CN106184702A - Waterproof quick-release combination lid - Google Patents
Waterproof quick-release combination lid Download PDFInfo
- Publication number
- CN106184702A CN106184702A CN201610843726.0A CN201610843726A CN106184702A CN 106184702 A CN106184702 A CN 106184702A CN 201610843726 A CN201610843726 A CN 201610843726A CN 106184702 A CN106184702 A CN 106184702A
- Authority
- CN
- China
- Prior art keywords
- lid
- small cap
- release
- waterproof quick
- big
- 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.)
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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
- B64C1/1407—Doors; surrounding frames
- B64C1/1446—Inspection hatches
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Casings For Electric Apparatus (AREA)
Abstract
Waterproof quick-release combination lid, including lid assembly, rotating shaft, support, waterproof quick-release button latch and sealing plate nut；Wherein, lid assembly includes big lid and small cap, and a part that small cap is big lid collectively form Aerodynamic Configuration of Aireraft with big lid；Being provided with rotating shaft in big lid, support one end is connected with rotating shaft simultaneously, and the other end connects small cap, and small cap is additionally provided with the installing hole for installing waterproof quick-release button latch；Additionally, big lid both sides are separately provided for the sealing plate nut being connected with housing construction.The present invention uses the version of combination lid to realize safeguarding equipment difference the suitability of type, waterproof quick-detachable lock is used to realize the quick-release of small cap, it is easy to the simple-to-maintain operation of equipment or conventional visual inspection, uses sealing plate nut and sealing gasket can realize combining the water-proof function of lid.
Description
Technical field
The present invention relates to aircaft configuration technical field, particularly relate to a kind of waterproof quick-release combination lid.
Background technology
Lid is widely used in aircraft circles, for the use of aircraft, safeguard in need to check, repair, adjust, fill out
The equipment that fills, decompose or change, adnexa, housing construction is provided with lid；Airplane design handbook divides for lid simultaneously
Class is generally classified, such as by the unlatching form of lid: the quick-release lid opened without instrument, needs the quick-release mouth that instrument is opened
Lid and need a few class lids such as stress lid of TO；But, along with equipment, the adnexa of aircraft are the most diversified, it makes
With maintenance requirement variation the most day by day, some equipment is dismantled number of times during using and is required less, but needs letter frequently
One-dimensional protects or conventional visual inspection, and has rainwater-proof requirement concurrently；Now, lid design is carried out according to the common lid of above classification
Then it is difficult to meet several respects working service requirement of equipment simultaneously.
Summary of the invention
Technical problem solved by the invention is to provide a kind of waterproof quick-release to combine lid, to solve above-mentioned background technology
Described in shortcoming.
Technical problem solved by the invention realizes by the following technical solutions:
Waterproof quick-release combination lid, including lid assembly, rotating shaft, support, waterproof quick-release button latch and sealing plate nut；Its
In, lid assembly includes big lid and small cap, and a part that small cap is big lid collectively forming with big lid flies
Machine aerodynamic configuration, big lid can provide bigger maintenance after opening, it is adaptable to plant maintenance or equipment that operation is complicated dismount
Use；Being provided with rotating shaft in big lid, support one end is connected with rotating shaft simultaneously, and the other end connects small cap, on small cap also
Being provided with the installing hole for installing waterproof quick-release button latch, to realize small cap open and close, but open area is less, uses
In the path that routine examination or simple-to-maintain operate；Additionally, what big lid both sides were separately provided for being connected with housing construction
Seal plate nut, to ensure the water-proof function of quick-release combination lid.
In the present invention, in big lid and small cap, it is separately installed with sealing gasket, for ensureing to combine the water proofing property of lid
Energy.
In the present invention, support is V-shape structure, with meet small cap open after can rotate around the axis and not with big lid
Interfere.
Beneficial effect: the present invention use combination lid version realize equipment difference working service is required be suitable for
Property, use waterproof quick-detachable lock to realize the quick-release of small cap, it is simple to the simple-to-maintain operation of equipment or conventional visual inspection, use close
Envelope plate nut and sealing gasket can realize combining the water-proof function of lid.
Accompanying drawing explanation
Fig. 1 is the structural representation of presently preferred embodiments of the present invention.
Fig. 2 is the supporting structure schematic diagram in presently preferred embodiments of the present invention.
Fig. 3 is the lid working state schematic representation in presently preferred embodiments of the present invention.
Fig. 4 is the sealing plate nut structural representation in presently preferred embodiments of the present invention.
Detailed description of the invention
For the technological means making the present invention realize, creation characteristic, reach purpose and be easy to understand with effect, below knot
Conjunction is specifically illustrating, and the present invention is expanded on further.
See Fig. 1 ~ Fig. 4 waterproof quick-release combination lid, including lid 1, lid 2, rotating shaft 3, support 4, waterproof quick-release by
Button lock 5, seal plate nut 6, sealing gasket A7, sealing gasket B8, the opening 9 of lid B, the closed mode 10 of lid B and interior
Portion's equipment 11；Wherein, lid 1 is big lid, and it can provide bigger maintenance after opening, it is adaptable to the equipment dimension that operation is complicated
Protect or equipment dismounting use, lid 2 is small cap, its be lid 1 a part and with lid 1 collectively form aircraft pneumatic outside
Shape；Being provided with rotating shaft 3 in lid 1, support 4 one end is connected with rotating shaft 3 simultaneously, and the other end connects lid 2, and lid 2 also sets
It is equipped with the installing hole for installing waterproof quick-release button latch 5, in order to realize lid 2 and open and close, but open area is less, uses
In the path that routine examination or simple-to-maintain operate；Lid 1 is connected by sealing plate nut 6 with housing construction, fast to ensure
Unload the water-proof function of combination lid；Additionally, be provided with sealing gasket A7 in lid 1, sealing gasket B8, sealing gasket are installed in lid 2
For ensureing to combine the water resistance of lid.
In the present embodiment, seal plate nut 6 and include nut body 12 and seal closure 13, and seal closure 13 is placed in nut body
12 is outside, and nut body 12 includes supporting plate, the section of closing in and is arranged at the screw thread within nut body, and supporting plate bottom is provided with sealing gasket, receives
Mouth section outer cover is equipped with sealing ring.
In the present embodiment, support 4 is V-shape structure, with meet lid 2 open after can around the shaft 3 rotate and not with mouth
Lid 1 interferes, under the work of support 4, and the opening and closing state of lid 2, as it is shown on figure 3, the unlatching shape of wherein lid B
State 9, the closed mode 10 of lid B and the application example that internal unit 11 is the present embodiment, this internal unit 11 be without
Often dismantling but need to frequently check the equipment of (as each sortie requires to check), now, the combination lid that the present embodiment provides can be fitted
Close requirement.
The ultimate principle of the present invention and principal character and advantages of the present invention have more than been shown and described.The technology of the industry
Personnel, it should be appreciated that the present invention is not restricted to the described embodiments, simply illustrating this described in above-described embodiment and description
The principle of invention, without departing from the spirit and scope of the present invention, the present invention also has various changes and modifications, and these become
Change and improvement both falls within scope of the claimed invention.Claimed scope by appending claims and
Equivalent defines.
Claims (3)
- The most waterproof quick-release combination lid, including lid assembly, rotating shaft, support, waterproof quick-release button latch and sealing plate nut； It is characterized in that, lid assembly includes big lid and small cap, and a part that small cap is big lid with big lid altogether With constituting Aerodynamic Configuration of Aireraft；Being provided with rotating shaft in big lid, support one end is connected with rotating shaft simultaneously, and the other end connects osculum Lid, small cap is additionally provided with the installing hole for installing waterproof quick-release button latch；Additionally, big lid both sides are respectively provided with useful In the sealing plate nut being connected with housing construction.
- Waterproof quick-release the most according to claim 1 combination lid, it is characterised in that big lid is respectively mounted in small cap There is sealing gasket.
- Waterproof quick-release the most according to claim 1 combination lid, it is characterised in that support is V-shape structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610843726.0A CN106184702A (en) | 2016-09-23 | 2016-09-23 | Waterproof quick-release combination lid |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610843726.0A CN106184702A (en) | 2016-09-23 | 2016-09-23 | Waterproof quick-release combination lid |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106184702A true CN106184702A (en) | 2016-12-07 |
Family
ID=58067147
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610843726.0A Pending CN106184702A (en) | 2016-09-23 | 2016-09-23 | Waterproof quick-release combination lid |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106184702A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628196A (en) * | 2017-02-14 | 2017-05-10 | 成都飞机工业（集团）有限责任公司 | Drag parachute housing with combined rear cover for aircraft |
| CN109263852A (en) * | 2018-08-31 | 2019-01-25 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of fixed device of airplane hatch cover |
| CN109606615A (en) * | 2018-11-07 | 2019-04-12 | 中国航空工业集团公司西安飞机设计研究所 | A kind of compound lid of aircraft |
| RU207718U1 (en) * | 2021-08-06 | 2021-11-12 | Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | Luke |
| RU2764320C1 (en) * | 2021-08-06 | 2022-01-17 | Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | Method for securing the lid on the coaming of a hatch |
| RU2770416C1 (en) * | 2021-08-06 | 2022-04-18 | Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | Aircraft hatch |
Citations (8)
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|---|---|---|---|---|
| CN2389219Y (en) * | 1999-09-30 | 2000-07-26 | 中国航空工业总公司第六一一研究所 | Water-proof push-botton lock |
| CN201232451Y (en) * | 2008-07-23 | 2009-05-06 | 成都飞机设计研究所 | Multifunction hinge |
| CN101665152A (en) * | 2009-09-29 | 2010-03-10 | 江西洪都航空工业集团有限责任公司 | Quick detachable combined cover cap capable of bearing stress |
| CN202642092U (en) * | 2012-07-02 | 2013-01-02 | 江西洪都航空工业集团有限责任公司 | Improved rainproof quick-release port cover |
| CN102991667A (en) * | 2011-09-14 | 2013-03-27 | 西安飞机工业（集团）有限责任公司 | Spring swing arm assembly and application method thereof |
| CN203430239U (en) * | 2013-04-12 | 2014-02-12 | 哈尔滨飞机工业集团有限责任公司 | Opening and closing device, with positioning pin, of airplane maintenance cover |
| CN204775985U (en) * | 2015-06-19 | 2015-11-18 | 中国航空工业集团公司西安飞机设计研究所 | Aircraft flap hinge structure |
| CN206125396U (en) * | 2016-09-23 | 2017-04-26 | 江西洪都航空工业集团有限责任公司 | Waterproof quick -release combination flap |
-
2016
- 2016-09-23 CN CN201610843726.0A patent/CN106184702A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2389219Y (en) * | 1999-09-30 | 2000-07-26 | 中国航空工业总公司第六一一研究所 | Water-proof push-botton lock |
| CN201232451Y (en) * | 2008-07-23 | 2009-05-06 | 成都飞机设计研究所 | Multifunction hinge |
| CN101665152A (en) * | 2009-09-29 | 2010-03-10 | 江西洪都航空工业集团有限责任公司 | Quick detachable combined cover cap capable of bearing stress |
| CN102991667A (en) * | 2011-09-14 | 2013-03-27 | 西安飞机工业（集团）有限责任公司 | Spring swing arm assembly and application method thereof |
| CN202642092U (en) * | 2012-07-02 | 2013-01-02 | 江西洪都航空工业集团有限责任公司 | Improved rainproof quick-release port cover |
| CN203430239U (en) * | 2013-04-12 | 2014-02-12 | 哈尔滨飞机工业集团有限责任公司 | Opening and closing device, with positioning pin, of airplane maintenance cover |
| CN204775985U (en) * | 2015-06-19 | 2015-11-18 | 中国航空工业集团公司西安飞机设计研究所 | Aircraft flap hinge structure |
| CN206125396U (en) * | 2016-09-23 | 2017-04-26 | 江西洪都航空工业集团有限责任公司 | Waterproof quick -release combination flap |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628196A (en) * | 2017-02-14 | 2017-05-10 | 成都飞机工业（集团）有限责任公司 | Drag parachute housing with combined rear cover for aircraft |
| CN106628196B (en) * | 2017-02-14 | 2023-05-09 | 成都飞机工业（集团）有限责任公司 | Aircraft drag parachute cabin with combined rear cover |
| CN109263852A (en) * | 2018-08-31 | 2019-01-25 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of fixed device of airplane hatch cover |
| CN109263852B (en) * | 2018-08-31 | 2022-02-22 | 中国航空工业集团公司沈阳飞机设计研究所 | Aircraft flap fixing device |
| CN109606615A (en) * | 2018-11-07 | 2019-04-12 | 中国航空工业集团公司西安飞机设计研究所 | A kind of compound lid of aircraft |
| RU207718U1 (en) * | 2021-08-06 | 2021-11-12 | Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | Luke |
| RU2764320C1 (en) * | 2021-08-06 | 2022-01-17 | Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | Method for securing the lid on the coaming of a hatch |
| RU2770416C1 (en) * | 2021-08-06 | 2022-04-18 | Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | Aircraft hatch |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161207 |