CN205221091U - Hatch door order difference adjustment mechanism - Google Patents
Hatch door order difference adjustment mechanism Download PDFInfo
- Publication number
- CN205221091U CN205221091U CN201521011109.1U CN201521011109U CN205221091U CN 205221091 U CN205221091 U CN 205221091U CN 201521011109 U CN201521011109 U CN 201521011109U CN 205221091 U CN205221091 U CN 205221091U
- Authority
- CN
- China
- Prior art keywords
- lock ring
- hatch door
- eccentric
- sleeve
- latch hook
- 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
Abstract
The utility model provides a hatch door order difference adjustment mechanism, a serial communication port, including fix lock ring holder (1) on the hatch door, with the eccentric catch (2) of latch hook complex, install in the mounting hole of lock ring holder (1) tip eccentric catch (2) for adjustment catch and latch hook assembly error.
Description
Technical field
The invention belongs to aviation field, particularly relate to a kind of can be used for undercarriage hatch door, in bury adjustable upper lock ring on the various aerial jacks such as weapon hatch door, flap, drag parachute housing, extendible air refueling pipe.
Background technology
Modern combat aircraft proposes high requirement to Stealth Fighter, and for meeting Stealth Fighter needs, the jacks such as hatch door are on receiving during state, and hatch door surrounding will overlap with fuselage skin, and strictly will control jump.
Due to upper lock ring, above-below direction is adjustable after mounting in the present invention, thus the aerial folding structure such as hatch door can well be controlled after locking, overlap jump with fuselage skin, good effect is served to the RCS reducing the folding structures such as hatch door, thus improves the Stealth Fighter of aircraft.When being provided with jump with front door mechanism, the lock ring or by producing new parts of need polishing, controls quality of fit, existing makes adjustment jump become simple by the present invention, easy.
Summary of the invention
The present invention proposes the hatch door jump regulating mechanism that a kind of structure is simple, easy to adjust, lightweight, reliability is high, applied widely.
The invention provides a kind of hatch door jump regulating mechanism, it is characterized in that, the eccentric lock ring (2) comprise the lock ring support (1) be fixed on hatch door, coordinating with latch hook, eccentric lock ring (2) is arranged in the mounting hole of lock ring support 1 end, for adjusting lock ring and latch hook assembly error.
Further, described eccentric lock ring (2) comprises edge with the cylindrical matrix (2-1) protruding block (2-2), cylindrical matrix (2-1) is provided with off-center column (2-3), off-center column (2-3) coordinates with latch hook, lock ring support (1) end has multiple adjusting grooves (1-1), by protruding coordinating of block (2-2) and adjusting grooves (1-1) of diverse location, off-center column (2-3) location deflection, realizes the adjustment of lock ring and latch hook assembly error.
Further, described off-center column (2-3) comprises lock ring sleeve (2-4), lock ring sleeve (2-4) is enclosed within off-center column (2-3), and off-center column (2-3) is coordinated with latch hook by lock ring sleeve (2-4).
Further, described lock ring sleeve (2-4) adopts hardness lower than the material of latch hook and off-center column (2-3).Realize the protection to latch hook and lock ring, improve reliability, strengthen its interchangeability.
Further, lock ring sleeve (2-4) adopts copper material.Larger than the material hardness of latch hook and lock ring, avoid organism material impaired, realize, to its protection, improve the reliability of aircraft.
Further, also comprise eccentric sleeve (3), eccentric sleeve (3) is arranged on eccentric lock ring (2) one end, and eccentric sleeve (3) is arranged in the mounting hole of lock ring support (1) end.Eccentric sleeve (3) can make eccentric lock ring (2) longer for service life.And eccentric sleeve (3) is easy to change.
Further, eccentric sleeve (3) is provided with the chute of logical grease.
Applied range of the present invention, be applicable to undercarriage door, in bury the various aerial folding structures such as weapon hatch door, flap, drag parachute housing, the aerial collection tube of extendible, the present invention can adjust the position of folding structure uplock easily, the jump that control folding structure and fuselage overlap, greatly fall folding structure RCS, improve the Stealth Fighter of aircraft.
Volume of the present invention is little, lightweight, easy to adjust, need not polish, and general, interchangeable, reliability is high.
Accompanying drawing explanation
Fig. 1 mounting structure schematic diagram of the present invention.
The schematic diagram of Fig. 2 lock ring support.
The schematic diagram of the eccentric lock ring of Fig. 3.
Fig. 4 is the scheme of installation of lock ring sleeve and eccentric sleeve.
Fig. 5 is the schematic diagram of lock ring sleeve.
Fig. 6 is the schematic diagram of eccentric sleeve.
Detailed description of the invention
The invention provides a kind of hatch door jump regulating mechanism, the eccentric lock ring 2 comprise the lock ring support 1 be fixed on hatch door, coordinating with latch hook, eccentric lock ring 2 coordinates with eccentric sleeve 3, is arranged on lock ring support 1 end, for adjusting lock ring and latch hook assembly error.
Eccentric lock ring 2 comprises the cylindrical matrix 2-1 of edge with outstanding block 2-2, cylindrical matrix is provided with off-center column 2-3, off-center column 2-3 coordinates with latch hook, lock ring support 1 end has multiple adjusting grooves 1-1, by coordinating of the adjusting grooves 1-1 of outstanding block 2-2 and diverse location, off-center column 2-3 location deflection, realizes the adjustment of lock ring and latch hook assembly error.
Off-center column 2-3 comprises lock ring sleeve 2-4, and lock ring sleeve 2-4 is enclosed within off-center column 2-3, and off-center column 2-3 is coordinated with latch hook by lock ring sleeve 2-4.
Lock ring sleeve 2-4 adopts hardness lower than the copper product of latch hook and off-center column 2-3.
Eccentric sleeve 3 is arranged on eccentric lock ring 2 one end, and eccentric sleeve 3 is arranged in the mounting hole of lock ring support 1 end.Eccentric sleeve 3 can make eccentric lock ring 2 longer for service life.And eccentric sleeve 3 is easy to change.
Further, eccentric sleeve 3 is provided with the chute of logical grease.
Hatch door or other locked object are when uplock is installed, the relative position of the eccentric protrusion block 2-2 of the lock ring 2 and adjusting grooves 1-1 of lock ring support 1 of adjustable, the adjustment realizing lock ring height direction is changed by the degree of eccentricity of eccentric lock ring 2, the upper lock ring of adjustable hatch door can meet folding structure lock install time height direction adjustment, finally reach the folding structures such as hatch door and the requirement meeting jump and control is installed, reduce RCS, improve aircraft Stealth Fighter.
Claims (7)
1. a hatch door jump regulating mechanism, it is characterized in that, the eccentric lock ring (2) comprise the lock ring support (1) be fixed on hatch door, coordinating with latch hook, eccentric lock ring (2) is arranged in the mounting hole of lock ring support (1) end, for adjusting lock ring and latch hook assembly error.
2. hatch door jump regulating mechanism according to claim 1, it is characterized in that, described eccentric lock ring (2) comprises edge with the cylindrical matrix (2-1) protruding block (2-2), cylindrical matrix is provided with off-center column (2-3), off-center column (2-3) coordinates with latch hook, lock ring support (1) end has multiple adjusting grooves (1-1), by protruding coordinating of block (2-2) and adjusting grooves (1-1) of diverse location, off-center column (2-3) location deflection, realizes the adjustment of lock ring and latch hook assembly error.
3. hatch door jump regulating mechanism according to claim 2, it is characterized in that, described off-center column (2-3) comprises lock ring sleeve (2-4), lock ring sleeve (2-4) is enclosed within off-center column (2-3), and off-center column (2-3) is coordinated with latch hook by lock ring sleeve (2-4).
4. hatch door jump regulating mechanism according to claim 3, is characterized in that, lock ring sleeve (2-4) adopts hardness lower than the material of latch hook and off-center column (2-3).
5. hatch door jump regulating mechanism according to claim 4, it is characterized in that, lock ring sleeve (2-4) adopts copper material.
6. hatch door jump regulating mechanism according to claim 1, it is characterized in that, also comprise eccentric sleeve (3), eccentric sleeve (3) is arranged on eccentric lock ring (2) one end, and eccentric sleeve (3) is arranged in the mounting hole of lock ring support (1) end.
7. hatch door jump regulating mechanism according to claim 6, is characterized in that, eccentric sleeve (3) is provided with the chute of logical grease.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521011109.1U CN205221091U (en) | 2015-12-08 | 2015-12-08 | Hatch door order difference adjustment mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521011109.1U CN205221091U (en) | 2015-12-08 | 2015-12-08 | Hatch door order difference adjustment mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205221091U true CN205221091U (en) | 2016-05-11 |
Family
ID=55896173
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521011109.1U Active CN205221091U (en) | 2015-12-08 | 2015-12-08 | Hatch door order difference adjustment mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205221091U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107724841A (en) * | 2017-09-30 | 2018-02-23 | 中国航空工业集团公司西安飞机设计研究所 | A kind of door ladder unification landing gate sequence control mechanism |
| CN112160959A (en) * | 2020-08-28 | 2021-01-01 | 成都飞机工业（集团）有限责任公司 | Workpiece non-step assembling structure and assembling method |
| CN114212245A (en) * | 2022-01-28 | 2022-03-22 | 中国商用飞机有限责任公司 | Position-adjustable lock ring device and landing gear cabin door comprising same |
-
2015
- 2015-12-08 CN CN201521011109.1U patent/CN205221091U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107724841A (en) * | 2017-09-30 | 2018-02-23 | 中国航空工业集团公司西安飞机设计研究所 | A kind of door ladder unification landing gate sequence control mechanism |
| CN107724841B (en) * | 2017-09-30 | 2019-03-08 | 中国航空工业集团公司西安飞机设计研究所 | A kind of ladder unification landing gate sequence control mechanism |
| CN112160959A (en) * | 2020-08-28 | 2021-01-01 | 成都飞机工业（集团）有限责任公司 | Workpiece non-step assembling structure and assembling method |
| CN112160959B (en) * | 2020-08-28 | 2022-04-08 | 成都飞机工业（集团）有限责任公司 | Workpiece non-step assembling structure and assembling method |
| CN114212245A (en) * | 2022-01-28 | 2022-03-22 | 中国商用飞机有限责任公司 | Position-adjustable lock ring device and landing gear cabin door comprising same |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205221091U (en) | Hatch door order difference adjustment mechanism | |
| CN104089547B (en) | A kind of Deployment and locking device of folding rudder face | |
| CN104648680A (en) | Fuel tank layout of flying wing configuration type airplane | |
| CN203949574U (en) | A kind of Deployment and locking device of folding rudder face | |
| CN104590592A (en) | Novel spatial electromagnetic docking mechanism | |
| CN103869821B (en) | Onboard automatic pesticide balancing system of agricultural unmanned aerial vehicle | |
| CN105000193A (en) | Follow-up radome bracket and follow-up radar with same as well as aircraft | |
| CN107878764B (en) | Integral sliding structure of hot wall exhaust pipe of fairing | |
| CN207660944U (en) | A kind of LED display arc lock construction | |
| CN104964139A (en) | High-stability rapid-connection tripod platform device | |
| CN105270603A (en) | Unmanned fixed-wing aircraft with large aspect ratio | |
| CN105438442A (en) | Aircraft with variable aerodynamic layout | |
| CN205273837U (en) | Variable aerodynamic layout's aircraft | |
| CN205311889U (en) | Upper catch of hatch door with adjustable | |
| CN104386243A (en) | Failure neutral-position return mechanism for steering engine of airplane | |
| CN208021743U (en) | A kind of food delivery unmanned plane | |
| CN205406707U (en) | Aircraft antenna setting support and quick -witted connection structure who carries on back | |
| CN204250346U (en) | A kind of anti-rollover airframe steel framework structure | |
| CN205499322U (en) | Integral cabin door lock locks seat | |
| CN211033026U (en) | Sliding block type mechanical interface | |
| CN215361885U (en) | Multispectral camera support of unmanned aerial vehicle mount | |
| CN206552275U (en) | A kind of multistage drawing and pulling type aviation dining table | |
| CN205221129U (en) | Helicopter is used and is not surveyd optoelectronic system to ground | |
| CN103523203A (en) | Front camera cabin of unmanned aerial vehicle | |
| CN104743126A (en) | Aircraft oil tank casting device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210324 Address after: 611731, No. four, West core road, hi tech West District, Sichuan, Chengdu Patentee after: AVIC (Chengdu) UAV System Co.,Ltd. Address before: 610091 planning and Development Department of Chengdu aircraft design and Research Institute, 1610 Riyue Avenue, Qingyang District, Chengdu City, Sichuan Province Patentee before: AVIC CHENGDU AIRCRAFT DESIGN & Research Institute |