CN206785219U - It is a kind of that lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically - Google Patents

It is a kind of that lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically Download PDF

Info

Publication number
CN206785219U
CN206785219U CN201720816444.1U CN201720816444U CN206785219U CN 206785219 U CN206785219 U CN 206785219U CN 201720816444 U CN201720816444 U CN 201720816444U CN 206785219 U CN206785219 U CN 206785219U
Authority
CN
China
Prior art keywords
twisted piece
piece spring
lock
slide rail
lid
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
Application number
CN201720816444.1U
Other languages
Chinese (zh)
Inventor
陈友伟
陈献平
包宇兵
骆洪志
黄诚
张希
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.)
CHINA GREAT WALL INDUSTRY Corp
China Academy of Launch Vehicle Technology CALT
Beijing Institute of Astronautical Systems Engineering
Original Assignee
CHINA GREAT WALL INDUSTRY Corp
China Academy of Launch Vehicle Technology CALT
Beijing Institute of Astronautical Systems Engineering
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 CHINA GREAT WALL INDUSTRY Corp, China Academy of Launch Vehicle Technology CALT, Beijing Institute of Astronautical Systems Engineering filed Critical CHINA GREAT WALL INDUSTRY Corp
Priority to CN201720816444.1U priority Critical patent/CN206785219U/en
Application granted granted Critical
Publication of CN206785219U publication Critical patent/CN206785219U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Underground Structures, Protecting, Testing And Restoring Foundations (AREA)

Abstract

It is a kind of that lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically; including mouth frame, cover plate, twisted piece spring hinge component and slide rail lock set; for Aircraft structure; automatic closing can be realized after the plug Automatic-falling of ground, protects aircraft inner structure and instrument from the influence of Aerodynamic Heating.Twisted piece spring hinge is buried in ingehious design, twisted piece spring is placed in the hollow circuit cylinder that cover plate is integrally machined, applied by the torsional deflection of twisted piece spring to cover plate and close driving force, design Straight pull sliding track lock in addition, dead bolt and operation pull bar are located on the same straight line in lock body, reasonable stress, dead bolt motion are more smooth.Built-in twisted piece spring hinge and closing Straight pull sliding track lock cause structure in closing space, have dust-proof and solar heat protection ability, and installation operation is convenient, and the whole automatic reliability for closing lid is high.

Description

It is a kind of that lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically
Technical field
The utility model is related to it is a kind of lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically, belong to flight Device structure-design technique field.
Background technology
As Flight Vehicle Structure is constantly brought forth new ideas, at present automatic closing lid mainly have problems with:
(1) assembly reliability is poor.Because part is more, fit dimension is more, tolerance is larger after the completion of assembling, and can not meet will Ask, it is necessary to artificially repair, have a strong impact on the reliability of automatic closing function;
(2) environmental suitability is poor.Aircraft transport, storage and flight environment of vehicle complexity are various, and dust-proof solar heat protection is proposed more High requirement.
For problem above, current automatic closing lid using the steel wire torsion spring of leakage, can not meet above-mentioned requirements, The lid development of new environment must be carried out being applicable.
Utility model content
Technology of the present utility model solves problem:Overcome the deficiencies in the prior art, there is provided one kind is cut with scissors using twisted piece spring The slide rail locking-type aircraft of chain closes lid automatically, and lid has auto-lock function, and assembly reliability is high, being capable of dust-proof solar heat protection.
Technical solution of the present utility model is:
It is a kind of that lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically, including:Mouth frame, cover plate, twisted piece spring Hinge component and slide rail lock set;
One end of cover plate is connected by twisted piece spring hinge component with mouth frame so that cover plate overturns and is bonded with respect to mouth frame;Patch During conjunction, the other end of cover plate is realized by slide rail lock set and mouth frame to be locked.
One end that cover plate is connected by twisted piece spring hinge component with mouth frame, hollow round tubular structure is provided with, the hollow circle The one end open of tubular structure, cylindric indent is provided with, the other end is a cylindric protrusion, and is set in the cylindric protrusion Limited location groove.
Twisted piece spring hinge component includes twisted piece spring component, torsion spring fixed seat and torsion spring blanking cover;
Twisted piece spring component is arranged on the hollow round tubular inside configuration, and one end of twisted piece spring component passes through the cylinder The stopper slot progress set in shape protrusion is circumferential spacing, and the cylindric protrusion is engaged with torsion spring blanking cover and cylindric protrusion exists Rotated in torsion spring blanking cover;
The other end of twisted piece spring component is extend into torsion spring fixed seat, by the protrusion cylindrical-shaped structure of torsion spring fixed seat The stopper slot of setting carries out circumferential spacing, the protrusion cylindrical-shaped structure of torsion spring fixed seat and one end of the hollow round tubular structure Cylindric indent be engaged;
Torsion spring fixed seat and torsion spring blanking cover are fixedly mounted on mouthful frame.
The twisted piece spring component is that multi-disc identical strip spring steel plate stacks to be formed.
The slide rail lock set includes lock, lock housing, dead bolt, lock body blanking cover, spring and pull bar;
Lock is fixed on mouthful frame, is fixed on the cover board with latching relative lock housing, pull bar sequentially pass through lock body blanking cover and Spring, it is fixedly connected, is placed in lock housing with dead bolt, lock body blanking cover is connected by screw thread and lock housing.
Lock housing is stretched out in the end of the dead bolt, and there is fillet the end of dead bolt.Fit clearance between dead bolt and lock housing is 0.5mm, make dead bolt in lock housing slidably.The axis of lock housing, pull bar and dead bolt overlaps.Matching somebody with somebody between pull bar and lock body blanking cover Conjunction gap is 0.5mm.Dead bolt and lock carry out chromium plating process.
The beneficial effect of the utility model compared with prior art is:
(1) technical solutions of the utility model have automatic closing function, and the twisted piece spring hinge and sliding track lock of ingehious design carry High aircraft closes the reliability of lid automatically.
(2) the twisted piece spring buried in can avoid the spring force during aircraft high-speed flight from failing, and improve lid Solar heat protection ability.
(3) Straight pull sliding track lock is designed, dead bolt and operation pull bar are located on the same straight line in lock body, reasonable stress, lock Tongue motion is more smooth.
(5) twisted piece spring hinge and sliding track lock have blanking cover to connect in assembling, and ensure after assembling in hinge and lock body to be close Space is sealed, there is dust reduction capability.
Brief description of the drawings
Fig. 1 is the automatic global picture for closing lid,
Fig. 2 is the automatic front view for closing lid lock-out state,
Fig. 3 is lock body sectional view,
Fig. 4 is built-in twisted piece spring hinge sectional view,
Fig. 5 is twisted piece spring component.
Embodiment
The utility model is applied to the lid with automatic closing function.This lid is after aircraft plug from falling, non- Human intervention situation the lower flap can close automatically.And buried in using and turn round chip type spring and sliding track lock, there is dust-proof heat resistance Can, reliable lock is high.
As shown in Figure 1, 2, closed automatically using the slide rail locking-type aircraft of twisted piece spring hinge the utility model proposes a kind of Remain silent lid, it is characterised in that including:Mouth frame 1, cover plate 2, twisted piece spring hinge component and slide rail lock set;One end of cover plate 2 passes through Twisted piece spring hinge component is connected with mouth frame 1 so that cover plate 2 overturns and is bonded with respect to mouthful frame 1;During fitting, the other end of cover plate 2 leads to Cross slide rail lock set and realize locking with mouth frame 1.
One end that cover plate 2 is connected by twisted piece spring hinge component with mouth frame 1, is provided with hollow round tubular structure, and this is hollow The one end open of round tube shape structure, cylindric indent is provided with, the other end is a cylindric protrusion, and is set in the cylindric protrusion It is equipped with stopper slot.
Steel wire torsion spring is replaced using twisted piece spring, is built in lid rotating shaft, is formed integrally the hinge of formula.Twisted piece spring is according to mouth The driving force size of lid, combined from the high-strength hot processing spring steel plate of different-thickness.In flight course, spring does not have Have in harsh flight environment of vehicle, improve the solar heat protection ability of lid.As shown in Figure 4,5, twisted piece spring hinge component includes Twisted piece spring component 3, torsion spring fixed seat 4 and torsion spring blanking cover 6;
Twisted piece spring component 3 is arranged on the hollow round tubular inside configuration, and one end of twisted piece spring component 3 passes through the circle The stopper slot set in column protrusion carries out circumferential spacing, and the cylindric protrusion is engaged and cylindric convex with torsion spring blanking cover 6 Go out and rotated in torsion spring blanking cover 6;
The other end of twisted piece spring component 3 is extend into torsion spring fixed seat 4, passes through the cylindric knot of the protrusion of torsion spring fixed seat 4 The stopper slot set in structure carries out circumferential spacing, the protrusion cylindrical-shaped structure of torsion spring fixed seat 4 and the hollow round tubular structure The cylindric indent of one end be engaged;
Torsion spring fixed seat 4 and torsion spring blanking cover 6 are fixedly mounted on mouthful frame 1.
Stack to be formed as shown in figure 5, the twisted piece spring component 3 is multi-disc identical strip spring steel plate.Spring steel plate Spring steel plate is handled from high-strength hot, thickness and size selection can be carried out according to the size and driving force of lid.
As shown in figure 3, the slide rail lock set includes lock 9, lock housing 10, dead bolt 11, lock body blanking cover 12, spring 13 and drawn Bar 14;Lock 9 is fixed on mouthful frame 1, is fixed on 9 relative lock housings 10 of lock on cover plate 2, pull bar 14 sequentially passes through lock body and blocked up Lid 12 and spring 13, are fixedly connected with dead bolt 11, are placed in lock housing 10, and lock body blanking cover 12 is connected by screw thread and lock housing 10.Lock Body blanking cover 12 can ensure that inside lock body be closing space, avoid fifth wheel from entering, have dust reduction capability.
Lock housing 10 is stretched out in the end of dead bolt 11, and there is fillet the end of dead bolt 11.Cooperation between dead bolt 11 and lock housing 10 Gap is 0.5mm, make dead bolt 11 in lock housing 10 slidably.The axis of lock housing 10, pull bar 14 and dead bolt 11 is overlapped, and operation is drawn Bar 14 is changed to Straight pull, avoids the side force for being opened and closed lid from influenceing dead bolt 11 and slides, and pull bar 14 and dead bolt 11 are in same cunning On dynamic rail road, stress is more rationally uniform.Fit clearance between pull bar 14 and lock body blanking cover 12 is 0.5mm.Dead bolt 11 and lock Button 9 carries out chromium plating process, improves the hardness and smoothness of contact surface, and it is smooth to ensure that dead bolt 11 slides.
Operation principle
In use, cover plate is opened certain angle by external force, the cover plate being now connected with twisted piece spring component both ends is cylindric convex Going out the stopper slot of interior setting and circumferentially opposed motion occurs for the stopper slot of torsion spring fixed seat, twisted piece spring component twists deformation, The driving force of opposite direction is produced to cover plate, so that cover plate returns to initial position.When cover plate moves to certain position, dead bolt Contacted with lock, both contact surfaces are separately designed as fillet and inclined-plane.Lock is integrally fixed on mouthful frame, can not be moved, institute It is compressed into dead bolt in dead bolt and lock relative movement in lock body.When cover plate, which moves to, to be contacted with mouth frame, dead bolt with Lock no longer contacts.Now dead bolt moves out in the presence of lock body inner spring power, returns to initial position, and in lock Constraint lower cover can not continue to move, so as to realize that lid locks.
Embodiment
(1) part covers together, ensures that all fit tolerances meet the requirements, especially lock body;
(2) twisted piece spring component is injected into torsion spring fixed seat, fixed using screw in compression;
(3) twisted piece spring is injected in cover plate square hole, the cover plate other end injects torsion spring fixed seat;
(4) cover plate one end blocks torsion spring blanking cover, and torsion spring blanking cover and torsion spring fixed seat are spirally connected and are riveted on mouthful frame respectively;
(5) it is spirally connected with pull bar through spring and blanking cover with dead bolt, is put into together in lock housing and blanking cover and lock housing are spirally connected fixation;
(6) by the lock body assembled riveting on the cover board;
(7) installation lock, it is ensured that the gap between lock body is 2mm;
(8) functional check, multiple lid opening and closing test is carried out.
Built-in twisted piece spring hinge and closing Straight pull sliding track lock cause structure in closing space, have dust-proof and solar heat protection Ability, and installation operation is convenient, and the whole automatic reliability for closing lid is high.

Claims (10)

1. a kind of close lid automatically using the slide rail locking-type aircraft of twisted piece spring hinge, it is characterised in that including:Mouth frame (1), Cover plate (2), twisted piece spring hinge component and slide rail lock set;
One end of cover plate (2) is connected by twisted piece spring hinge component with mouth frame (1) so that cover plate (2) with respect to mouth frame (1) upset and Fitting;During fitting, the other end of cover plate (2) is realized by slide rail lock set and mouth frame (1) to be locked.
2. it is according to claim 1 it is a kind of lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically, it is special Sign is:One end that cover plate (2) is connected by twisted piece spring hinge component with mouth frame (1), is provided with hollow round tubular structure, in this The one end open of empty round tube shape structure, cylindric indent being provided with, the other end is a cylindric protrusion, and in the cylindric protrusion It is provided with stopper slot.
3. it is according to claim 2 it is a kind of lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically, it is special Sign is:Twisted piece spring hinge component includes twisted piece spring component (3), torsion spring fixed seat (4) and torsion spring blanking cover (6);
Twisted piece spring component (3) is arranged on the hollow round tubular inside configuration, and one end of twisted piece spring component (3) passes through the circle The stopper slot set in column protrusion carries out circumferential spacing, and the cylindric protrusion is engaged and cylindric with torsion spring blanking cover (6) Protrusion rotates in torsion spring blanking cover (6);
The other end of twisted piece spring component (3) is extend into torsion spring fixed seat (4), and the protrusion by torsion spring fixed seat (4) is cylindric The stopper slot set in structure carries out circumferential spacing, protrusion cylindrical-shaped structure and the hollow round tubular of torsion spring fixed seat (4) The cylindric indent of one end of structure is engaged;
Torsion spring fixed seat (4) and torsion spring blanking cover (6) are fixedly mounted on a mouthful frame (1).
4. it is according to claim 3 it is a kind of lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically, it is special Sign is:The twisted piece spring component (3) is that multi-disc identical strip spring steel plate stacks to be formed.
5. it is according to claim 1 it is a kind of lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically, it is special Sign is:The slide rail lock set includes lock (9), lock housing (10), dead bolt (11), lock body blanking cover (12), spring (13) and drawn Bar (14);
Lock (9) is fixed on a mouthful frame (1), is fixed on lock (9) relative lock housing (10) on cover plate (2), pull bar (14) according to It is secondary to pass through lock body blanking cover (12) and spring (13), it is fixedly connected, is placed in lock housing (10) with dead bolt (11), lock body blanking cover (12) is logical Screw thread is crossed to be connected with lock housing (10).
6. it is according to claim 5 it is a kind of lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically, it is special Sign is:Lock housing (10) is stretched out in the end of the dead bolt (11), and there is fillet the end of dead bolt (11).
7. it is according to claim 6 it is a kind of lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically, it is special Sign is:Fit clearance between dead bolt (11) and lock housing (10) is 0.5mm, makes dead bolt (11) in lock housing (10) interior free skating It is dynamic.
8. it is according to claim 5 it is a kind of lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically, it is special Sign is:The axis of lock housing (10), pull bar (14) and dead bolt (11) overlaps.
9. it is according to claim 1 it is a kind of lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically, it is special Sign is:Fit clearance between pull bar (14) and lock body blanking cover (12) is 0.5mm.
10. it is according to claim 5 it is a kind of lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically, it is special Sign is:Dead bolt (11) and lock (9) carry out chromium plating process.
CN201720816444.1U 2017-07-07 2017-07-07 It is a kind of that lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically Active CN206785219U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720816444.1U CN206785219U (en) 2017-07-07 2017-07-07 It is a kind of that lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720816444.1U CN206785219U (en) 2017-07-07 2017-07-07 It is a kind of that lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically

Publications (1)

Publication Number Publication Date
CN206785219U true CN206785219U (en) 2017-12-22

Family

ID=60718069

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720816444.1U Active CN206785219U (en) 2017-07-07 2017-07-07 It is a kind of that lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically

Country Status (1)

Country Link
CN (1) CN206785219U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108674629A (en) * 2018-05-22 2018-10-19 西北工业大学 A kind of mechanism type sealing cover of aircraft store mounting point
CN111457796A (en) * 2020-04-13 2020-07-28 北京中科宇航技术有限公司 Lock catch and cover of automatic closing cover for spaceflight and carrier rocket
CN112249371A (en) * 2020-10-30 2021-01-22 北京空间飞行器总体设计部 Return capsule pressure release hole plugging device
CN113790002A (en) * 2021-09-07 2021-12-14 贵州航天天马机电科技有限公司 Automatic open locking the hinge mechanism

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108674629A (en) * 2018-05-22 2018-10-19 西北工业大学 A kind of mechanism type sealing cover of aircraft store mounting point
CN108674629B (en) * 2018-05-22 2021-10-12 西北工业大学 Mechanism type sealing opening cover of aircraft external hanging point
CN111457796A (en) * 2020-04-13 2020-07-28 北京中科宇航技术有限公司 Lock catch and cover of automatic closing cover for spaceflight and carrier rocket
CN112249371A (en) * 2020-10-30 2021-01-22 北京空间飞行器总体设计部 Return capsule pressure release hole plugging device
CN113790002A (en) * 2021-09-07 2021-12-14 贵州航天天马机电科技有限公司 Automatic open locking the hinge mechanism

Similar Documents

Publication Publication Date Title
CN206785219U (en) It is a kind of that lid is closed using the slide rail locking-type aircraft of twisted piece spring hinge automatically
CN203358716U (en) Plastic charging opening cover structure
CN203374089U (en) Switch cabinet door lock mechanism
CN103132823B (en) A kind of automobile right front door lock assembly
CN202520104U (en) Engine cover lock pin
CN203684801U (en) Secondary opening mechanism for internal opening of automobile door lock
CN104005609A (en) Middle door lock clamping device
CN205531862U (en) Integrated hinge of flexible roller formula
CN203925033U (en) Front door lock gripping mechanism
CN209870558U (en) Side wall charging port
CN207078073U (en) A kind of push type opening structure of automobile glove box
CN102561869B (en) Limiting oil-filling valve
CN203925034U (en) Opening mechanism in middle grille body
CN205654200U (en) Locking device
CN212249594U (en) Common power source locking device based on displacement difference
CN203925037U (en) Door lock in one
CN205220819U (en) Opening/closing structure of electric vehicle charging flap
CN210264264U (en) Opening and closing position switching and locking mechanism of cover door actuator
CN107630919B (en) Spring piece type rotating piece opening and closing control device and control method
CN107479423B (en) Engagement type rotating member folding control device and control method
CN219197008U (en) Sliding plug door locking mechanism
CN206581742U (en) A kind of driver of band PUSH PUSH structures
CN209600264U (en) Oil filler cap structure assembly and automobile
CN111775845A (en) Storage box opening structure for automobile main driving and using method thereof
CN210343016U (en) Handle structure

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant