CN106080524A - A kind of airplane windscreen rain removal device - Google Patents
A kind of airplane windscreen rain removal device Download PDFInfo
- Publication number
- CN106080524A CN106080524A CN201610474098.3A CN201610474098A CN106080524A CN 106080524 A CN106080524 A CN 106080524A CN 201610474098 A CN201610474098 A CN 201610474098A CN 106080524 A CN106080524 A CN 106080524A
- Authority
- CN
- China
- Prior art keywords
- rain
- cavity
- water pump
- brushing piece
- wiper arm
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60S—SERVICING, CLEANING, REPAIRING, SUPPORTING, LIFTING, OR MANOEUVRING OF VEHICLES, NOT OTHERWISE PROVIDED FOR
- B60S1/00—Cleaning of vehicles
- B60S1/02—Cleaning windscreens, windows or optical devices
- B60S1/46—Cleaning windscreens, windows or optical devices using liquid; Windscreen washers
- B60S1/48—Liquid supply therefor
- B60S1/481—Liquid supply therefor the operation of at least part of the liquid supply being controlled by electric means
- B60S1/482—Liquid supply therefor the operation of at least part of the liquid supply being controlled by electric means combined with the operation of windscreen wipers
- B60S1/483—Liquid supply therefor the operation of at least part of the liquid supply being controlled by electric means combined with the operation of windscreen wipers using a supply pump driven by the windscreen-wiper motor
-
- 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)
- Water Supply & Treatment (AREA)
- Cleaning In General (AREA)
Abstract
The invention discloses a kind of airplane windscreen rain removal device, belong to frontal windshield except rain field.The present invention, including: except rain switch, controller, motor, water pump, drive deceleration mechanism, Wiper arm, fluid reservoir, brushing piece and induction apparatus；Controller one end is connected with except rain switch, the controller other end is connected with motor, water pump respectively, water pump one end is connected with fluid reservoir by pipeline, and drive deceleration mechanism one end is connected with water pump by pipeline, and the other end is connected with motor, Wiper arm is connected in drive deceleration mechanism, Wiper arm one end is provided with induction apparatus and connection has brushing piece, is provided with cavity passage in the middle of Wiper arm, is provided with cavity in the middle of brushing piece, cavity connects with brushing piece cavity passage, and cavity is disposed with through hole.Under the effect of brushing piece, making except rain agent is coated uniformly on windshield surface, the wiper in conjunction with brushing piece itself removes rain function, and windshield cleaning effect is excellent, it is ensured that under harsh condition of raining, pilot's gets a clear view.
Description
Technical field
The invention belongs to frontal windshield and remove rain technical field, be specifically related to a kind of airplane windscreen rain removal device.
Background technology
At precipitation weather, aircraft sliding running, take off, march into the arena, land during its front windshield must have and meet visibility requirement
Crucial field of vision.Traditional mainly have two kinds except rain method: one is to use motor to drive rain brush, by the brushing piece on rain brush
Wiper effect on windshield surface removes the rainwater on windscreen；The second is to apply waterproof coating on windshield surface,
Make it form the molecular film of layer of transparent on windscreen, reduce the bonding force between water and glass, by the height flow through along windscreen
These globules are removed by speed air-flow.But, under some intense rainfall condition, the mechanical type only relying on rain brush brushing piece removes rain, easily
One layer of water smoke is formed, it is impossible to ensure getting a clear view of pilot between brushing piece and glass；Waterproof coating is the most aging, causes glass
Glass dazzle and field of vision obscure, it is necessary to frequently change windshield, be substantially reduced the economy of aircraft.
Summary of the invention
The present invention seeks to: provide a kind of airplane windscreen except the device of rain, it is possible to quickly except rain, it is ensured that harsh
Under condition of raining, pilot's gets a clear view, it is to avoid the problem that the tradition the cleanest and rainproof coating aging of rain brush wiper brings.
The technical scheme is that a kind of airplane windscreen rain removal device, including: except rain switch, controller, electricity
Machine, water pump, drive deceleration mechanism, Wiper arm, fluid reservoir, brushing piece and induction apparatus.
Controller one end is connected with except rain switch, and the controller other end is connected with motor, water pump respectively, and water pump one end is passed through
Pipeline is connected with fluid reservoir, and drive deceleration mechanism one end is connected with water pump by pipeline, and the other end is connected with motor, and Wiper arm is even
Being connected in drive deceleration mechanism, Wiper arm one end is provided with induction apparatus and connection has brushing piece, is provided with cavity in the middle of Wiper arm
Passage, is provided with cavity in the middle of brushing piece, cavity connects with the cavity passage of Wiper arm, and cavity is disposed with through hole.
Preferably, described fluid reservoir is provided with except rain agent.
Preferably, described cavity circumference is evenly arranged with through hole.
Preferably, described drive deceleration mechanism is provided with being connected except rain agent outlet conduit except rain agent passage and water pump.
Preferably, the cavity passage except rain agent outlet conduit with Wiper arm of described water pump is joined directly together.
Technical solution of the present invention advantage is: under the effect of brushing piece, makes except rain agent is coated uniformly on windshield surface, knot
Close the wiper of brushing piece itself except rain function, windshield cleaning effect excellence, it is ensured that pilot under harsh condition of raining
Get a clear view.
Accompanying drawing explanation
Fig. 1 is the structural representation of a preferred embodiment of the present invention a kind of airplane windscreen rain removal device.
Wherein, 1-switchs except rain, 2-controller, 3-motor, 4-water pump, 5-drive deceleration mechanism, 6-Wiper arm, 7-liquid storage
Tank, 8-brushing piece, 9-induction apparatus, 10-cavity, 11-through hole；
Detailed description of the invention
Clearer for the purpose making the present invention implement, technical scheme and advantage, below in conjunction with in the embodiment of the present invention
Accompanying drawing, the technical scheme in the embodiment of the present invention is further described in more detail.In the accompanying drawings, the most identical or class
As label represent same or similar element or there is the element of same or like function.Described embodiment is the present invention
A part of embodiment rather than whole embodiments.The embodiment described below with reference to accompanying drawing is exemplary, it is intended to use
In explaining the present invention, and it is not considered as limiting the invention.Based on the embodiment in the present invention, ordinary skill people
The every other embodiment that member is obtained under not making creative work premise, broadly falls into the scope of protection of the invention.Under
Face combines accompanying drawing and is described in detail embodiments of the invention.
In describing the invention, it is to be understood that term " " center ", " longitudinally ", " laterally ", "front", "rear",
The orientation of the instruction such as "left", "right", " vertically ", " level ", " top ", " end " " interior ", " outward " or position relationship are for based on accompanying drawing institute
The orientation shown or position relationship, be for only for ease of and describe the present invention and simplify description rather than instruction or the dress of hint indication
Put or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that protect the present invention
The restriction of scope.
As it is shown in figure 1, a kind of airplane windscreen rain removal device, including: except rain switch 1, controller 2, motor 3, water pump
4, drive deceleration mechanism 5, Wiper arm 6, fluid reservoir 7, brushing piece 8 and induction apparatus 9,
Opening windscreen and remove rain switch 1, power supply will be separately input to motor 3 and water pump 4 through controller 2, and motor 3 drives and subtracts
Speed mechanism 5 makes it drive Wiper arm 6 to carry out angular motion；Meanwhile, water pump 4 will be drawn through pipeline except rain agent in fluid reservoir 7
It is transported to drive deceleration mechanism 5, is finally transported in the cavity passage of Wiper arm 6；Or water pump 4 by fluid reservoir 7 except rain
Agent extract out be delivered directly to water pump 4 by fluid reservoir 7 except rain agent extract out.
By the induction apparatus 9 being arranged between Wiper arm 6 and brushing piece 8, except rain agent enters in brushing piece 8 under a certain pressure
Cavity 10 in, from cavity 10, be uniformly distributed through hole 11 spray；Along with the angular motion of Wiper arm 6, brushing piece 8 starts wiper wind
Gear glass surface, through hole 11 is sprayed except rain agent uniform application is on windshield, and by continuous wiper remove windscreen
The rainwater on surface.
Technical solution of the present invention advantage is: under the effect of brushing piece, makes except rain agent is coated uniformly on windshield surface, knot
Close the wiper of brushing piece itself except rain function, windshield cleaning effect excellence, it is ensured that pilot under harsh condition of raining
Get a clear view.
Last it is noted that above example is only in order to illustrate technical scheme, it is not intended to limit.To the greatest extent
The present invention has been described in detail by pipe with reference to previous embodiment, it will be understood by those within the art that: it is still
Technical scheme described in foregoing embodiments can be modified, or wherein portion of techniques feature is carried out equivalent replace
Change；And these amendments or replacement, do not make the essence of appropriate technical solution depart from the essence of various embodiments of the present invention technical scheme
God and scope.
Claims (5)
1. an airplane windscreen rain removal device, it is characterised in that including: except rain switch (1), controller (2), motor (3),
Water pump (4), drive deceleration mechanism (5), Wiper arm (6), fluid reservoir (7), brushing piece (8) and induction apparatus (9)；
Controller (2) one end is connected with except rain switch (1), and controller (2) other end is connected with motor (3), water pump (4) respectively,
Water pump (4) one end is connected with fluid reservoir (7) by pipeline, and drive deceleration mechanism (5) one end is connected with water pump (4) by pipeline,
The other end is connected with motor (3), and Wiper arm (6) is connected in drive deceleration mechanism (5), and Wiper arm (6) one end is provided with injection
Device (9) and connection have brushing piece (8), and middle being provided with in the middle of cavity passage, brushing piece (8) of Wiper arm (6) is provided with cavity (10),
Cavity (10) connects with Wiper arm (6) cavity passage, and cavity (10) is disposed with through hole (11).
Airplane windscreen rain removal device the most according to claim 1, described fluid reservoir (7) is provided with except rain agent.
Airplane windscreen rain removal device the most according to claim 1, described cavity (10) circumference is evenly arranged with through hole
(11)。
Airplane windscreen rain removal device the most according to claim 1, described drive deceleration mechanism (5) is provided with except rain agent
Being connected except rain agent outlet conduit of passage and water pump (4).
Airplane windscreen rain removal device the most according to claim 4, described water pump (4) except rain agent outlet conduit and rain
The cavity passage of brush arm (6) is joined directly together.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610474098.3A CN106080524A (en) | 2016-06-24 | 2016-06-24 | A kind of airplane windscreen rain removal device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610474098.3A CN106080524A (en) | 2016-06-24 | 2016-06-24 | A kind of airplane windscreen rain removal device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106080524A true CN106080524A (en) | 2016-11-09 |
Family
ID=57252664
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610474098.3A Pending CN106080524A (en) | 2016-06-24 | 2016-06-24 | A kind of airplane windscreen rain removal device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106080524A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108058675A (en) * | 2017-11-03 | 2018-05-22 | 中航通飞研究院有限公司 | A kind of amphibious aircraft windshield washing system |
| CN111210406A (en) * | 2019-12-27 | 2020-05-29 | 中国航空工业集团公司西安飞机设计研究所 | Method for calculating position of glare source of cockpit |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6266842B1 (en) * | 1998-05-06 | 2001-07-31 | MüLLER HERMANN-FRANK | Windshield cleaning device with liquid collection |
| CN201317345Y (en) * | 2008-10-23 | 2009-09-30 | 凌云科技集团有限责任公司 | Windscreen wiper speed reducer of plane |
| CN203246437U (en) * | 2013-05-20 | 2013-10-23 | 株洲联诚集团有限责任公司 | Washing device with alarm function and for high speed train unit |
| CN203805862U (en) * | 2014-04-17 | 2014-09-03 | 昆达电脑科技(昆山)有限公司 | Defrosting device for automobile glass |
| CN103707849B (en) * | 2014-01-09 | 2015-11-04 | 任强 | Singly scrape bobbin commutation and synchronously scrub wiper |
| CN204775143U (en) * | 2015-06-11 | 2015-11-18 | 黄冰勇 | Water spray windshield wiper |
-
2016
- 2016-06-24 CN CN201610474098.3A patent/CN106080524A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6266842B1 (en) * | 1998-05-06 | 2001-07-31 | MüLLER HERMANN-FRANK | Windshield cleaning device with liquid collection |
| CN201317345Y (en) * | 2008-10-23 | 2009-09-30 | 凌云科技集团有限责任公司 | Windscreen wiper speed reducer of plane |
| CN203246437U (en) * | 2013-05-20 | 2013-10-23 | 株洲联诚集团有限责任公司 | Washing device with alarm function and for high speed train unit |
| CN103707849B (en) * | 2014-01-09 | 2015-11-04 | 任强 | Singly scrape bobbin commutation and synchronously scrub wiper |
| CN203805862U (en) * | 2014-04-17 | 2014-09-03 | 昆达电脑科技(昆山)有限公司 | Defrosting device for automobile glass |
| CN204775143U (en) * | 2015-06-11 | 2015-11-18 | 黄冰勇 | Water spray windshield wiper |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108058675A (en) * | 2017-11-03 | 2018-05-22 | 中航通飞研究院有限公司 | A kind of amphibious aircraft windshield washing system |
| CN111210406A (en) * | 2019-12-27 | 2020-05-29 | 中国航空工业集团公司西安飞机设计研究所 | Method for calculating position of glare source of cockpit |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205989726U (en) | A kind of jet-impingement wiper | |
| CN105480202A (en) | Windscreen-wiper blade, system and method for wiping a glass surface of a motor vehicle | |
| CN106080524A (en) | A kind of airplane windscreen rain removal device | |
| CN203318294U (en) | Wing mirror | |
| CN103010101A (en) | Airflow guide rearview mirror for automobile | |
| CN105835841B (en) | Intelligent vehicle washing system and car-washing method | |
| CN203511585U (en) | Windshield wiper with water spraying openings | |
| CN206749745U (en) | A kind of composite type vehicle wiper | |
| CN205652106U (en) | Multifunctional wiper | |
| CN104071130A (en) | Automotive windscreen wiper | |
| CN206749743U (en) | Windshield washer formula rain brush | |
| CN205327019U (en) | Can be before start -up wet wiper | |
| CN204623407U (en) | Energy-conservation rain brush | |
| CN204139118U (en) | A kind of Road Snow Agent flusher | |
| CN209241037U (en) | A kind of heating device cleaning vehicle glass | |
| CN106347314A (en) | Full-automatic water tank type air window washer | |
| CN106274822A (en) | Defroster device for vehicle wiper | |
| CN104908717A (en) | Cleaning device | |
| CN204452372U (en) | Automobile-used washing equipment | |
| CN207141022U (en) | A kind of automobile rain scraper plate with heating function | |
| CN204432524U (en) | A kind of passive de-watering apparatus for automobile rearview mirror | |
| CN205387124U (en) | Polishing wax -polishing machine | |
| CN204340978U (en) | A kind of rain-proof rear-viewing mirror | |
| CN205668554U (en) | Intelligence vehicle washing system | |
| CN207617683U (en) | A kind of painting device for protecting vehicle glass |
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: 20161109 |