriented rocket nose body |
| CN103256866A (en) * | 2013-04-25 | 2013-08-21 | 蒋成吉 | Connecting plate of rocket connector |
| CN203981034U (en) * | 2014-05-28 | 2014-12-03 | 晋西工业集团有限责任公司 | A kind of rocket projectile mechanism of reliably opening the cabin |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2002198B1 (en) * | 2006-03-30 | 2013-04-24 | Raytheon Company | Methods and apparatus for integrated locked thruster mechanism |
| KR101117100B1 (en) * | 2009-09-03 | 2012-02-22 | 국방과학연구소 | Separation device of ejector motor for portable missile |
-
2014
- 2014-05-28 CN CN201410233959.XA patent/CN104034213B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5131610A (en) * | 1990-07-11 | 1992-07-21 | Aerospatiale Societe Nationale Industrielle | Front end structure of a booster rocket mounted on the main body of a launcher |
| CN102494565A (en) * | 2011-11-11 | 2012-06-13 | 中国航天科技集团公司第四研究院第四十一研究所 | Separation mechanism of oriented rocket nose body |
| CN103256866A (en) * | 2013-04-25 | 2013-08-21 | 蒋成吉 | Connecting plate of rocket connector |
| CN203981034U (en) * | 2014-05-28 | 2014-12-03 | 晋西工业集团有限责任公司 | A kind of rocket projectile mechanism of reliably opening the cabin |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104034213A (en) | 2014-09-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104034212B (en) | A kind of rocket projectile connection separation mechanism | |
| CN104034213B (en) | A kind of rocket projectile reliably opens the cabin mechanism | |
| AR083884A1 (en) | DOUBLE CHAMBER AND FILLING SYRINGE OF ARIPIPRAZOL IN THE SYRINGE | |
| CN207045672U (en) | Airplane hatch cover fixed structure | |
| CN204992054U (en) | Can dismantle electric connector | |
| CN208451077U (en) | A kind of nonmetallic piston ring machining tooling | |
| MX2018004080A (en) | Dispensing capsule. | |
| CN102829056B (en) | Firmware of riveting tightly is attacked from brill | |
| CN104976466B (en) | A kind of new-type softer, elastic water pipe head | |
| CN203848761U (en) | Connection and separation mechanism for rocket projectile | |
| CN203981034U (en) | A kind of rocket projectile mechanism of reliably opening the cabin | |
| CN205872408U (en) | Deep water power pressurized cabin | |
| CN104343398B (en) | A kind of polygonal pyramid sealed auger stem of quick grafting | |
| CN107059853A (en) | Band tooth connector | |
| CN204664093U (en) | A kind of fast self-locking mechanical fastener | |
| CN105587729A (en) | Hexagon bolt with sealing rings | |
| CN206255166U (en) | Low noise bay section separating mechanism | |
| CN203809915U (en) | Hose nippler for high-pressure rubber hose bursting test | |
| CN204433060U (en) | Aircraft load release device | |
| CN106628105A (en) | Unmanned aerial vehicle with rod-shaped plug batteries | |
| CN208859164U (en) | Sealed vibration-proof rotary hose joint | |
| CN105257667A (en) | Looseness-proof machinery fastening mechanism | |
| CN202768825U (en) | Sucker sealing part | |
| CN204468993U (en) | Safe large discharge drainage connecting pipe | |
| CN202768828U (en) | Suction cup sealing element |
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 |