CN204776061U - Aircraft on aircraft carrier can prevent to rush out device of runway when from taking off and land - Google Patents
Aircraft on aircraft carrier can prevent to rush out device of runway when from taking off and land Download PDFInfo
- Publication number
- CN204776061U CN204776061U CN201520430474.XU CN201520430474U CN204776061U CN 204776061 U CN204776061 U CN 204776061U CN 201520430474 U CN201520430474 U CN 201520430474U CN 204776061 U CN204776061 U CN 204776061U
- Authority
- CN
- China
- Prior art keywords
- runway
- aircraft
- damper leg
- roller bearing
- carbon roller
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses an aircraft on aircraft carrier can prevent to rush out device of runway when from taking off and land, include by a plurality of being " one " font arrange in proper order set up the bumper post that puts, set up carbon roller bearing between bumper post, bumper post group that the bearing of the piston cross shaft joint of bumper post top and piston cross shaft joint both sides constitutes, characterized by: the bumper post component is do not buried underground perpendicularly and is buried underground in the left and right both sides of runway in runway below and parallel, and the carbon roller bearing is higher than airport runway surface 2 -4cm. The utility model has the advantages that: simple structure, convenient operation, the take -off speed of aircraft can also can be accelerated to the runway of rushing out out of control in the time of can not only preventing that aircraft on the aircraft carrier from taking off and land when taking off, slow down when the descending taxiing speed of aircraft of aircraft.
Description
Technical field
The utility model relates to takeoff and landing, the device specifically gunned off the runway during a kind of takeoff and landing that can prevent on aircraft carrier.
Background technology
Taking off of traditional aircraft does not have power-assisted, only takes off by engine power, takes off slow, and fuel oil power consumption is large; Mainly rely on parachute to produce resistance during aircraft landing, aircraft landing brake is slow.
For this reason, applicant in this case once disclosed a kind of device that can provide power-assisted and resistance to takeoff and landing with Chinese patent CN203714180U, this device is provided with damper leg at the sagging direct-burried of airstrip, carbon roller bearing and piston cross drive coupling, though this structure can realize the takeoff speed accelerating aircraft when aircraft normally takes off, slow down when aircraft landing the object of coasting speed of aircraft, but nose wheel angle is the straight angle 180 degree during aircraft safety landing, and when aircraft nose wheel angle is less than the straight angle (i.e. obtuse angle), aircraft is easily out of control to gun off the runway, dangerous huge, therefore the practice effect of this device is unsatisfactory.
Utility model content
The purpose of this utility model is for overcoming the deficiencies in the prior art, and the device gunned off the runway during a kind of takeoff and landing that can prevent on aircraft carrier is provided, out of controlly when this device can not only prevent the takeoff and landing on aircraft carrier to gun off the runway, the takeoff speed accelerating aircraft when aircraft normally takes off can also be realized, the object of the coasting speed of the aircraft that slows down when aircraft landing.
The technical scheme realizing the utility model object is:
The device gunned off the runway during a kind of takeoff and landing that can prevent on aircraft carrier, comprise by multiple in " one " font order arrange setting damper leg, be arranged on the carbon roller bearing between damper leg, damper leg group that the bearing of the piston cross drive coupling above damper leg and piston cross drive coupling both sides is formed, unlike the prior art: damper leg group is embedded vertically at respectively below the runway of deck and is embedded in deck runway arranged on left and right sides with parallel, runway is that middle part is high, the low structure in both sides, carbon roller bearing higher than deck runway surface 2-4cm, wherein:
Bottom distance in the first damper leg group below runway between each carbon roller bearing and aircraft, the distance of two wheels is close;
Carbon roller bearing motion for the relative rotation respectively in second and third damper leg group of runway arranged on left and right sides, and contact with front-wheel bottom aircraft respectively;
The motor that the side of damper leg is provided with change speed gear box and is connected with change speed gear box, change speed gear box is connected with bearing.
Described runway arranged on left and right sides is slightly low 2-4cm in the middle of runway comparatively, and is provided with a drain tank at lower portion, and avoid has ponding in runway in rainy season weather.
Comprising 3-5 double acting oil gas damper leg in described each damper leg group, is prior art.
The length of described each carbon roller bearing is 4-5 rice.
During installation, under this device being embedded vertically at deck runway and arranged on left and right sides, carbon roller bearing, higher than runway ground, deck 2-4cm, is arranged along deck runway every 300 meters of intervals.
The working process of the utility model device is:
When aircraft is out of control, prepare to gun off the runway or sideslip time, drive carbon roller bearing to rotate to direction inside runway by electrical motor and change speed gear box, aircraft nose wheel produced and guides propelling thrust, aircraft is led back in normal runway, in straight angle Normal Take-Off And Landing;
When taking off, driving carbon roller bearing to operate in the same way to the direction of wheel turns when taking off by electrical motor and change speed gear box, to taking off generation power-assisted, reaching the object accelerating speed of taking off; When aircraft landing, drive carbon roller bearing to the direction reversed operation of wheel turns during aircraft landing by electrical motor and change speed gear box, produce resistance to aircraft landing, reach the object of the aircraft taxi speed that slows down.
The utility model has the advantages that: structure is simple, easy to operate, out of controlly when can not only prevent the takeoff and landing on aircraft carrier to gun off the runway, can also can accelerate the takeoff speed of aircraft when taking off, the coasting speed of the aircraft that slows down during aircraft landing.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is integral installation schematic diagram of the present utility model.
In figure: 1. damper leg 2. carbon roller bearing 3. piston cross drive coupling 4. bearing 5. electric shift case 6. electrical motor.
Detailed description of the invention
With reference to Fig. 1, the device gunned off the runway during a kind of takeoff and landing that can prevent on aircraft carrier, by by 3-5 in " one " font order arrange setting double acting oil gas damper leg, be arranged on the carbon roller bearing between damper leg, the first damper leg group, the second damper leg group and the 3rd damper leg group formation that the bearing of the piston cross drive coupling above damper leg and piston cross drive coupling both sides form, first damper leg group is embedded vertically at below the runway of deck, and bottom the distance between each carbon roller bearing and aircraft, the distance of two wheels is close; Second damper leg group and the 3rd damper leg group are set in parallel in runway arranged on left and right sides respectively, carbon roller bearing motion for the relative rotation respectively in the second damper leg group and three damper leg groups, and contact with front-wheel bottom aircraft respectively; Carbon roller bearing is higher than airport runway surface 2-4cm, and the length of each carbon roller bearing is 4-5 rice.The motor that the side of damper leg is provided with change speed gear box and is connected with change speed gear box, change speed gear box is connected with bearing.Runway arranged on left and right sides is slightly low 2-4cm in the middle of runway comparatively, and is provided with a drain tank at lower portion, and avoid has ponding in runway in rainy season weather
Described damper leg group by damper leg 1, be arranged on the first module that the piston cross drive coupling 3 on damper leg 1 and the bearing 4 that is arranged on piston cross drive coupling 3 both sides form, this unit from bearing 4 turn left in-line order be disposed with carbon roller bearing 2, bearing 4, piston cross drive coupling 3, bearing 4, electric shift case 5 and electrical motor 6, formed second unit; First module from bearing 4 turn right in-line order arrangement be also provided with carbon roller bearing 2, bearing 4, piston cross drive coupling 3, bearing 4, electric shift case 5 and electrical motor 6, form Unit the 3rd, first module, to be separated by carbon roller bearing 2 between second unit and Unit the 3rd.
Claims (4)
1. the device that can prevent from gunning off the runway during the takeoff and landing on aircraft carrier, comprise by multiple in " one " font order arrange setting damper leg, be arranged on the carbon roller bearing between damper leg, damper leg group that the bearing of the piston cross drive coupling above damper leg and piston cross drive coupling both sides is formed, it is characterized in that: damper leg group is embedded vertically at respectively below the runway of deck and is embedded in deck runway arranged on left and right sides with parallel, runway is that middle part is high, the low structure in both sides, carbon roller bearing higher than airport runway surface 2-4cm, wherein:
Bottom distance in the first damper leg group below runway between each carbon roller bearing and aircraft, the distance of two wheels is close;
Carbon roller bearing motion for the relative rotation respectively in second and third damper leg group of runway arranged on left and right sides, and contact with front-wheel bottom aircraft respectively;
Runway arranged on left and right sides is comparatively slightly low in the middle of runway, the motor that the side of damper leg is provided with change speed gear box and is connected with change speed gear box, and change speed gear box is connected with bearing.
2. device according to claim 1, is characterized in that: described runway arranged on left and right sides is the middle slightly low 2-4cm of runway comparatively, and is provided with a drain tank at lower portion.
3. device according to claim 1, is characterized in that: comprise 3-5 double acting oil gas damper leg in described each damper leg group.
4. device according to claim 1, is characterized in that: the length of described each carbon roller bearing is 4-5 rice.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520430474.XU CN204776061U (en) | 2015-06-23 | 2015-06-23 | Aircraft on aircraft carrier can prevent to rush out device of runway when from taking off and land |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520430474.XU CN204776061U (en) | 2015-06-23 | 2015-06-23 | Aircraft on aircraft carrier can prevent to rush out device of runway when from taking off and land |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204776061U true CN204776061U (en) | 2015-11-18 |
Family
ID=54516163
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520430474.XU Expired - Fee Related CN204776061U (en) | 2015-06-23 | 2015-06-23 | Aircraft on aircraft carrier can prevent to rush out device of runway when from taking off and land |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204776061U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104986349A (en) * | 2015-06-23 | 2015-10-21 | 李竟儒 | Device capable of preventing aircraft on aircraft carrier from rushing out of runway in take-off and landing processes |
-
2015
- 2015-06-23 CN CN201520430474.XU patent/CN204776061U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104986349A (en) * | 2015-06-23 | 2015-10-21 | 李竟儒 | Device capable of preventing aircraft on aircraft carrier from rushing out of runway in take-off and landing processes |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151118 Termination date: 20210623 |