CN108639381A - A kind of pop-up type locking relieving mechanism - Google Patents

A kind of pop-up type locking relieving mechanism Download PDF

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Publication number
CN108639381A
CN108639381A CN201810267190.1A CN201810267190A CN108639381A CN 108639381 A CN108639381 A CN 108639381A CN 201810267190 A CN201810267190 A CN 201810267190A CN 108639381 A CN108639381 A CN 108639381A
Authority
CN
China
Prior art keywords
hand pawl
left hand
right hand
pawl
pop
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.)
Pending
Application number
CN201810267190.1A
Other languages
Chinese (zh)
Inventor
董毅
于爽
王浩淼
罗小乐
蒋秋香
经贵如
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.)
Shanghai Aerospace System Engineering Institute
Original Assignee
Shanghai Aerospace System Engineering Institute
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 Shanghai Aerospace System Engineering Institute filed Critical Shanghai Aerospace System Engineering Institute
Priority to CN201810267190.1A priority Critical patent/CN108639381A/en
Publication of CN108639381A publication Critical patent/CN108639381A/en
Pending legal-status Critical Current

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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/18Means for stabilising antennas on an unstable platform
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/27Adaptation for use in or on movable bodies
    • H01Q1/28Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • H01Q1/288Satellite antennas
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/02Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
    • H01Q3/08Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation

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  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Clamps And Clips (AREA)

Abstract

The invention discloses a kind of pop-up types to lock relieving mechanism, including pedestal and the left hand pawl and right hand pawl that are located at the pedestal both sides, wherein, close up the left hand pawl and the right hand pawl can will be locked mechanism locking, when releasing locking state, movement outward discharges the mechanism that is locked to the left hand pawl and right hand pawl respectively, while continuing the spacing lever moved outward equipped with the limitation left hand pawl and the right hand pawl on the pedestal.The present invention is widely used in driving space photoelectricity class load and rotates and be fixedly supported on a certain position, uses gapless, self-locking design, compared to existing technology, has the advantages that expansion process is stable, in-placing precision is high, locking rigidity is high.

Description

A kind of pop-up type locking relieving mechanism
Technical field
The invention belongs to aerospace field of electromechanical technology, more particularly to a kind of pop-up type locks relieving mechanism.
Background technology
Directing mechanism is that satellite antenna is realized to the important execution unit of target following, orientation, is modern spacecraft system Important component.In order to improve the gain of satellite antenna, antenna aperture and weight is increasing, beam angle of antenna Become very narrow, in order to increase the slewing area of satellite antenna, and avoids in rotation process encountering around satellite body or antenna Other load, need launching phase by antenna gathering be pressed on satellite side, after entering the orbit by antenna expansion be supported on it is separate Celestial body a certain position remote enough, then rotated and oriented, therefore, the error of expanded angle is by the fixation as satellite antenna Error in pointing, this error always exist, it can be seen that, the pointing accuracy that satellite antenna can be improved in precision of expansion is improved, is had Critically important engineering significance;In addition, as technology develops, the requirement to the platform stable degree of spacecraft is also higher and higher, to boat The interference requirement generated in its device extravehicular activity component rotation process is also very harsh.Need satellite antenna in the fundamental frequency of unfolded state It is as high as possible, and maximum to fundamental frequency influence factor is system weight and locking rigidity, it is seen that improve the lock of expansion locking mechanism Tight rigidity is critically important to satellite antenna and spacecraft platform.
Some existing satellite antennas, the holding torque for only relying on motor realizes that the position of directing mechanism is kept, but keeps Rigidity is low and is easily influenced by external interference.Some satellite antennas are unfolded by passive spring or torsional spring, rely on lock afterwards in place Positioning, but expansion process is uncontrollable, impact is big in place, and lock-bit precision is low and rigidity is low due to locking device gap is excessive.
Invention content
The present invention provides a kind of pop-up type locking relieving mechanism, rigid to have solved lock-bit precision of the existing technology and locking Degree is inadequate, and expansion process is uncontrollable, and impacts big technical problem in place.
Technical scheme is as follows:
A kind of pop-up type locking relieving mechanism, including pedestal and the left hand pawl and right hand pawl that are located at the pedestal both sides, Wherein, close up the left hand pawl and the right hand pawl can will be locked mechanism locking, when releasing locking state, the left side Movement outward discharges the mechanism that is locked respectively for paw and right hand pawl, while the limitation left hand is equipped on the pedestal Pawl and the right hand pawl continue the spacing lever moved outward.
Preferably, the left hand pawl, the right hand pawl are located at the pedestal by torsion axis and torsionspring Both sides so that the left hand pawl, the right hand pawl obtain the torque moved outward.
Preferably, the torsion axis and the torsionspring are located at the lower end of the left hand pawl, and are connected to institute On the pedestal stated;The torsion axis and the torsionspring are located at the lower end of the right hand pawl, and are connected to described On pedestal.
Preferably, it is equipped with the fixed compressor arm with the right hand pawl locking state on the left hand pawl, while The right hand pawl is equipped with the cut-out compressor arm to release the cutter of locking state.
Preferably, the compressor arm is located at the top half of the left hand pawl, when locking described in compressor arm pass through The through-hole of the cutter is simultaneously fixedly connected by the end of thread of the compressor arm with the right hand pawl.
Preferably, the side of the compressor arm on the left hand pawl described in face is equipped with the pressure after recycling cut-out The compression headgear of tight bar.
Preferably, the link that a kind of pop-up type of the invention locking relieving mechanism further includes and the mechanism that is locked connects, The left hand pawl and the right hand pawl embrace and by way of the link locked.
Preferably, the knead dough of embracing of the left hand pawl and the right hand pawl and the link is " V " type structure, Simultaneously in the both sides of the link equipped with the end face for matching locking with " V " type structure.
Preferably, locking state, the left hand pawl and the right hand pawl and the pedestal are in 90 °, are deployed into Position state, the left hand pawl and the right hand pawl are with the pedestal finally at 30 °.
Preferably, the torsion axis uses Ti materials, axial plane to coat MoS2Solid lubricant film;The torsionspring is adopted With 1Cr18Ni9 materials, locking state torque is 0.4N.m, and it is 0.17N.m to expand in place state torque.
Preferably, the surface in the left hand pawl and right hand pawl is coated with carbonization tungsten film, carbonization tungsten film requirement:Coating Thickness is 0.2mm ± 0.05mm, and the left hand pawl and right hand pawl pawl is embraced and the rear coupling mechanism force having not less than 7100N.
Compared with prior art, beneficial effects of the present invention are as follows:
A kind of pop-up type of the present invention locks relieving mechanism, is widely used in driving space photoelectricity class load and rotates and fix It is supported on a certain position, uses gapless, self-locking design, compared to existing technology, has expansion process stable, smart in place The advantage that degree is high, locking rigidity is high.
Certainly, it implements any of the products of the present invention and does not necessarily require achieving all the advantages described above at the same time.
Description of the drawings
Fig. 1 is that a kind of pop-up type of the present invention locks the structural schematic diagram of relieving mechanism;
Fig. 2 is that a kind of pop-up type of the present invention locks the locking state schematic diagram of relieving mechanism;
Fig. 3 expands in place status diagram for a kind of pop-up type locking relieving mechanism of the invention.
Specific implementation mode
Present invention will be further explained below with reference to specific examples.It should be understood that these embodiments are merely to illustrate this hair It is bright, rather than limit protection scope of the present invention.Those skilled in the art change according to what the present invention made in practical applications Into and adjustment, still fall within protection scope of the present invention.
In order to better illustrate the present invention, the present invention is described in detail below with attached drawing.
As shown in Figures 1 to 3, a kind of pop-up type of the invention locks relieving mechanism, including pedestal 7 and is located at the pedestal The left hand pawl 4 and right hand pawl 9 of 7 both sides, wherein close up the left hand pawl 4 and the right hand pawl 9 can will be locked mechanism lock Tightly, when releasing locking state, movement release outward is locked mechanism to being deployed into respectively for the left hand pawl 4 and right hand pawl 9 Position state, while being moved outward equipped with the limitation left hand pawl 4 and the right hand pawl 9 continuation on the pedestal 7 Spacing lever 6.
Specifically, the present embodiment by between the left hand pawl 4 and right hand pawl 9 of pedestal 7 and both sides be arranged torsion axis 8 and Torsionspring 5 so that once releasing locking state, unlock, but this hair are completed in movement outward respectively for left hand pawl 4 and right hand pawl 9 It is bright to be not limited to the set-up mode:The left hand pawl 4, the right hand pawl 9 are located at institute by torsion axis 8 and torsionspring 5 The both sides for the pedestal 7 stated so that the left hand pawl 4, the right hand pawl 9 obtain the torque moved outward.
Further, the torsion axis 8 and the torsionspring 5 are located at the lower end of the left hand pawl 4, and are connected to On the pedestal 7;The torsion axis 8 and the torsionspring 5 are located at the lower end of the right hand pawl 9, and are connected to On the pedestal 7.
In addition, being preferable to provide in the present embodiment one kind:Fixed and described right hand pawl is equipped on the left hand pawl 4 The compressor arm 2 of 9 locking states, i.e., close up left hand pawl 4 and right hand pawl 9 will be locked mechanism locking when fix the locking state, The cut-out compressor arm 2 is equipped on the right hand pawl 9 simultaneously to release the cutter 10 of locking state, that is, passes through cutting Compressor arm 2 is cut off in the igniting of device 10 releases locking state, and left hand pawl 4 and right hand pawl 9 move under the action of torque outward To the state that expands in place, the mechanism that is locked is discharged.
In the present embodiment, the possible a kind of setting of the compressor arm 2:The compressor arm 2 is located at the left hand The top half of pawl 4, when locking described in compressor arm 2 pass through the through-hole 101 of the cutter 10 and pass through the compression The end of thread 21 of bar 2 is fixedly connected with the right hand pawl 9.
The side of compressor arm 2 also on the left hand pawl 4 described in face is equipped with the compression after recycling cut-out The compression headgear 3 of bar 2, after 2 cleaved device of compressor arm, 10 ignition cut, the compressor arm 2 positioned at 4 side of left hand pawl is recovered in hold-down head Set 3 avoids falling into outer space, and would not be fallen into positioned at the compressor arm 2 of 9 side of right hand pawl because being screwed on right hand pawl 9 Outer space.
For the ease of realizing that the locking relieving mechanism of the present invention locks the mechanism that is locked, a kind of pop-up type of the invention locking Relieving mechanism further includes and the link 1 for the mechanism connection that is locked, the left hand pawl 4 and the right hand pawl 9 by embracing and Mode the link 1 is locked.The present invention it is a kind of possible armful and locking mode it is as follows, but the present invention do not limit with Lower structure:The knead dough of embracing of the left hand pawl 4 and the right hand pawl 9 and the link 1 is " V " type structure 11, together When be equipped in the both sides of the link 1 and match with " V " type structure the end face 12 of locking, therefore, locking of the invention is released Laying mechanism, when locking state, the left hand pawl 4 and the right hand pawl 9 and the pedestal 7 are in 90 °, left and right claw with Link is embraced with after, side clearance 0.5mm, as shown in Fig. 2, when expanding in place state, the left hand pawl 4 and the right side Paw 9 is last at 30 ° with the pedestal 7, as shown in Figure 3.
In this regard, torsion axis 8 of the present invention uses Ti materials, axial plane to coat MoS2Solid lubricant film;The torsion It is 0.4N.m that spring 5, which uses 1Cr18Ni9 materials, locking state torque, and it is 0.17N.m to expand in place state torque;The left side Surface spraying in paw 4 and right hand pawl 9 has carbonization tungsten film, carbonization tungsten film requirement:Coating layer thickness is 0.2mm ± 0.05mm, WC Anchoring strength of coating is more than or equal to 45MPa;When service load is 3.0KN, the confficient of static friction of coatings friction pairs is more than or equal to 0.5, and the left hand pawl 4 and 9 pawl of right hand pawl is embraced and the rear coupling mechanism force having not less than 7100N.
A kind of pop-up type of the present invention locks relieving mechanism, and link 1 is fixedly connected with the mechanism that is locked, by left jamming claw 4, Right jamming claw 9 is embraced and is fixed with link 1, and is fixed by compressor arm 2 and realized locking, and torsionspring 5 is in compressive state at this time, Torque is 0.4Nm, when reaching predetermined state, is lighted a fire by cutter 10 and cuts off compressor arm 2, and the release of 5 torque of torsionspring is driven Dynamic left and right claw rotary expansion is simultaneously detached from link 1, in the process as torsion 5 torque of bullet tapers into, driving left and right The acceleration of claw also tapers into, and due to the effect of limited block 6, left and right claw rotation angle is limited in 60 °, due to arriving Position retrotorsion spring 5 still has the surplus torque of 0.17Nm, left and right claw to be pressed in a certain extent on limited block 6, locks Tight relieving mechanism state determines that the link institution where he works realizes release.
The present invention is widely used in spacecraft motion transmitter section and effectively fixes, and is reliably discharged after entering the orbit, and has Have the advantages that simple in structure, bearing capacity is strong, separation is reliable.
Present invention disclosed above preferred embodiment is only intended to help to illustrate the present invention.There is no detailed for preferred embodiment All details are described, are not limited the invention to the specific embodiments described.Obviously, according to the content of this specification, It can make many modifications and variations.These embodiments are chosen and specifically described to this specification, is in order to preferably explain the present invention Principle and practical application, to enable skilled artisan to be best understood by and utilize the present invention.The present invention is only It is limited by claims and its full scope and equivalent.

Claims (10)

1. a kind of pop-up type locks relieving mechanism, which is characterized in that including pedestal and the left hand pawl for being located at the pedestal both sides With right hand pawl, wherein close up the left hand pawl and the right hand pawl can will be locked mechanism locking, shape is locked when releasing Movement outward discharges the mechanism that is locked respectively for state, the left hand pawl and right hand pawl, while limit is equipped on the pedestal The system left hand pawl and the right hand pawl continue the spacing lever moved outward.
2. pop-up type according to claim 1 locks relieving mechanism, which is characterized in that the left hand pawl, the right side Paw is located at the both sides of the pedestal by torsion axis and torsionspring so that the left hand pawl, the right hand pawl Obtain the torque moved outward.
3. pop-up type according to claim 2 locks relieving mechanism, which is characterized in that the torsion axis and the torsion Turn spring and be located at the lower end of the left hand pawl, and is connected on the pedestal;The torsion axis and the torsion bullet Spring is located at the lower end of the right hand pawl, and is connected on the pedestal.
4. pop-up type according to claim 1 or 3 locks relieving mechanism, which is characterized in that worn on the left hand pawl There is the fixed compressor arm with the right hand pawl locking state, while being equipped with the cut-out compressor arm on the right hand pawl To release the cutter of locking state.
5. pop-up type according to claim 4 locks relieving mechanism, which is characterized in that the compressor arm is located at described The top half of left hand pawl, when locking described in compressor arm pass through the through-hole of the cutter and pass through the compressor arm The end of thread is fixedly connected with the right hand pawl.
6. pop-up type according to claim 5 locks relieving mechanism, which is characterized in that the face institute on the left hand pawl The side for the compressor arm stated is equipped with the compression headgear of the compressor arm after recycling cut-out.
7. pop-up type locks relieving mechanism according to claim 1 or 5, which is characterized in that further include and the mechanism that is locked The link of connection, the left hand pawl and the right hand pawl embrace and by way of the link locked.
8. pop-up type according to claim 7 locks relieving mechanism, which is characterized in that the left hand pawl and the right side The knead dough of embracing of paw and the link is " V " type structure, while being equipped with and " V " type knot in the both sides of the link Structure matches the end face of locking.
9. pop-up type according to claim 8 locks relieving mechanism, which is characterized in that locking state, the left hand pawl It is in 90 ° with the right hand pawl and the pedestal, expand in place state, the left hand pawl and the right hand pawl and institute The pedestal stated is finally at 30 °.
10. pop-up type according to claim 1 locks relieving mechanism, which is characterized in that the left hand pawl and right hand pawl Interior surface is coated with carbonization tungsten film, carbonization tungsten film requirement:Coating layer thickness is 0.2mm ± 0.05mm, and the left hand pawl It is embraced with right hand pawl pawl and rear with the coupling mechanism force for being not less than 7100N;The torsion axis uses Ti materials, axial plane to coat MoS2Gu Body lubricating film;It is 0.4N.m that the torsionspring, which uses 1Cr18Ni9 materials, locking state torque, expands in place state torque For 0.17N.m.
CN201810267190.1A 2018-03-28 2018-03-28 A kind of pop-up type locking relieving mechanism Pending CN108639381A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109616741A (en) * 2018-11-15 2019-04-12 上海宇航系统工程研究所 Active matrix driving two-dimensional development formula antenna
CN111409876A (en) * 2020-04-09 2020-07-14 北京控制工程研究所 Tool box device for locking multi-degree-of-freedom mechanism
CN114180102A (en) * 2021-12-17 2022-03-15 清华大学深圳国际研究生院 Locking device for movable and deployable mechanism on spacecraft
CN115473053A (en) * 2022-09-22 2022-12-13 深圳航天东方红卫星有限公司 Folding and unfolding satellite-borne yagi antenna locked in encircling mode

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CN108054515A (en) * 2017-10-27 2018-05-18 上海卫星工程研究所 The specific spaceborne two-dimentional driving number being initially directed toward can be achieved and pass antenna system

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EP1595658A1 (en) * 2000-05-30 2005-11-16 Universite Laval Power switching mechanism for selectively connecting a robotic system to a robot tool
CN101934524A (en) * 2009-07-02 2011-01-05 中日龙(襄樊)机电技术开发有限公司 Automatic quick-change fixture tray
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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109616741A (en) * 2018-11-15 2019-04-12 上海宇航系统工程研究所 Active matrix driving two-dimensional development formula antenna
CN111409876A (en) * 2020-04-09 2020-07-14 北京控制工程研究所 Tool box device for locking multi-degree-of-freedom mechanism
CN111409876B (en) * 2020-04-09 2021-10-01 北京控制工程研究所 Tool box device for locking multi-degree-of-freedom mechanism
CN114180102A (en) * 2021-12-17 2022-03-15 清华大学深圳国际研究生院 Locking device for movable and deployable mechanism on spacecraft
CN114180102B (en) * 2021-12-17 2023-08-01 清华大学深圳国际研究生院 Locking device for movable and expandable mechanism on spacecraft
CN115473053A (en) * 2022-09-22 2022-12-13 深圳航天东方红卫星有限公司 Folding and unfolding satellite-borne yagi antenna locked in encircling mode

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Application publication date: 20181012