CN109398736A - Aircraft landing runway and aero tyre - Google Patents
Aircraft landing runway and aero tyre Download PDFInfo
- Publication number
- CN109398736A CN109398736A CN201811561437.7A CN201811561437A CN109398736A CN 109398736 A CN109398736 A CN 109398736A CN 201811561437 A CN201811561437 A CN 201811561437A CN 109398736 A CN109398736 A CN 109398736A
- Authority
- CN
- China
- Prior art keywords
- runway
- aircraft
- aircraft landing
- pastes
- recess
- 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
- 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
- B64F1/02—Arresting gear; Liquid barriers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
- B64C25/36—Arrangements or adaptations of wheels, tyres or axles in general
-
- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01C—CONSTRUCTION OF, OR SURFACES FOR, ROADS, SPORTS GROUNDS, OR THE LIKE; MACHINES OR AUXILIARY TOOLS FOR CONSTRUCTION OR REPAIR
- E01C9/00—Special pavings; Pavings for special parts of roads or airfields
Abstract
The invention discloses a kind of aircraft landing runway and aero tyres, it is characterized in that the aircraft landing runway is divided into three sections, two sections of front and back is existing runway, interlude is equipped with into lower recess, recess pastes stick, before, during and after three sections of surface in same level, the aircraft nose wheel tire is existing tire, two rear tyre surfaces, which are equipped with, pastes tooth, after aircraft landing runway of the invention is in contact with aero tyre, mutual paste link stops rapidly after making aircraft landing, is particularly suitable for using on the aircraft carrier with ejector.
Description
Technical field
The invention belongs to technical field of aerospace, specifically, more particularly to a kind of aircraft landing runway and aero tyre.
Background technique
National defence of the air force, China in China is very important, even more important especially in coastal frontier defense, now, China
There is the aircraft carrier of oneself, therefore, very high to air force pilot's requirement of ship-board aircraft, air force pilot needs process very long
The flight training of time, gets to the requirement of carrier-borne pilot, one of the main reasons, be exactly the landing distance of runway too
It is short, it is especially high to the technical requirements of pilot, as soon as cultivating a carrier-borne aircraft pilot, used dedicated for aircraft landing training
Many fuel oils and many valuable times of pilot cannot be cultivated in a short time more since the aircraft carrier in China is limited
More carrier-borne aircraft pilots uses cobweb principle for this purpose, aircraft landing runway of the invention and aero tyre, can be compared with
Big degree shortens the gliding landing distance of ship-board aircraft, reduce carrier-borne aircraft warship risk, can be in shorter flight training
Warship technology is known, turns out more carrier-borne aircraft pilots for China.
Summary of the invention
Aircraft landing runway that is simple, practical, facilitating aircraft landing is installed the purpose of the present invention is to provide a kind of
And aero tyre.
In order to achieve the above object, the present invention provides a kind of aircraft landing runway and aero tyre, it is characterised in that described
Aircraft landing runway is divided into three sections, and two sections of front and back runway is existing runway, and interlude runway is equipped with into lower recess, recess to be pasted
Stick, in same level, the aircraft nose wheel tire is existing tire on the surface of leading portion runway, middle section runway and back segment runway,
Aircraft rear tyre surface, which is equipped with, pastes the gear teeth.
As optimization: the interlude runway is equipped with into lower recess, recess pastes stick, pastes and is equipped between stick
The place of isolation strip, isolation strip section runway in the pre-connection wants wider, successively successively decreases；The stickup stick is close to leading portion
The place of runway wants narrower, incremented by successively；As another optimization, it is equipped on pasting stick and pastes tooth, paste the direction of tooth
The stickup tooth that the gear teeth and runway are pasted to runway back sweep, when aircraft landing is mutually ratcheting hingedly, and the inertia of aircraft is quickly disappeared
Consuming makes aircraft stop in relatively short distance.
As optimization: the aircraft nose wheel tire is existing aero tyre, two rear tyre surface both sides of aircraft and two sides
Equipped with pasting the gear teeth, the stickup gear teeth are to the same direction and aircraft forward to inclination, the stickup tooth of tilt angle and runway
It is corresponding to coincide.
As another optimization: freezing plastic can be equipped on the stickup stick of runway, increase stickup dynamics to shorten drop
The gliding distance of aircraft is fallen, while being equipped with softening agent in aircraft nose wheel prevents aircraft nose wheel from pasting, electrostatic and friction in order to prevent
The spark of generation can be put into seawater (liquid) in recess；As another optimization, runway part can be magnetized, flown
Machine rear-wheel installs magnetisable material additional, is quickly come to a complete stop after aircraft landing by magnetic pole principle.
In the technical program, new material energy and aircraft landing can be used as the resistance drop umbrella into one-step optimization again, airplane tail group
Runway phase adhesion, to increase the resistance of aircraft glide；Or resistance device is set in airplane tail group, for example formed with runway
A kind of magnetic devices to attract each other.
In conclusion aircraft landing runway of the invention and aero tyre, after there is mutual paste link to make aircraft landing
Stop rapidly, is particularly suitable for the aircraft carrier with ejector device and uses.
Detailed description of the invention
Fig. 1 is structural schematic diagram of the invention.
Fig. 2 is the structural relation figure of the aircraft landing runway in the present invention.
Fig. 3 is the structure chart of the aircraft rear tyre in the present invention.
Fig. 4 is the sectional view of the aircraft rear tyre in the present invention.
Specific embodiment
The present invention will be further described in detail below with reference to the accompanying drawings and embodiments.
When it is implemented, as shown in Figures 1 to 4, a kind of aircraft landing runway 1 and aero tyre 2, it is characterised in that described
It is three sections that aircraft landing runway 1, which divides, and two sections of front and back is existing runway 3, and interlude runway 4 is equipped with into lower recess 4a, recess 4a
Stick 5 is pasted, in same level, the aircraft nose wheel tire 2 is on the surface of leading portion runway 3, middle section runway 4 and back segment runway 3
Existing aero tyre 2, two surfaces rear tyre 2a of aircraft, which are equipped with, pastes the gear teeth 6；Isolation strip is equipped between the stickup stick 5
7；The stickup gear teeth 6 are to the same direction and aircraft forward to inclination.
In addition, when it is implemented, following the steps below to implement:
1, installation prepare: on aircraft landing runway 1, by runway interlude to lower recess 4a be predetermined depth, paste stick 5
On set paste tooth 5a, by the original rear tyre of aircraft be changed to paste the gear teeth 6 rear tyre 2a；
2, runway is installed: successively isolation strip 7, stickup stick 5 being laid on the runway of recess 4a.
Present embodiment is used only for further explanation of the invention rather than limits, when it is implemented, may be used also
To make various equivalent variations without departing from the spirit and scope of the present invention, for example runway part magnetized, after aircraft
Wheel installs magnetisable material additional, or forms a kind of magnetic devices to attract each other in airplane tail group setting resistance device and runway
Deng then should be regarded as equivalent replacement and still fall within protection scope of the present invention.
Claims (3)
1. a kind of aircraft landing runway and aero tyre, it is characterised in that the aircraft landing runway is divided into three sections, two sections of front and back
Runway is existing runway, and interlude runway is equipped with into lower recess, recess pastes stick, leading portion runway, middle section runway and back segment
In same level, the aircraft nose wheel tire is existing tire on the surface of runway, and aircraft rear tyre surface, which is equipped with, pastes the gear teeth.
2. aircraft landing runway according to claim 1 and aero tyre, it is characterised in that: the interlude runway is downward
It is equipped in recess, recess and pastes stick, pasted and be equipped with isolation strip between stick.
3. aircraft landing runway according to claim 1 and aero tyre, it is characterised in that: the aircraft nose wheel tire is existing
Have a tire, the rear tyre surface two sides of aircraft, which are equipped with, pastes the gear teeth, the stickup gear teeth to the same direction and aircraft forward to
Inclination.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811561437.7A CN109398736A (en) | 2018-12-12 | 2018-12-12 | Aircraft landing runway and aero tyre |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811561437.7A CN109398736A (en) | 2018-12-12 | 2018-12-12 | Aircraft landing runway and aero tyre |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109398736A true CN109398736A (en) | 2019-03-01 |
Family
ID=65460052
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811561437.7A Pending CN109398736A (en) | 2018-12-12 | 2018-12-12 | Aircraft landing runway and aero tyre |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109398736A (en) |
Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2004037450A2 (en) * | 2002-10-23 | 2004-05-06 | Coelho, Marcelo Machado | Landing gear of aircraft with air jet devices |
| US20040165950A1 (en) * | 2003-02-24 | 2004-08-26 | Rastegar Jahangir S. | Roadway for decelerating and/or accelerating a vehicle including and aircraft |
| US20040256519A1 (en) * | 2003-03-12 | 2004-12-23 | Ellis Stephen C. | System for recovery of aerial vehicles |
| CN2892532Y (en) * | 2006-04-13 | 2007-04-25 | 朱华强 | Vehicle antisliding strip |
| CN101301886A (en) * | 2007-05-11 | 2008-11-12 | 董泽明 | Automobile strong adherence ground type super resistance source braking system |
| CN102837829A (en) * | 2011-06-25 | 2012-12-26 | 孙善骏 | Flying and landing retardance runway |
| CN103121443A (en) * | 2011-11-19 | 2013-05-29 | 李忠华 | Prompt braking assembly |
| KR20150057619A (en) * | 2013-11-20 | 2015-05-28 | 한국항공우주연구원 | Means for take-off and landing of vertical take-off and landing miniature drone |
| CN105691629A (en) * | 2016-01-27 | 2016-06-22 | 陈小燕 | Anti-skid blanket for aircraft to take off from or land on snowfield |
| CN106068351A (en) * | 2014-03-03 | 2016-11-02 | 工程阻拦系统公司 | Macroscopic pattern formed material and structure for vehicles arresting system |
| CN106628221A (en) * | 2016-11-08 | 2017-05-10 | 黄延庆 | Novel airplane runway |
| CN206644601U (en) * | 2017-04-20 | 2017-11-17 | 代志军 | A kind of antiskid device for tire of agricultural machine |
-
2018
- 2018-12-12 CN CN201811561437.7A patent/CN109398736A/en active Pending
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2004037450A2 (en) * | 2002-10-23 | 2004-05-06 | Coelho, Marcelo Machado | Landing gear of aircraft with air jet devices |
| US20040165950A1 (en) * | 2003-02-24 | 2004-08-26 | Rastegar Jahangir S. | Roadway for decelerating and/or accelerating a vehicle including and aircraft |
| US20040256519A1 (en) * | 2003-03-12 | 2004-12-23 | Ellis Stephen C. | System for recovery of aerial vehicles |
| CN2892532Y (en) * | 2006-04-13 | 2007-04-25 | 朱华强 | Vehicle antisliding strip |
| CN101301886A (en) * | 2007-05-11 | 2008-11-12 | 董泽明 | Automobile strong adherence ground type super resistance source braking system |
| CN102837829A (en) * | 2011-06-25 | 2012-12-26 | 孙善骏 | Flying and landing retardance runway |
| CN103121443A (en) * | 2011-11-19 | 2013-05-29 | 李忠华 | Prompt braking assembly |
| KR20150057619A (en) * | 2013-11-20 | 2015-05-28 | 한국항공우주연구원 | Means for take-off and landing of vertical take-off and landing miniature drone |
| CN106068351A (en) * | 2014-03-03 | 2016-11-02 | 工程阻拦系统公司 | Macroscopic pattern formed material and structure for vehicles arresting system |
| CN105691629A (en) * | 2016-01-27 | 2016-06-22 | 陈小燕 | Anti-skid blanket for aircraft to take off from or land on snowfield |
| CN106628221A (en) * | 2016-11-08 | 2017-05-10 | 黄延庆 | Novel airplane runway |
| CN206644601U (en) * | 2017-04-20 | 2017-11-17 | 代志军 | A kind of antiskid device for tire of agricultural machine |
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| 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 | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190301 |