CN106288954A - A kind of pollution-free, firing box Rapid opening device without ejecta - Google Patents

A kind of pollution-free, firing box Rapid opening device without ejecta Download PDF

Info

Publication number
CN106288954A
CN106288954A CN201610819439.6A CN201610819439A CN106288954A CN 106288954 A CN106288954 A CN 106288954A CN 201610819439 A CN201610819439 A CN 201610819439A CN 106288954 A CN106288954 A CN 106288954A
Authority
CN
China
Prior art keywords
flange
lid body
box
case lid
shear pin
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
Application number
CN201610819439.6A
Other languages
Chinese (zh)
Other versions
CN106288954B (en
Inventor
杨娇萍
张平雨
冯雨
邓科
于殿君
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Beijing Institute of Specialized Machinery
Original Assignee
Beijing Institute of Specialized Machinery
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Beijing Institute of Specialized Machinery filed Critical Beijing Institute of Specialized Machinery
Priority to CN201610819439.6A priority Critical patent/CN106288954B/en
Publication of CN106288954A publication Critical patent/CN106288954A/en
Application granted granted Critical
Publication of CN106288954B publication Critical patent/CN106288954B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/042Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F7/00Launching-apparatus for projecting missiles or projectiles otherwise than from barrels, e.g. using spigots

Abstract

The present invention relates to a kind of pollution-free, firing box Rapid opening device without ejecta, belong to lift-off technology field.The present invention is before vehicle launch, and under the signal of telecommunication triggers, case lid, under the thrust that motor-driven cylinder produces, can overcome weak link, quickly open, and uncaps and locks on casing after putting in place, and front ready rear outlet penetrated by aircraft.Experiment proves that, it is achieved this mode of uncapping there is no any smog, aircraft target seeker will not be produced any pollution, there is no any fragment of dishing out, other transmitting equipment of ground will not be produced any infringement, safety is high;Time of uncapping is short, can uncap in 1s;And this apparatus structure is simple, generalization is strong, and with low cost, practicality is good.

Description

A kind of pollution-free, firing box Rapid opening device without ejecta
Technical field
The present invention relates to lift-off technology field, be specifically related to a kind of firing box Rapid opening pollution-free, without ejecta and fill Put.
Background technology
The case lid of firing box is arranged in firing box two ends, realizes the sealing to firing box and bear the airtight of casing during storage Pressure, opens during transmitting, gets out of the way aircraft motion and combustion gas stream arranges pathway.
There is multiple mode of uncapping in firing box case lid at present: the electromechanics mode of uncapping is to use motor to produce thrust to be beaten by case lid Opening, this mode of uncapping can be uncapped in advance, however it is necessary that driven opening lid mechanism is arranged in certain space, and uncaps the time one As long, be the most all much larger than 1s;Thrust cylinder or the primacord mode of uncapping are that the thrust utilizing priming system blast to produce is by case Lid is dished out, and this mode of uncapping can also be uncapped in advance, the time of uncapping short (being smaller than 1s), but thrust cylinder and primacord blast Time can produce smog, aircraft target seeker is had certain pollution, further, since there is ejecta, this throwing lid mode meeting There is certain potential safety hazard;Case lid is pushed open by the shock wave produced when the gas shock-wave mode of uncapping is to utilize vehicle launch, this Although it is easy to plant mode of uncapping, but cannot open in advance, can only uncap after aircraft is lighted a fire, and shock wave needs through flying Row device, can cause certain impact, once use and need to accumulate substantial amounts of examination the outthrust on body such as rudder face or missile wing etc. Verify.
According to vehicle launch requirement, firing box case lid must be opened before transmission, and the time of uncapping is less than 1s, it is impossible to produce Any smog, it is impossible to have ejecta, the most above-mentioned mode of uncapping all can not meet requirement.
Summary of the invention
(1) to solve the technical problem that
The technical problem to be solved in the present invention is: how to design a kind of pollution-free, firing box Rapid opening without ejecta Device.
(2) technical scheme
In order to solve above-mentioned technical problem, the invention provides a kind of pollution-free, firing box Rapid opening without ejecta Device, including motor-driven cylinder 1, box flange 2, Moveable lid body 3, case lid flange 4, shear pin 5, rotating shaft 6, turnover hinge 7 and lock Tight assembly 8;
It is connected by shear pin 5 between described Moveable lid body 3 and case lid flange 4;
Described Moveable lid body 3, case lid flange 4, shear pin 5, rotating shaft 6 and turnover hinge 7 form launching box cover, described transmitting Case lid is integrally attached to the front end face of box flange 2;Described motor-driven cylinder 1 is fixedly mounted on the back side of box flange 2;Electrical actuation Extension bar 1a on device 1 passes box flange 2 and case lid flange 4, contacts with the Moveable lid body 3 of launching box cover;Described locking group Part 8 is fixed on below box flange 2, is made up of fixing seat 9 and two locking reeds 10;Locking reed 10 is stuck in fixing seat 9 Boss on;Moveable lid body 3 is connected with box flange 2 by shear pin 5, and rotating shaft 6 is arranged on Moveable lid body 3 bottom;Upset hinge Chain 7 is screwed onto on Moveable lid body 3;Moveable lid body 3 can overturn along rotating shaft 6 after being cut off by shear pin 5, after upset puts in place, and upset hinge Chain 7 is between two locking reeds 10, and the trapezium structure on turnover hinge 7 is blocked locking by two locking reeds 10.
Preferably, during storage, between described Moveable lid body 3 and case lid flange 4, seam crossing uses sealant sealing.
Preferably, side and the bottom surface of described fixing seat 9 is screwed locking reed 10.
Preferably, described launching box cover is fixed on the front end face of box flange 2 entirely through screw.
(3) beneficial effect
The present invention is before vehicle launch, and under the signal of telecommunication triggers, case lid, can under the thrust that motor-driven cylinder produces Overcoming weak link, quickly open, uncap and lock on casing after putting in place, front ready rear outlet penetrated by aircraft.Through test Checking, it is achieved this mode of uncapping there is no any smog, will not to aircraft target seeker produce any pollution, there is no any throwing Going out fragment, other transmitting equipment of ground will not produce any infringement, safety is high;Time of uncapping is short, can uncap in 1s;And This apparatus structure is simple, and generalization is strong, and with low cost, practicality is good.
Accompanying drawing explanation
Fig. 1 is apparatus structure and the firing box pass lid view of the embodiment of the present invention;Wherein (a) left figure is for facing Figure, right figure is left view;
Fig. 2 is apparatus structure and the firing box uncapped state schematic diagram of the embodiment of the present invention;Wherein (a) left figure is for facing Figure, right figure is left view;.
Detailed description of the invention
For making the purpose of the present invention, content and advantage clearer, below in conjunction with the accompanying drawings and embodiment, to the present invention's Detailed description of the invention is described in further detail.
As Figure 1-Figure 2, the embodiment of the present invention pollution-free, without the firing box Rapid opening device of ejecta, including Motor-driven cylinder 1, box flange 2, Moveable lid body 3, case lid flange 4, shear pin 5, rotating shaft 6, turnover hinge 7 and latch assembly 8;
Described Moveable lid body 3, case lid flange 4, shear pin 5, rotating shaft 6 and turnover hinge 7 form launching box cover, described transmitting Case lid is fixed on the front end face of box flange 2 entirely through screw;Described motor-driven cylinder 1 is fixedly mounted on the back of the body of box flange 2 Face;Extension bar 1a on motor-driven cylinder 1 passes box flange 2 and case lid flange 4, contacts with the Moveable lid body 3 of launching box cover;Institute State latch assembly 8 and be fixed on below box flange 2, be made up of fixing seat 9 and two locking reeds 10;Locking reed 10 is stuck in On the boss of fixing seat 9, the side of described fixing seat 9 and bottom surface are screwed locking reed 10.Moveable lid body 3 is by shearing Pin 5 is connected with box flange 2, and rotating shaft 6 is arranged on Moveable lid body 3 bottom;Turnover hinge 7 is screwed onto on Moveable lid body 3;Removable cover Body 3 can overturn along rotating shaft 6, after upset puts in place, turnover hinge 7 between two locking reeds 10, trapezoidal on turnover hinge 7 Structure is blocked locking by two locking reeds 10.
During storage, it is connected by shear pin 5 between described Moveable lid body 3 and case lid flange 4, described Moveable lid body 3 and case What between lid flange 4, seam crossing used that sealant sealing realizes between Moveable lid body 3 and case lid flange 4 is airtight.Case lid flange 4 leads to That crosses that O and screw realize between casing is airtight.
When this number position is launched, providing motor-driven cylinder 1 actuating signal before transmitting, on motor-driven cylinder 1, extension bar stretches out, and generation pushes away Power acts on Moveable lid body 3, and shear pin 5 is cut off tailing edge rotating shaft 6 and overturn by Moveable lid body 3, and after upset puts in place, 7 are positioned at two Between 10, the part that the trapezium structure on turnover hinge 7 is pulled open by two locking reed 10 sides blocks locking, and case lid has been opened Finish.The whole time of uncapping, less than 1s, does not has any ejecta, does not has any cigarette in motor-driven cylinder 1 mechanism during uncapping Mist produces, and meets this system and uncaps technology requirement.
When adjacent position is launched, the external pressure that aircraft gas produces acts on Moveable lid body 3 outer surface, and is delivered to case lid On flange 4, then be delivered on box flange 2, it is achieved launching box cover hold external pressure ability.
The above is only the preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art For Yuan, on the premise of without departing from the technology of the present invention principle, it is also possible to make some improvement and deformation, these improve and deformation Also should be regarded as protection scope of the present invention.

Claims (4)

1. pollution-free, a firing box Rapid opening device without ejecta, it is characterised in that include motor-driven cylinder (1), casing Flange (2), Moveable lid body (3), case lid flange (4), shear pin (5), rotating shaft (6), turnover hinge (7) and latch assembly (8);
During storage, it is connected by shear pin (5) between described Moveable lid body (3) with case lid flange (4);
Described Moveable lid body (3), case lid flange (4), shear pin (5), rotating shaft (6) and turnover hinge (7) composition launching box cover, institute State launching box cover and be integrally attached to the front end face of box flange (2);Described motor-driven cylinder (1) is fixedly mounted on box flange (2) The back side;Extension bar (1a) on motor-driven cylinder (1) passes box flange (2) and case lid flange (4), with the activity of launching box cover Lid (3) contacts;Described latch assembly (8) is fixed on below box flange (2), by fixing seat (9) and two locking reeds (10) composition;Locking reed (10) is stuck on the boss of fixing seat (9);Moveable lid body (3) passes through shear pin (5) and box flange (2) connecting, rotating shaft (6) is arranged on Moveable lid body (3) bottom;Turnover hinge (7) is screwed onto on Moveable lid body (3);Moveable lid body (3) can overturn along rotating shaft (6) after being cut off by shear pin (5), after upset puts in place, turnover hinge (7) is positioned at two locking reeds (10), between, the trapezium structure on turnover hinge (7) is blocked locking by two locking reeds (10).
2. device as claimed in claim 1, it is characterised in that during storage, described Moveable lid body (3) and case lid flange (4) it Sealant sealing is used at seam.
3. device as claimed in claim 1, it is characterised in that side and the bottom surface of described fixing seat (9) are screwed lock Tight reed (10).
4. the device as described in claim 1 or 2 or 3, it is characterised in that described launching box cover is fixed on case entirely through screw The front end face of body flange (2).
CN201610819439.6A 2016-09-12 2016-09-12 A kind of pollution-free, without ejecta firing box Rapid opening device Active CN106288954B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610819439.6A CN106288954B (en) 2016-09-12 2016-09-12 A kind of pollution-free, without ejecta firing box Rapid opening device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610819439.6A CN106288954B (en) 2016-09-12 2016-09-12 A kind of pollution-free, without ejecta firing box Rapid opening device

Publications (2)

Publication Number Publication Date
CN106288954A true CN106288954A (en) 2017-01-04
CN106288954B CN106288954B (en) 2017-12-05

Family

ID=57709957

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610819439.6A Active CN106288954B (en) 2016-09-12 2016-09-12 A kind of pollution-free, without ejecta firing box Rapid opening device

Country Status (1)

Country Link
CN (1) CN106288954B (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108871059A (en) * 2018-06-08 2018-11-23 南京理工大学 It hits unlock-spring potential energy and drives firing box hood-opening device
CN109470081A (en) * 2018-12-17 2019-03-15 贵州航天风华精密设备有限公司 A kind of firing box locking and electronic hood-opening device
CN110045609A (en) * 2019-04-17 2019-07-23 北京理工大学 It is a kind of that perpendicular apparatus control system is played based on PID- sliding-mode variable structure algorithm
CN110360883A (en) * 2019-07-03 2019-10-22 北京航天发射技术研究所 A kind of ground installation protective device of adaptive rocket motion
CN113104388A (en) * 2021-04-23 2021-07-13 王树珉 Automatic bottle opener
CN114353588A (en) * 2022-01-19 2022-04-15 北京凌空天行科技有限责任公司 Launch canister packaging device
RU2775500C2 (en) * 2020-09-07 2022-07-04 Российская Федерация в лице Министерства обороны РФ Container for launching ammunition

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB256741A (en) * 1925-06-11 1926-08-19 Whitehead Torpedo Company Ltd Improvements in or relating to launching or ejecting tubes for automobile torpedoes
US5956901A (en) * 1997-06-24 1999-09-28 Northrop Grumman Corporation Gas driven hatch cover assembly
CN103790460A (en) * 2012-11-01 2014-05-14 上海新跃仪表厂 Automatic rapid opening and closing mechanism of cabin door
CN104527996A (en) * 2014-12-01 2015-04-22 南京理工大学 Integrated rail type cube satellite launching device
CN105043166A (en) * 2015-07-20 2015-11-11 北京理工大学 Low-impact overall ejection type launching canister front cover

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB256741A (en) * 1925-06-11 1926-08-19 Whitehead Torpedo Company Ltd Improvements in or relating to launching or ejecting tubes for automobile torpedoes
US5956901A (en) * 1997-06-24 1999-09-28 Northrop Grumman Corporation Gas driven hatch cover assembly
CN103790460A (en) * 2012-11-01 2014-05-14 上海新跃仪表厂 Automatic rapid opening and closing mechanism of cabin door
CN104527996A (en) * 2014-12-01 2015-04-22 南京理工大学 Integrated rail type cube satellite launching device
CN105043166A (en) * 2015-07-20 2015-11-11 北京理工大学 Low-impact overall ejection type launching canister front cover

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108871059A (en) * 2018-06-08 2018-11-23 南京理工大学 It hits unlock-spring potential energy and drives firing box hood-opening device
CN109470081A (en) * 2018-12-17 2019-03-15 贵州航天风华精密设备有限公司 A kind of firing box locking and electronic hood-opening device
CN109470081B (en) * 2018-12-17 2020-10-16 贵州航天风华精密设备有限公司 Launching box locking and electric cover opening device
CN110045609A (en) * 2019-04-17 2019-07-23 北京理工大学 It is a kind of that perpendicular apparatus control system is played based on PID- sliding-mode variable structure algorithm
CN110360883A (en) * 2019-07-03 2019-10-22 北京航天发射技术研究所 A kind of ground installation protective device of adaptive rocket motion
CN110360883B (en) * 2019-07-03 2021-05-11 北京航天发射技术研究所 Ground equipment protection device capable of self-adapting to rocket motion
RU2775500C2 (en) * 2020-09-07 2022-07-04 Российская Федерация в лице Министерства обороны РФ Container for launching ammunition
CN113104388A (en) * 2021-04-23 2021-07-13 王树珉 Automatic bottle opener
CN114353588A (en) * 2022-01-19 2022-04-15 北京凌空天行科技有限责任公司 Launch canister packaging device
CN114353588B (en) * 2022-01-19 2023-07-18 北京凌空天行科技有限责任公司 Packaging device for transmitting tube

Also Published As

Publication number Publication date
CN106288954B (en) 2017-12-05

Similar Documents

Publication Publication Date Title
CN106288954A (en) A kind of pollution-free, firing box Rapid opening device without ejecta
CN103940566B (en) Trainable electronic control type bird bullet impact test device
KR20120136283A (en) Stealth aerial vehicle
US4391094A (en) Destructable air inlet cover for rocket engines
DK2941616T3 (en) Amphibious vehicle and method of operating an amphibious vehicle
CN203323620U (en) Rain-increasing hail-suppressing rocket projectile recycling device
US20180327104A1 (en) Aircraft propulsion assembly comprising a fan conjointly driven by two engines
DE60309380T2 (en) Locking system for an opening of an air inlet duct of a combustion chamber of a ramjet engine, and ramjet engine and missile with such a system
RU161930U1 (en) AIR REJECTIVE AIR-ENGINE DEVICE PLUGGING PLUG
CN206704518U (en) Fixed-wing unmanned plane with shatter-resistant function
RU191818U1 (en) Air intake device with resettable plug of the jet engine
CN204788051U (en) Formula tray protecgulum is wholly launched to low impact
CN103940614A (en) Turbofan engine inlet part ice ball collision device
CN101672602B (en) Outer-layer safeguard structure for preventing bullet from penetrating tank
CN111017213B (en) Unmanned aerial vehicle recovery system guide umbrella penetrates umbrella mechanism
CN103940567A (en) Electronic control type aimable ice shot impact testing device
CN107588681A (en) One kind can automatically reset launching tube bonnet
CN103939218B (en) Turbofan engine imported equipments and parts bird bullet percussion device
CN106005435A (en) Pneumatic parachute opening system for parachute of unmanned aerial vehicle
CN205880022U (en) Fireproof waterproof ammeter case
CN104973249A (en) Effector With Ejectable Stealth Shell
US9045228B2 (en) Arrangement at an aircraft of a dispenser unit for countermeasures
CN110030879A (en) A kind of unmanned aerial vehicle onboard platform catches net emitter
CN205396525U (en) Many rotors armed helicopter
US3409254A (en) Safety aircraft

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant