CN110155361A - A kind of aircraft landing system - Google Patents
A kind of aircraft landing system Download PDFInfo
- Publication number
- CN110155361A CN110155361A CN201910111596.5A CN201910111596A CN110155361A CN 110155361 A CN110155361 A CN 110155361A CN 201910111596 A CN201910111596 A CN 201910111596A CN 110155361 A CN110155361 A CN 110155361A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- vehicle
- travel controlling
- controlling system
- unlocking structure
- 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
- 230000007547 defect Effects 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
-
- 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
-
- 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
- B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
- B64F1/10—Ground or aircraft-carrier-deck installations for launching aircraft using self-propelled vehicles
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Transportation (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention discloses a kind of aircraft landing systems, including vehicle, travel controlling system and aircraft, locking unlocking structure is set on the vehicle, the structural body to match with the locking unlocking structure is set on the aircraft, the vehicle is controlled by the travel controlling system, and the travel controlling system is by the flying vehicles control.Aircraft landing system disclosed in this invention can omit the train system of aircraft, and then a series of huge brought defects of huge structure, complexity and the quality for overcoming tradition to have due to the aircraft of setting train.
Description
Technical field
The present invention relates to aircraft field more particularly to a kind of aircraft landing systems.
Background technique
The landing train of aircraft is very huge, complicated and quality is huge, if the train system tool of aircraft can be omitted
It is significant.Moreover, since unmanned plane is difficult to bear landing train, so omitting the landing train of aircraft to nobody
Machine has more significance.Therefore, it is necessary to invent a kind of course of new aircraft landing system.
Summary of the invention
To solve the above-mentioned problems, technical solution proposed by the present invention is as follows:
Scheme 1: a kind of aircraft landing system, including vehicle, travel controlling system and aircraft are set on the vehicle
Set locking unlocking structure, the structural body to match with the locking unlocking structure be set on the aircraft, the vehicle by
The travel controlling system control, the travel controlling system is by the flying vehicles control.
Scheme 2: a kind of aircraft landing system, including vehicle, travel controlling system and aircraft are set on the vehicle
Set locking unlocking structure, the structural body to match with the locking unlocking structure be set on the aircraft, the vehicle by
The travel controlling system control, the travel controlling system is by the flying vehicles control, and the locking unlocking structure is by described
Flying vehicles control.
Scheme 3: a kind of aircraft landing system, including vehicle, travel controlling system and aircraft are set on the vehicle
Set locking unlocking structure, the structural body to match with the locking unlocking structure be set on the aircraft, the vehicle by
The travel controlling system control, the travel controlling system are controlled by the driver of the aircraft.
Scheme 4: a kind of aircraft landing system, including vehicle, travel controlling system and aircraft are set on the vehicle
Set locking unlocking structure, the structural body to match with the locking unlocking structure be set on the aircraft, the vehicle by
The travel controlling system control, the travel controlling system are controlled by the driver of the aircraft, the locking unlock knot
Structure is controlled by the driver of the aircraft.
In the present invention, should according to the well-known technique in aircraft field, necessary place be arranged necessary component, unit or
System etc..
Beneficial effects of the present invention are as follows: aircraft landing system disclosed in this invention can omit the train of aircraft
System, and then the huge structure, complexity and the quality that overcome tradition to have due to the aircraft of setting train are huge brought
Defect.
Detailed description of the invention:
Fig. 1 is structural schematic diagram of the embodiment of the present invention 1 to embodiment 4.
Specific embodiment
Embodiment 1
As shown in Figure 1, a kind of aircraft landing system, including vehicle 1, travel controlling system 2 and aircraft 3, described
Locking unlocking structure 11 is set on vehicle 1, the structure to match with the locking unlocking structure 11 is set on the aircraft 3
Body 31, the vehicle 1 are controlled by the travel controlling system 2, and the travel controlling system 2 is controlled by the aircraft 3.
Embodiment 2
As shown in Figure 1, a kind of aircraft landing system, including vehicle 1, travel controlling system 2 and aircraft 3, described
Locking unlocking structure 11 is set on vehicle 1, the structure to match with the locking unlocking structure 11 is set on the aircraft 3
Body 31, the vehicle 1 are controlled by the travel controlling system 2, and the travel controlling system 2 is controlled by the aircraft 3, described
Locking unlocking structure 11 is controlled by the aircraft 3.
Embodiment 3
As shown in Figure 1, a kind of aircraft landing system, including vehicle 1, travel controlling system 2 and aircraft 3, described
Locking unlocking structure 11 is set on vehicle 1, the structure to match with the locking unlocking structure 11 is set on the aircraft 3
Body 31, the vehicle 1 are controlled by the travel controlling system 2, driver of the travel controlling system 2 by the aircraft 3
Control.
Embodiment 4
As shown in Figure 1, a kind of aircraft landing system, including vehicle 1, travel controlling system 2 and aircraft 3, described
Locking unlocking structure 11 is set on vehicle 1, the structure to match with the locking unlocking structure 11 is set on the aircraft 3
Body 31, the vehicle 1 are controlled by the travel controlling system 2, driver of the travel controlling system 2 by the aircraft 3
Control, the locking unlocking structure 11 are controlled by the driver of the aircraft 3.
It is clear that the invention is not restricted to above embodiments, according to techniques known and technology disclosed in this invention
Scheme, can derive or associate many variant schemes out, and all these variant schemes also are regarded as being protection model of the invention
It encloses.
Claims (4)
1. a kind of aircraft landing system, including vehicle (1), travel controlling system (2) and aircraft (3), it is characterised in that:
Locking unlocking structure (11) are set on the vehicle (1), setting and the locking unlocking structure (11) on the aircraft (3)
The structural body (31) to match, the vehicle (1) by the travel controlling system (2) control, the travel controlling system (2) by
Aircraft (3) control.
2. a kind of aircraft landing system, including vehicle (1), travel controlling system (2) and aircraft (3), it is characterised in that:
Locking unlocking structure (11) are set on the vehicle (1), setting and the locking unlocking structure (11) on the aircraft (3)
The structural body (31) to match, the vehicle (1) by the travel controlling system (2) control, the travel controlling system (2) by
Aircraft (3) control, the locking unlocking structure (11) are controlled by the aircraft (3).
3. a kind of aircraft landing system, including vehicle (1), travel controlling system (2) and aircraft (3), it is characterised in that:
Locking unlocking structure (11) are set on the vehicle (1), setting and the locking unlocking structure (11) on the aircraft (3)
The structural body (31) to match, the vehicle (1) by the travel controlling system (2) control, the travel controlling system (2) by
The driver of the aircraft (3) controls.
4. a kind of aircraft landing system, including vehicle (1), travel controlling system (2) and aircraft (3), it is characterised in that:
Locking unlocking structure (11) are set on the vehicle (1), setting and the locking unlocking structure (11) on the aircraft (3)
The structural body (31) to match, the vehicle (1) by the travel controlling system (2) control, the travel controlling system (2) by
The driver of the aircraft (3) controls, and the locking unlocking structure (11) is controlled by the driver of the aircraft (3).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810146141 | 2018-02-12 | ||
| CN2018101461412 | 2018-02-12 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110155361A true CN110155361A (en) | 2019-08-23 |
Family
ID=67645358
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910111596.5A Pending CN110155361A (en) | 2018-02-12 | 2019-02-12 | A kind of aircraft landing system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110155361A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104670516A (en) * | 2015-02-15 | 2015-06-03 | 南京理工大学 | Rapid taking-off and landing device of air vehicle |
| CN104760705A (en) * | 2015-02-15 | 2015-07-08 | 南京理工大学 | Vehicle-mounted aircraft taking-off and landing device |
| KR20160119988A (en) * | 2015-04-07 | 2016-10-17 | 자동차부품연구원 | Folding type multi-purpose multi-rotor drone which can takeoff and landing on the moving vehicle |
| CN106218914A (en) * | 2016-09-22 | 2016-12-14 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Aircraft and railcar overlap-connected landing system and method |
| CN106292684A (en) * | 2015-05-13 | 2017-01-04 | 日立(中国)研究开发有限公司 | Carry the vehicle of aircraft |
| CN206050096U (en) * | 2016-09-22 | 2017-03-29 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Aircraft and the overlap-connected landing system of railcar |
-
2019
- 2019-02-12 CN CN201910111596.5A patent/CN110155361A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104670516A (en) * | 2015-02-15 | 2015-06-03 | 南京理工大学 | Rapid taking-off and landing device of air vehicle |
| CN104760705A (en) * | 2015-02-15 | 2015-07-08 | 南京理工大学 | Vehicle-mounted aircraft taking-off and landing device |
| KR20160119988A (en) * | 2015-04-07 | 2016-10-17 | 자동차부품연구원 | Folding type multi-purpose multi-rotor drone which can takeoff and landing on the moving vehicle |
| CN106292684A (en) * | 2015-05-13 | 2017-01-04 | 日立(中国)研究开发有限公司 | Carry the vehicle of aircraft |
| CN106218914A (en) * | 2016-09-22 | 2016-12-14 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Aircraft and railcar overlap-connected landing system and method |
| CN206050096U (en) * | 2016-09-22 | 2017-03-29 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Aircraft and the overlap-connected landing system of railcar |
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| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |