CN106342158B - A kind of guided missile records cabin hatch structure - Google Patents

A kind of guided missile records cabin hatch structure

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Publication number
CN106342158B
CN106342158B CN200710081195.7A CN200710081195A CN106342158B CN 106342158 B CN106342158 B CN 106342158B CN 200710081195 A CN200710081195 A CN 200710081195A CN 106342158 B CN106342158 B CN 106342158B
Authority
CN
China
Prior art keywords
window body
rectangle
hatch
hole
cabin
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.)
Expired - Fee Related
Application number
CN200710081195.7A
Other languages
Chinese (zh)
Inventor
王福山
王晖
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 Airborne Missile Academy
Original Assignee
China Airborne Missile Academy
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 Airborne Missile Academy filed Critical China Airborne Missile Academy
Priority to CN200710081195.7A priority Critical patent/CN106342158B/en
Application granted granted Critical
Publication of CN106342158B publication Critical patent/CN106342158B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The invention belongs to missile airframe structure, relate to the improvement of guided missile being recorded to cabin hatch structure. It comprises records cabin housing [1], hatch board [2], and window body [3], cyclic sealing gasket [4] and sealing ring [7], is characterized in that, hatch board [2] is connected by spring hinge with window body [3]. The present invention makes hatch board [2] and window body [3] realize chain connection, makes the disassembling section of hatch cover panel very flexible, simple, quick and easy, and has sealing protection, safe and reliable feature. Meanwhile, structure of the present invention is small and exquisite simple, handling ease, and easy for installation, cost is low.

Description

A kind of guided missile records cabin hatch structure
Technical field
The invention belongs to missile airframe structure, relate to the improvement of guided missile being recorded to cabin hatch structure.
Background technology
Certain small size air air-to-air missile (AAM) dummy round records cabin and is mainly used to record dummy round in flight trainingThe various data of parameters and pilot operator, judge whether pilot's operation meets specification.After flight training end aircraft lands, first to open the hatchcover that records cabin, carry out dataDownload, remove the operations such as record, then build hatchcover and wait for flight training next time. Due to flightFrequent training, user wishes to record the disassembling section of cabin hatch cover panel can be flexibly, simple, fastPrompt, convenient, open rear deck lid and screw and do not come off, be connected with cabin body all the time, and hatch boardAlso need to there is sealing protection, safe and reliable function. The existing cabin hatch structure that records is: have oneIndividual with rectangle hatch record cabin housing 1, be embedded in the hatch board 2, on above-mentioned rectangle hatchThe individual rectangle hatch below that is positioned at is screwed in the window body 3 recording on the skeleton of cabin, window body 3 footpathsBe slightly larger than the rectangle of above-mentioned rectangle hatch profile to the rectangle of direction profile, the outer surface of window body 3For the arc surface concentric with recording cabin housing 1, the radius of window body 3 outer surfaces with record cabin housing 1Internal diameter identical, the inner surface of window body 3 is plane, hatch board 2 is by multiple screws and windowThe outer surface of body 3 connects, and the outer surface of hatch board 2 is coplanar with the periphery that records cabin housing 1,Between hatch board 2 and the outer surface of window body 3, there is the cyclic sealing gasket 4 of a rectangle, at windowThere is a rectangular through-hole 5 of holding rectangular receptacle the centre of body 3, on the outer surface of window body 3, hasA seal groove 6 around rectangular through-hole 5, sealing ring 7 is arranged in seal groove 6. This hatchThe disassembling section complexity of structure, the consumption time is long; And separate with cabin body after hatch board dismounting, holdEasily lose or polluted.
Summary of the invention
The object of the invention is: propose a kind of hinged cabin hatch structure that records that adopts, make cabinThe disassembling section of velar plate can be flexible, simple, quick and easy, opens rear deck lid and screwDo not come off, be connected with cabin body all the time, and there is sealing protection, safe and reliable feature.
Technical scheme of the present invention is: a kind of guided missile records cabin hatch structure, comprises with rectangular cabinMouthful record cabin housing 1,2, one of hatch boards that are embedded on above-mentioned rectangle hatch are positioned at rectangular cabinBelow mouthful, be screwed in the window body 3 recording on the skeleton of cabin, window body 3 radial direction profilesRectangle is slightly larger than the rectangle of above-mentioned rectangle hatch profile, and the outer surface of window body 3 is and records cabin shellThe arc surface that body 1 is concentric, the radius of window body 3 outer surfaces is identical with the internal diameter that records cabin housing 1,The inner surface of window body 3 is plane, and hatch board 2 is connected with the outer surface of window body 3 by screw,The outer surface of hatch board 2 is coplanar with the periphery that records cabin housing 1, in hatch board 2 and window body 3Outer surface between have the cyclic sealing gasket 4 of a rectangle, have one to hold in the centre of window body 3The rectangular through-hole 5 of rectangular receptacle has one around rectangular through-hole 5 on the outer surface of window body 3Seal groove 6, sealing ring 7 is arranged in seal groove 6, it is characterized in that hatch board 2 and window body3 connect by spring hinge, and its concrete structure is as follows:
(1) between side of window body 3 and rectangular through-hole 5, there is a rectangle through hole 8,The long limit of this rectangle through hole 8 is parallel to the axial direction that records cabin housing 1, at rectangle through hole 8The mid portion of medial surface 9 have two screwed holes, respectively have one to hang down in the both sides of two screwed holesStraight in the narrow groove 10 of rectangle through hole 8;
(2) have a spring shaft 11, it is connected by two pivots 12, one end and the pivot 12 at two endsTwo two circle wind springs 13 that connect and the rotating shaft 14 that connects two two circle wind spring 13 other ends form,Pivot 12 is perpendicular to the wind spring plane of two circle wind springs 13, and rotating shaft 14 is parallel with pivot 12 and keepDistance of shaft centers d=6-12mm; Distance between two two circle wind springs 13 equals rectangle through hole 8 medial surfacesThe centre-to-centre spacing of two narrow grooves 10 on 9, the rotating shaft 14 on spring shaft 11 be positioned at two narrow grooves 10 itBetween medial surface 9 on, two individual pen wind springs 13 lay respectively in two narrow grooves 10; There is a bandHave the spring support 15 that connects half slot, its length is less than two distances between two circle wind springs 15, passes throughScrew 16 is fixed to spring support 12 on two medial surfaces 9 between narrow groove 10, by spring shaft 11Compress;
(3) at hatch board 2 lateral edges corresponding with rectangle through hole 8 in window body 3 with twoThe position of 17, two lugs 17 of individual lug is corresponding with two pivots 12 on spring shaft 11 respectively,On lug 17, record the axial axis hole of cabin housing 1 with being parallel to, two pivots 12 are inserted respectivelyEnter in two axis holes; The outer rim of said lug 17 is protruded the edge of hatch board 2, its projectionBe stuck in the rim under surface that records cabin housing 1 rectangle hatch; Hatch board 2 with two lugsThere is a screw hole at 17 another relative edges, said by outside hatch board 2 and window body 3The screw that surface connects is one and do not deviate from screw 18, and it is screwed in the screwed hole of window body 3, willHatch board 2 is pressed in window body 3.
Advantage of the present invention is: the present invention has overcome the difficulty that hatch tegmental wall is thin, hinge can not be installed,Make hatch board 2 and window body 3 realize chain connection, make the disassembling section of hatch cover panel very cleverAlive, simple, quick and easy, open rear deck lid and screw and do not come off, be connected with cabin body all the time,And there is sealing protection, safe and reliable feature. Meanwhile, structure of the present invention is small and exquisite simple, addsWork is easy, easy for installation, and cost is low.
Brief description of the drawings
Fig. 1 is the stereogram after hatch structure of the present invention is installed on the body of cabin.
Fig. 2 is the explosive view of hatch structure of the present invention.
Detailed description of the invention
Below the present invention is described in further details. Referring to Fig. 1, guided missile of the present invention records cabin, cabinMouth structure, comprise with rectangle hatch record cabin housing 1, be embedded in the cabin on above-mentioned rectangle hatch2, one of lids are positioned at rectangle hatch below and are screwed in the window body 3 recording on the skeleton of cabin,The rectangle of window body 3 radial direction profiles is slightly larger than the rectangle of above-mentioned rectangle hatch profile, window body 3Outer surface be the arc surface concentric with recording cabin housing 1, radius and the note of window body 3 outer surfacesThe internal diameter of record cabin housing 1 is identical, and the inner surface of window body 3 is plane, and hatch board 2 passes through screwBe connected the outer surface of hatch board 2 and the periphery that records cabin housing 1 with the outer surface of window body 3Coplanar, between hatch board 2 and the outer surface of window body 3, there is the cyclic sealing gasket 4 of a rectangle,There is a rectangular through-hole 5 of holding rectangular receptacle in the centre of window body 3, in the appearance of window body 3On face, have a seal groove 6 around rectangular through-hole 5, sealing ring 7 is arranged in seal groove 6, itsBe characterised in that, hatch board 2 is connected by spring hinge with window body 3, and its concrete structure is as follows:
(1) between side of window body 3 and rectangular through-hole 5, there is a rectangle through hole 8,The long limit of this rectangle through hole 8 is parallel to the axial direction that records cabin housing 1, at rectangle through hole 8The mid portion of medial surface 9 have two screwed holes, respectively have one to hang down in the both sides of two screwed holesStraight in the narrow groove 10 of rectangle through hole 8.
(2) have a spring shaft 11, it is connected by two pivots 12, one end and the pivot 12 at two endsTwo two rotating shafts 14 of enclosing wind springs 13 and the two circle of two lists of connection wind spring 13 other ends that connect form,Pivot 12 is perpendicular to the wind spring plane of two circle wind springs 13, and rotating shaft 14 is parallel with pivot 12 and keepDistance of shaft centers d=6-12mm; Distance between two two circle wind springs 13 equals rectangle through hole 8 medial surfacesThe centre-to-centre spacing of two narrow grooves 10 on 9, the rotating shaft 14 on spring shaft 11 be positioned at two narrow grooves 10 itBetween medial surface 9 on, two two circle wind springs 13 lay respectively in two narrow grooves 10; There is a bandHave the spring support 15 that connects half slot, its length is less than two distances between two circle wind springs 13, passes throughScrew 16 is fixed to spring support 15 on two medial surfaces 9 between narrow groove 10, by spring shaft 11Compress.
(3) at hatch board 2 lateral edges corresponding with rectangle through hole 8 in window body 3 with twoThe position of 17, two lugs 17 of individual lug is corresponding with two pivots 12 on spring shaft 11 respectively,On lug 17, record the axial axis hole of cabin housing 1 with being parallel to, two pivots 12 are inserted respectivelyEnter in two axis holes; The outer rim of said lug 17 is protruded the edge of hatch board 2, its projectionBe stuck in the rim under surface that records cabin housing 1 rectangle hatch; Hatch board 2 with two lugsThere is a screw hole at 17 another relative edges, said by outside hatch board 2 and window body 3The screw that surface connects is one and do not deviate from screw 18, and it is screwed in the screwed hole of window body 3, willHatch board 2 is pressed in window body 3.
In one embodiment of the invention, distance of shaft centers d=6.6mm.
The course of work of the present invention is: when dismounting hatch board 2, turn on to deviate from screw 16, upwardsPull-up is also rotated hatch board 2, hatch board 2 can be opened. Under the effect of spring shaft 11, cabinLid 2 is locked in vertical unlocking state.

Claims (1)

1. guided missile records a cabin hatch structure, comprise with rectangle hatch record cabin housing [1],Be embedded in the hatch board [2] on above-mentioned rectangle hatch, one is positioned at rectangle hatch below and is screwedIn the window body [3] recording on the skeleton of cabin, the rectangle of window body [3] radial direction profile is slightly larger thanState the rectangle of rectangle hatch profile, the outer surface of window body [3] is for to record cabin housing [1] concentricArc surface, the radius of window body [3] outer surface is identical with the internal diameter that records cabin housing [1], window body[3] inner surface is plane, and hatch board [2] is connected with the outer surface of window body [3] by screw, cabinThe outer surface of lid [2] is coplanar with the periphery that records cabin housing [1], in hatch board [2] and window body[3] cyclic sealing gasket [4] that has a rectangle between outer surface, has one in the centre of window body [3]The individual rectangular through-hole [5] of holding rectangular receptacle has one around square on the outer surface of window body [3]The seal groove [6] of shape through hole [5], sealing ring [7] is arranged in seal groove [6], it is characterized in that,Hatch board [2] is connected by spring hinge with window body [3], and its concrete structure is as follows:
(1) between side of window body [3] and rectangular through-hole [5], there is a rectangle through hole[8], the long limit of this rectangle through hole [8] is parallel to the axial direction that records cabin housing [1], at rectangleThe mid portion of the medial surface [9] of through hole [8] has two screwed holes, in the both sides of two screwed holesRespectively there is a narrow groove [10] perpendicular to rectangle through hole [8];
(2) have a spring shaft [11], it is by two pivots [12], one end and the pivot [12] at two endsThe rotating shaft [14] of two two circle wind spring [13] other ends of two the two circle wind springs [13] that connect and connectionForm, pivot [12] is perpendicular to the wind spring plane of two circle wind springs [13], rotating shaft [14] and pivot [12]Parallel and keep distance of shaft centers d=6-12mm; Distance between two two circle wind springs [13] equals rectangle and passes throughThe centre-to-centre spacing of two the narrow grooves [10] on through hole [8] medial surface [9], the rotating shaft [14] on spring shaft [11]Be positioned on the medial surface [9] between two narrow grooves [10], two two circle wind springs [13] lay respectively at twoIn narrow groove [10]; Have one with the spring support [15] that connects half slot, its length is less than two two circlesDistance between wind spring [13], by screw [16] by spring support [15] be fixed to two narrow grooves [10] itBetween medial surface [9] upper, spring shaft [11] is compressed;
(3) at a side marginal zone corresponding to the upper rectangle through hole [8] of hatch board [2] and window body [3]Have two lugs [17], the position of two lugs [17] respectively with spring shaft [11] on two pivots[12] correspondence, above records the axial axis hole of cabin housing [1], two axles with being parallel at lug [17]Point [12] inserts respectively in two axis holes; The outer rim of said lug [17] is protruded the limit of hatch board [2]Edge, its projection is stuck in the rim under surface that records cabin housing [1] rectangle hatch; Hatch board [2]And have a screw hole with another relative edge of two lugs [17], said by hatch board[2] screw being connected with the outer surface of window body [3] is one and do not deviate from screw [18], and it is screwed in windowIn the screwed hole of mouth body [3], hatch board [2] is pressed in window body [3].
CN200710081195.7A 2007-04-23 2007-04-23 A kind of guided missile records cabin hatch structure Expired - Fee Related CN106342158B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN200710081195.7A CN106342158B (en) 2007-04-23 2007-04-23 A kind of guided missile records cabin hatch structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN200710081195.7A CN106342158B (en) 2007-04-23 2007-04-23 A kind of guided missile records cabin hatch structure

Publications (1)

Publication Number Publication Date
CN106342158B true CN106342158B (en) 2012-01-18

Family

ID=57797829

Family Applications (1)

Application Number Title Priority Date Filing Date
CN200710081195.7A Expired - Fee Related CN106342158B (en) 2007-04-23 2007-04-23 A kind of guided missile records cabin hatch structure

Country Status (1)

Country Link
CN (1) CN106342158B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108267863A (en) * 2018-01-04 2018-07-10 中国空空导弹研究院 A kind of compact super-resolution imaging optical system
CN109606617A (en) * 2018-11-28 2019-04-12 天津津航技术物理研究所 A kind of supersonic aircraft visible light window assembly

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108267863A (en) * 2018-01-04 2018-07-10 中国空空导弹研究院 A kind of compact super-resolution imaging optical system
CN108267863B (en) * 2018-01-04 2020-11-24 中国空空导弹研究院 Compact super-resolution imaging optical system
CN109606617A (en) * 2018-11-28 2019-04-12 天津津航技术物理研究所 A kind of supersonic aircraft visible light window assembly

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GR03 Grant of secret patent right
DC01 Secret patent status has been lifted
DCSP Declassification of secret patent
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20120118

Termination date: 20190423