CN110356538A - A kind of linkage adjustment mechanism for canopy latch mechanism and leak-tight system - Google Patents
A kind of linkage adjustment mechanism for canopy latch mechanism and leak-tight system Download PDFInfo
- Publication number
- CN110356538A CN110356538A CN201811205700.9A CN201811205700A CN110356538A CN 110356538 A CN110356538 A CN 110356538A CN 201811205700 A CN201811205700 A CN 201811205700A CN 110356538 A CN110356538 A CN 110356538A
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- China
- Prior art keywords
- tight
- air
- jacking block
- backing plate
- switch
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- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
- B64C1/1476—Canopies; Windscreens or similar transparent elements
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Switch Cases, Indication, And Locking (AREA)
- Lock And Its Accessories (AREA)
Abstract
A kind of linkage adjustment mechanism for canopy latch mechanism and leak-tight system, including bracket, jacking block, pull rod, air-tight switch and backing plate, wherein bracket is mounted on airframe structure, jacking block is sleeved on the pull rod of lock system and can slide along pull rod, and air-tight switch is fixed on bracket by backing plate;It is provided on backing plate multiple for adjusting the mounting hole of air-tight switch vertical direction relative position;The tooth form backing plate of air-tight switch vertical direction relative position is adjusted by setting and adjusts the jacking block of relative position between air-tight switch and canopy latch mechanism, enable freely to adjust in vector and vertical direction, lateral go up, it is effectively improved assembly process process, reduces assembly positioning difficulty.
Description
Technical field
The present invention relates to Flight Vehicle Structure technical fields more particularly to a kind of for canopy latch mechanism and leak-tight system
Linkage adjustment mechanism.
Background technique
Canopy steerable system and lock system, leak-tight system are typically designed as process control, i.e. once-through operation can be completed
Release it is airtight, unlock, open canopy or close lid, locking and the preset programs such as airtight, therefore aircraft lock system and leak-tight system
It is linked by jacking block on lock pull rod and leak-tight system air-tight switch, when locking, locks jacking block on pull rod for air-tight switch mandril
It pushes, it is airtight after locking in place to realize;When unlocking, the jacking block locked on pull rod is detached from air-tight switch mandril, airtight system first
System is deflated, and lock pull rod is being continued to press on, to realize that lock system is unlocked;To guarantee the reliability and assembly relation correctness that link,
It needs to assemble the regulating device with positioning between the two, current regulating device cannot be in vector and vertical direction
Difficulty is big when freely adjusting air-tight switch installation site, and assembling positioning.
Summary of the invention
Technical problem solved by the invention is to provide a kind of linkage tune for canopy latch mechanism and leak-tight system
Mechanism is saved, to solve the disadvantage in above-mentioned background technique.
Technical problem solved by the invention is realized using following technical scheme:
A kind of linkage adjustment mechanism for canopy latch mechanism and leak-tight system, including bracket, jacking block, pull rod, air-tight switch
And backing plate, wherein bracket is mounted on airframe structure, and jacking block is sleeved on the pull rod of lock system and can slide along pull rod, airtight
Switch is fixed on bracket by backing plate;Multiple mounting holes are provided on backing plate, it is opposite for adjusting air-tight switch vertical direction
Position.
In the present invention, the connection bolt for adjusting air-tight switch relative position is provided on bracket.
In the present invention, it is separately provided for adjusting the connection spiral shell of air-tight switch relative position on air-tight switch and backing plate
Bolt.
In the present invention, backing plate is tooth form backing plate.
In the present invention, the toothed surface with backing plate mutual cooperation adjusting position is provided on air-tight switch.
In the present invention, fastening screw nut is respectively arranged on the pull rod for being located at jacking block both ends.
In the present invention, the gasket for adjusting jacking block and air-tight switch upper ejector pin deviation to the right is provided on backing plate.
In the present invention, the gasket for adjusting jacking block and air-tight switch upper ejector pin deviation to the right is provided on bracket.
In the present invention, after the locking in place of canopy latch mechanism, jacking block is moved along pull rod, by the mandril pressure of air-tight switch
Under, leak-tight system is connected, to enable the relative position of air-tight switch and jacking block to guarantee that the two is normal in locking and unlocking
Dynamic, the mandril volume under pressure and mandril of air-tight switch should all match in the position of jacking block contact plane with interaction relation;Work as gas
When close switch mandril volume under pressure exceeds normal range value, unscrew the connection bolt of connection air-tight switch, tooth form backing plate and bracket, it will
Until air-tight switch up and down adjustment to satisfaction;When there are deviation in air-tight switch and jacking block course relative position, unscrew and press closer block
On two fastening screw nuts, jacking block is free to slide on pull rod at this time, so as to adjust the rigging position of jacking block;When jacking block with it is airtight
Mandril on switch to the right deviation when, pass through and increase gasket on tooth form backing plate and bracket and adjust.
The utility model has the advantages that the present invention adjusts the tooth form backing plate of air-tight switch vertical direction relative position by setting and adjusts gas
The jacking block of relative position between close switch and canopy latch mechanism, enable vector and vertical direction, it is lateral it is upper from
By adjusting, it is effectively improved assembly process process, reduces assembly positioning difficulty.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of presently preferred embodiments of the present invention.
Fig. 2 is jacking block in the presently preferred embodiments of the present invention scheme of installation on pull rod.
Specific embodiment
In order to be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, tie below
Conjunction is specifically illustrating, and the present invention is further explained.
Referring to a kind of linkage adjustment mechanism for canopy latch mechanism and leak-tight system of FIG. 1 to FIG. 2, including bracket 1,
Jacking block 2, fastening screw nut 3, pull rod 4, air-tight switch 5 and tooth form backing plate 6, wherein bracket 1 is mounted on airframe structure, lock system
Pull rod 4 penetrate through jacking block 2 and stretch out jacking block 2, and be provided with fastening screw nut 3 on the pull rod 4 for being located at 2 both ends of jacking block, it is airtight to open
5 are closed to be fixed on bracket 1 by tooth form backing plate 6;It is provided with multiple mounting holes on tooth form backing plate 6, hangs down for adjusting air-tight switch 5
Histogram is to relative position;
The connection bolt for adjusting 5 relative position of air-tight switch is provided on bracket 1;
After the locking in place of canopy latch mechanism, jacking block 2 is moved along pull rod 4, and the mandril of air-tight switch 5 is depressed, and leak-tight system connects
It is logical, to enable the relative position of air-tight switch 5 and jacking block 2 to guarantee normal linkage of the two in locking and unlocking, air-tight switch 5
Mandril volume under pressure and mandril should all match with interaction relation in the position of 2 contact plane of jacking block;
Regulating mechanism working principle is as follows: when 5 mandril volume under pressure of air-tight switch exceeds normal range value, unscrewing and connects airtight open
Close 5, the connection bolt of tooth form backing plate 6 and bracket 1, until 5 up and down adjustment to satisfaction of air-tight switch, tooth form backing plate 6 with it is airtight
It is provided with toothed surface on switch 5, for the adjusting position that cooperates;When air-tight switch 5 and 2 course relative position of jacking block have partially
When poor, unscrew and press closer two fastening screw nuts 3 of block 2, jacking block 2 is free to slide on pull rod 4 at this time, so as to adjust jacking block 2
Rigging position;When the mandril deviation to the right on jacking block 2 and air-tight switch 5, padded by increasing on tooth form backing plate 6 and bracket 1
Piece is adjusted.
The above shows and describes the basic principles and main features of the present invention and the advantages of the present invention.The technology of the industry
Personnel are it should be appreciated that the present invention is not limited to the above embodiments, and the above embodiments and description only describe this
The principle of invention, without departing from the spirit and scope of the present invention, various changes and improvements may be made to the invention, these changes
Change and improvement all fall within the protetion scope of the claimed invention.The claimed scope of the invention by appended claims and its
Equivalent thereof.
Claims (9)
1. a kind of linkage adjustment mechanism for canopy latch mechanism and leak-tight system, including bracket, jacking block, pull rod, airtight open
Pass and backing plate, which is characterized in that bracket is mounted on airframe structure, and jacking block is sleeved on the pull rod of lock system and can be sliding along pull rod
Dynamic, air-tight switch is fixed on bracket by backing plate;It is provided on backing plate multiple opposite for adjusting air-tight switch vertical direction
The mounting hole of position.
2. a kind of linkage adjustment mechanism for canopy latch mechanism and leak-tight system according to claim 1, feature
It is, the connection bolt for adjusting air-tight switch relative position is provided on bracket.
3. a kind of linkage adjustment mechanism for canopy latch mechanism and leak-tight system according to claim 1, feature
It is, the connection bolt of adjustment air-tight switch relative position is separately provided on air-tight switch and backing plate.
4. a kind of linkage adjustment mechanism for canopy latch mechanism and leak-tight system according to claim 1, feature
It is, backing plate is tooth form backing plate.
5. a kind of linkage adjustment mechanism for canopy latch mechanism and leak-tight system according to claim 1, feature
It is, the toothed surface with backing plate mutual cooperation adjusting position is provided on air-tight switch.
6. a kind of linkage adjustment mechanism for canopy latch mechanism and leak-tight system according to claim 1, feature
It is, is respectively arranged with fastening screw nut on the pull rod for being located at jacking block both ends.
7. a kind of linkage adjustment mechanism for canopy latch mechanism and leak-tight system according to claim 1, feature
It is, the gasket for adjusting jacking block and air-tight switch upper ejector pin deviation to the right is provided on backing plate.
8. a kind of linkage adjustment mechanism for canopy latch mechanism and leak-tight system according to claim 1, feature
It is, the gasket for adjusting jacking block and air-tight switch upper ejector pin deviation to the right is provided on bracket.
9. a kind of described in any item linkages for canopy latch mechanism and leak-tight system adjust machine according to claim 1~8
Structure, which is characterized in that after the locking in place of canopy latch mechanism, jacking block is moved along pull rod, and the mandril of air-tight switch is depressed, airtight
System is connected, airtight to enable the relative position of air-tight switch and jacking block to guarantee normal linkage of the two in locking and unlocking
The mandril volume under pressure and mandril of switch should all match in the position of jacking block contact plane with interaction relation;When air-tight switch top
When bar volume under pressure exceeds normal range value, unscrew the connection bolt of connection air-tight switch, tooth form backing plate and bracket, by air-tight switch
Until up and down adjustment to satisfaction;When there are deviation in air-tight switch and jacking block course relative position, unscrew and press closer two on block
Fastening screw nut, jacking block is free to slide on pull rod at this time, so as to adjust the rigging position of jacking block;When on jacking block and air-tight switch
Mandril to the right deviation when, pass through and increase gasket on tooth form backing plate and bracket and adjust.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201811205700.9A CN110356538B (en) | 2018-10-17 | 2018-10-17 | Linkage adjusting mechanism for canopy lock mechanism and airtight system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201811205700.9A CN110356538B (en) | 2018-10-17 | 2018-10-17 | Linkage adjusting mechanism for canopy lock mechanism and airtight system |
Publications (2)
Publication Number | Publication Date |
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CN110356538A true CN110356538A (en) | 2019-10-22 |
CN110356538B CN110356538B (en) | 2022-10-11 |
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CN201811205700.9A Active CN110356538B (en) | 2018-10-17 | 2018-10-17 | Linkage adjusting mechanism for canopy lock mechanism and airtight system |
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Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3180302A (en) * | 1961-07-13 | 1965-04-27 | Pneumo Dynamics Corp | Hatch cover system |
SU393154A1 (en) * | 1971-09-16 | 1973-08-10 | LOCKING DEVICE FOR A TIGHTNESS COVER | |
US4176812A (en) * | 1977-10-31 | 1979-12-04 | The Boeing Company | Midcabin door for blended wing aircraft |
GB2047330A (en) * | 1979-04-10 | 1980-11-26 | Messerschmitt Boelkow Blohm | Closable flap arrangement for an aircraft or a spacecraft |
US5577781A (en) * | 1994-01-24 | 1996-11-26 | Daimler-Benz Aerospace Airbus Gmbh | Apparatus for locking an aircraft door |
US20080035514A1 (en) * | 2006-08-10 | 2008-02-14 | Gudeng Precision Industrial Co., Ltd. | Metal photomask box |
CN102062229A (en) * | 2009-11-17 | 2011-05-18 | 上海屹尧仪器科技发展有限公司 | Hermetic switch and application thereof |
CN102561851A (en) * | 2011-12-14 | 2012-07-11 | 江西洪都航空工业集团有限责任公司 | Aircraft cabin latch type lock |
CN203996909U (en) * | 2014-06-17 | 2014-12-10 | 江西洪都航空工业集团有限责任公司 | A kind of aircraft cockpit lock anti-mistaking locking device |
CN204587299U (en) * | 2015-04-17 | 2015-08-26 | 陕西飞机工业(集团)有限公司 | A kind of airtight quick-detachable lock device |
CN206017720U (en) * | 2016-08-25 | 2017-03-15 | 施拉姆电磁传感技术(扬州)有限公司 | A kind of screw-in air-tight switch Magnet |
CN207960427U (en) * | 2018-02-28 | 2018-10-12 | 中山三和五金声控有限公司 | A bottomless frame hermetic door |
-
2018
- 2018-10-17 CN CN201811205700.9A patent/CN110356538B/en active Active
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3180302A (en) * | 1961-07-13 | 1965-04-27 | Pneumo Dynamics Corp | Hatch cover system |
SU393154A1 (en) * | 1971-09-16 | 1973-08-10 | LOCKING DEVICE FOR A TIGHTNESS COVER | |
US4176812A (en) * | 1977-10-31 | 1979-12-04 | The Boeing Company | Midcabin door for blended wing aircraft |
GB2047330A (en) * | 1979-04-10 | 1980-11-26 | Messerschmitt Boelkow Blohm | Closable flap arrangement for an aircraft or a spacecraft |
US5577781A (en) * | 1994-01-24 | 1996-11-26 | Daimler-Benz Aerospace Airbus Gmbh | Apparatus for locking an aircraft door |
US20080035514A1 (en) * | 2006-08-10 | 2008-02-14 | Gudeng Precision Industrial Co., Ltd. | Metal photomask box |
CN102062229A (en) * | 2009-11-17 | 2011-05-18 | 上海屹尧仪器科技发展有限公司 | Hermetic switch and application thereof |
CN102561851A (en) * | 2011-12-14 | 2012-07-11 | 江西洪都航空工业集团有限责任公司 | Aircraft cabin latch type lock |
CN203996909U (en) * | 2014-06-17 | 2014-12-10 | 江西洪都航空工业集团有限责任公司 | A kind of aircraft cockpit lock anti-mistaking locking device |
CN204587299U (en) * | 2015-04-17 | 2015-08-26 | 陕西飞机工业(集团)有限公司 | A kind of airtight quick-detachable lock device |
CN206017720U (en) * | 2016-08-25 | 2017-03-15 | 施拉姆电磁传感技术(扬州)有限公司 | A kind of screw-in air-tight switch Magnet |
CN207960427U (en) * | 2018-02-28 | 2018-10-12 | 中山三和五金声控有限公司 | A bottomless frame hermetic door |
Non-Patent Citations (3)
Title |
---|
张玎等: "某型飞机座舱盖系统气密压力低故障分析", 《装备制造技术》 * |
徐锦锦等: "飞机起落架舱门收放联动机构气密性分析", 《机械设计与制造》 * |
李玲等: "某型飞机环境控制系统常见故障分析及维护策略", 《新技术新工艺》 * |
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