CN109969423A - A kind of aircraft bad weather oiling protective device - Google Patents
A kind of aircraft bad weather oiling protective device Download PDFInfo
- Publication number
- CN109969423A CN109969423A CN201711449054.6A CN201711449054A CN109969423A CN 109969423 A CN109969423 A CN 109969423A CN 201711449054 A CN201711449054 A CN 201711449054A CN 109969423 A CN109969423 A CN 109969423A
- Authority
- CN
- China
- Prior art keywords
- mouth
- perspex
- cover
- protective device
- lateral surface
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/28—Liquid-handling installations specially adapted for fuelling stationary aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Professional, Industrial, Or Sporting Protective Garments (AREA)
Abstract
The present invention relates to a kind of aircraft bad weather oiling protective devices, including cover (1), the cover (1) forms by the upper encloser (11) in sleeve-shaped and in round table-like lower encioser (12) is extended out, Rubber washer (4) are provided at the top of upper encloser (11), the center of Rubber washer (4) offers the oil gun mouth (41) penetrated for refueling nozzle, the bottom of lower encioser (12) is provided with circular magnetic chuck (2), is covered with anti-abrasion pad (3) on one side on the lateral surface of lower encioser (12)；It is characterized in that, another side on the lateral surface of lower encioser (12) is provided with Perspex mouth (8), several air vents (9) are evenly arranged on Perspex mouth (8), the cover (6) for rolling is additionally provided on the outside of Perspex mouth (8), and the lower edge of cover (6) and the lower edge of Perspex mouth (8) are in 15 ~ 45 ° of angle；Structure is simple, coefficient easy to use, safe is high, dust-proof anti-wear, and cost is relatively low.
Description
Technical field
The present invention relates to a kind of protective device more particularly to a kind of aircraft bad weather oiling protective devices.
Background technique
The oiling of all purpose aircraft at present is all open gravity oiling, and the environment relative requirement of oiling is higher, is not had
Dust-proof, rainwater-proof the measure of effect generally will use umbrella and rag and simply block or weather be waited to take a turn for the better again and refuel, no
It only wastes time, and influences follow-up work；Thus dust storm, rain, the severe weather conditions such as fugitive dust, haze all can not be timely
Add aircraft fuel.It is easy to cause pollutant to enter fuel system if adding fuel oil in the environment of this rather harsh, sternly
Ghost image rings the flight safety of aircraft；Refueling nozzle is larger heavier when refueling simultaneously, is easy to cause to rub to refueling nozzle and airplane component
It wipes and collides with, airframe is caused to damage.
Summary of the invention
The technical problem to be solved by the present invention is in order to overcome the deficiencies in the prior art and defect, the present invention is mentioned
Supply that a kind of structure is simple, coefficient easy to use, safe is high, dust-proof anti-wear, and lower-cost aircraft bad weather refuels
Protective device.
The technical solution adopted by the present invention to solve the technical problems is: a kind of aircraft bad weather oiling protective device,
Including cover, cover is formed by the upper encloser in sleeve-shaped and in round table-like lower encioser is extended out, and is arranged at the top of upper encloser
There is Rubber washer, the center of Rubber washer offers the oil gun mouth penetrated for refueling nozzle, the bottom of lower encioser is provided with circular magnetic chuck,
It is covered with anti-abrasion pad on one side on the lateral surface of lower encioser；It is characterized in that, the another side on the lateral surface of lower encioser is set
It is equipped with Perspex mouth, several air vents are evenly arranged on Perspex mouth, in Perspex mouth
The cover that outside is additionally provided with for rolling, and the lower edge of the lower edge of cover and Perspex mouth is in 15 ~ 45 ° of folder
Angle.
Further, the top edge of Perspex mouth is additionally provided with several LED cold light driven by button cell
Lamp.
Further, the lateral surface of lower encioser is provided with ground line, and ground line connects with the static discharger on aircraft wing
It connects.
Further, the lateral surface of lower encioser is additionally provided with storage space, and storage space memory is placed with rubber gloves.
Further, cover is all put down pave after, between the lower edge of cover and the lower edge of Perspex mouth
There are the gaps of triangle.
Further, the lower surface of circular magnetic chuck is evenly arranged with several suction pawls.
Further, anti-abrasion pad can be removed manually, and when refueling, pad is in the contact site of refueling nozzle and oil gun mouth.
Further, Perspex mouth be set on the lateral surface of lower encioser and be located at anti-abrasion pad and storage space it
Between.
Further, Perspex mouth is symmetrically arranged with 2 on the lateral surface of lower encioser.
The beneficial effects of the present invention are:
(1) aircraft fuel can be added in time under the severe weather conditions such as dust storm, rainy, fugitive dust, haze, guarantee that aircraft flies
Row safety, avoids unexpected situation；
(2) by the setting of anti-abrasion pad, refueling nozzle is larger heavier when avoiding refueling, to cause to refueling nozzle and airplane component
Friction and collide with, cause airframe to damage, and anti-abrasion pad is set together with protective device, easily take and easily take, be not easy to forget；
(3) setting for passing through Perspex mouth, cover and air vent, realizes while observing internal state in time
Internal gas discharge, cover still can not influence internal gas discharge and external with dustproof and rainproof water, and after cover is all put down
Observing effect；The top edge of Perspex mouth is additionally provided with several LED cold light lamps driven by button cell, night
It is able to achieve timely oiling.
(4) storage space memory is placed with rubber gloves, opens fuel tank flap and uses when closing fuel tank flap, protects hand
Prevent external dust.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of aircraft bad weather oiling protective device of the present invention；
In figure, 1--- cover, 11--- upper encloser, 12--- lower encioser, 2--- sucker, 3--- anti-abrasion pad, 4--- Rubber washer,
41--- oil gun mouth, 5---LED cold light lamp, 6--- cover, 7--- ground line, 8--- Perspex mouth, 9--- air vent,
10--- storage space.
Specific embodiment
In conjunction with the accompanying drawings, the present invention is further explained in detail.These attached drawings are simplified schematic diagram, only with
Illustration illustrates basic structure of the invention, therefore it only shows the composition relevant to the invention.
As shown in Figure 1, a kind of aircraft bad weather oiling protective device, including cover 1, cover 1 is by the upper of sleeve-shaped
It housing 11 and is formed in round table-like lower encioser 12 is extended out, the top of upper encloser 11 is provided with Rubber washer 4, in Rubber washer 4
Centre offers the oil gun mouth 41 penetrated for refueling nozzle, the bottom of lower encioser 12 is provided with circular magnetic chuck 2, in circular magnetic chuck 2
The heart offers the through-hole for placing refueling nozzle, and refueling nozzle successively passes through oil gun mouth 41 and through-hole and is connected to aircraft refuelling mouth, aircraft
Oil filler is tightly attached on the lower surface of sucker 2 by sucker 2, is covered with anti-abrasion pad 3 on one side on the lateral surface of lower encioser 12；
Another side on the lateral surface of lower encioser 12 is provided with Perspex mouth 8, is evenly arranged on Perspex mouth 8
Several air vents 9 are additionally provided with the cover 6 for rolling, and the lower edge of cover 6 in the outside of Perspex mouth 8
Lower edge with Perspex mouth 8 is in 15 ~ 45 ° of angle.
Specifically, the top edge of Perspex mouth 8 is additionally provided with several LED cold light lamps driven by button cell
5, to adapt to the needs of night refueling and observation.
Specifically, the lateral surface of lower encioser 12 is provided with ground line 7, ground line 7 and the static discharger on aircraft wing
Connection discharges the electrostatic that cover generates by the static discharger on aircraft wing.
Specifically, the lateral surface of lower encioser 12 is additionally provided with storage space 10, and 10 memory of storage space is placed with rubber gloves,
Rubber gloves are used, when opening fuel tank flap and closing fuel tank flap to protect hand to prevent external dust and grease stain.
Specifically, cover 6 is all put down pave after, between the lower edge of cover 6 and the lower edge of Perspex mouth 8
There are the gaps of triangle, and the location of airport staff and angle are uncertain when due to bad weather, so that
Even if internal oil gas can be still discharged by the air vent 9 of the gap location of triangle, outside after cover 6, which is all put down, to be paved
Portion maintenance personnel can still observe the situations such as internal volume read-out in different angles and positions in time.
Specifically, the lower surface of circular magnetic chuck 2 is evenly arranged with several suction pawls, to improve the absorption with aircraft refuelling mouth
Effect.
Specifically, anti-abrasion pad 3 can be removed manually, and when refueling, pad is avoided in the contact site of refueling nozzle and oil gun mouth 41
Refueling nozzle is larger heavier when oiling, to rub and collide with caused by refueling nozzle and airplane component, airframe is caused to damage
Wound, and anti-abrasion pad is set together with protective device, easily takes and easily takes, and is not easy to forget；Anti-abrasion pad 3, Rubber washer 4, Yi Jiyuan simultaneously
Shape sucker 2 is fitted closely with refueling nozzle, can play sealing function；Anti-abrasion pad 3 can also be covered on lower encioser 12 again when not used
Lateral surface on, take conveniently.
Specifically, Perspex mouth 8 is set on the lateral surface of lower encioser 12 and is located at anti-abrasion pad 3 and storage space
Between 10.
Specifically, Perspex mouth 8 is symmetrically arranged with 2 on the lateral surface of lower encioser 12.
Cover 1 will consider that wind direction avoids oil gun mouth 41 from placing windward when placing, and not have to observe for a long time when refueling organic
Glass viewing port.
Taking the above-mentioned ideal embodiment according to the present invention as inspiration, through the above description, relevant staff is complete
Various changes and amendments can be carried out without departing from the scope of the technological thought of the present invention' entirely.The technology of this invention
Property range is not limited to the contents of the specification, it is necessary to which the technical scope thereof is determined according to the scope of the claim.
Claims (9)
1. a kind of aircraft bad weather oiling protective device, including cover (1), the cover (1) is by the upper encloser in sleeve-shaped
(11) and in round table-like lower encioser (12) composition is extended out, Rubber washer (4), Rubber washer are provided at the top of upper encloser (11)
(4) center offers the oil gun mouth (41) penetrated for refueling nozzle, and the bottom of lower encioser (12) is provided with circular magnetic chuck (2),
It is covered with anti-abrasion pad (3) on one side on the lateral surface of lower encioser (12)；It is characterized in that, on the lateral surface of lower encioser (12)
Another side be provided with Perspex mouth (8), several air vents (9) are evenly arranged on Perspex mouth (8),
The cover (6) for rolling, and the lower edge of cover (6) and organic glass are additionally provided on the outside of Perspex mouth (8)
The lower edge of glass observation panel (8) is in 15 ~ 45 ° of angle.
2. protective device according to claim 1, it is characterised in that: the top edge of the Perspex mouth (8) is also
It is provided with several LED cold light lamps (5) driven by button cell.
3. protective device according to claim 1, it is characterised in that: the lateral surface of the lower encioser (12) is provided with ground connection
Line (7), the ground line (7) connect with the static discharger on aircraft wing.
4. protective device according to claim 1, it is characterised in that: the lateral surface of the lower encioser (12) is additionally provided with storage
It hides space (10), storage space (10) memory is placed with rubber gloves.
5. protective device according to claim 1, it is characterised in that: the cover (6) is all put down pave after, cover
(6) there are the gaps of triangle between the lower edge of lower edge and Perspex mouth (8).
6. protective device according to claim 1, it is characterised in that: the lower surface of the circular magnetic chuck (2) is uniformly arranged
There are several to inhale pawl.
7. protective device according to claim 1, it is characterised in that: the anti-abrasion pad (3) can manually remove, when refueling
Pad is in the contact site of refueling nozzle and oil gun mouth (41).
8. protective device according to claim 4, it is characterised in that: the Perspex mouth (8) is set to lower cover
On the lateral surface of shell (12) and between anti-abrasion pad (3) and storage space (10).
9. protective device according to claim 8, it is characterised in that: the Perspex mouth (8) is in lower encioser
(12) 2 are symmetrically arranged on lateral surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711449054.6A CN109969423A (en) | 2017-12-27 | 2017-12-27 | A kind of aircraft bad weather oiling protective device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711449054.6A CN109969423A (en) | 2017-12-27 | 2017-12-27 | A kind of aircraft bad weather oiling protective device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109969423A true CN109969423A (en) | 2019-07-05 |
Family
ID=67072235
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711449054.6A Withdrawn CN109969423A (en) | 2017-12-27 | 2017-12-27 | A kind of aircraft bad weather oiling protective device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109969423A (en) |
-
2017
- 2017-12-27 CN CN201711449054.6A patent/CN109969423A/en not_active Withdrawn
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| ES2682964A1 (en) | AEROTRANSPORTABLE DEVICE FOR LAUNCHING PRESSURE LIQUID (Machine-translation by Google Translate, not legally binding) | |
| CN107298184A (en) | A kind of protection type unmanned plane draw off gear | |
| CN207860497U (en) | A kind of aircraft bad weather oiling protective device | |
| CN109969423A (en) | A kind of aircraft bad weather oiling protective device | |
| CN205819535U (en) | A kind of aircraft fuselage skin osculum seals structure | |
| CN108216557A (en) | A kind of unmanned marine monitoring aircraft | |
| CN205982238U (en) | Machine carries rain -proof box of temperature and humidity sensor probe | |
| CN208770733U (en) | A kind of automatic water cannon runner big gun head protection cover | |
| CN207144555U (en) | Protective room in airfield runway automatic tour inspection system | |
| CN205378744U (en) | Bird robot is driven in intellectuality | |
| CN205872434U (en) | Unmanned aerial vehicle fuselage protector | |
| CN100577256C (en) | Airplane fuel oil filtering apparatus based on high altitude environment | |
| CN208616187U (en) | A kind of aircraft earth observation window assembly | |
| CN207496457U (en) | A kind of automotive oil tank outer cover | |
| CN202869861U (en) | Protective device for sampling | |
| CN206442626U (en) | Protective housing for atmospheric sampling instrument | |
| CN204090864U (en) | A kind of laser bird dispeller of multifunctional protection type | |
| CN214775569U (en) | Rain-proof cap of tank car | |
| CN201559813U (en) | Novel pilotless aircraft engine cover | |
| CN204037915U (en) | A kind of unmanned plane | |
| CN108128452A (en) | A kind of VTOL formula fixed-wing unmanned plane | |
| CN208813520U (en) | Large-scale fixed wing aircraft modular shelter coat | |
| CN204371061U (en) | A kind of OLED is except haze clearing window | |
| CN209495602U (en) | A kind of rotating turret type multifunctional protecting cabin | |
| CN109911238A (en) | A kind of seaplane oiling method |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190705 |