CN203512028U - Undercarriage folding and unfolding device for airplane - Google Patents
Undercarriage folding and unfolding device for airplane Download PDFInfo
- Publication number
- CN203512028U CN203512028U CN201320436314.7U CN201320436314U CN203512028U CN 203512028 U CN203512028 U CN 203512028U CN 201320436314 U CN201320436314 U CN 201320436314U CN 203512028 U CN203512028 U CN 203512028U
- Authority
- CN
- China
- Prior art keywords
- control module
- airplane
- height
- folding
- motor control
- 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
Links
Images
Landscapes
- Traffic Control Systems (AREA)
Abstract
The utility model discloses an undercarriage folding and unfolding device for an airplane. The undercarriage folding and unfolding device comprises a control circuit part and a mechanical driving mechanism, wherein the mechanical driving mechanism comprises a motor, a buffer, a piston rod and a connecting component; the control circuit part is provided with a motor control module; the buffer is provided with a laser rangefinder for calculating the height between the airplane and a runway; and the laser rangefinder is connected with the motor control module; and the motor control module controls the folding and unfolding heights of the piston rod by the laser rangefinder. The undercarriage folding and unfolding device disclosed by the utility model has the advantages that the height between the airplane and the runway when the airplane takes off and lands can be calculated by measurement of the laser rangefinder, and the piston rod is controlled by the actual height to adjust the height of wheels, so that the practicability is strong and the promotion value is large.
Description
Technical field
The utility model relates to the undercarriage control device that a kind of aircraft is used.
Background technology
At present, the alighting gear of aircraft is followed the take-off and landing state of different aircrafts and is changed, and wherein the folding structure of the alighting gear of aircraft need to regulate folding and unfolding height according to the distance of real aircraft and runway, and traditional undercarriage tends to because it is improper to regulate, and taking off while landing and the friction of the large resistance of runway, often emerge one blue or green cigarette or print at the runway one section of deep tire that rubs out of friction on runway, causes the serious wearing and tearing of tire.
Utility model content
The utility model, in order to solve the above-mentioned deficiency of prior art, has proposed the undercarriage control device that a kind of aircraft is used.
In order to solve the problems of the technologies described above, the utility model by the following technical solutions: the undercarriage control device that a kind of aircraft is used, comprise control circuit part and mechanical driving mechanism, mechanical driving mechanism comprises motor, energy disperser, piston rod and coupling assembling; Described control circuit partly has motor control module; On described energy disperser, be provided with one for calculating the airborne laser range finder of aircraft and runway height, described airborne laser range finder is connected with motor control module, and described motor control module is by the folding and unfolding height of airborne laser range finder control plunger bar.
Compared with prior art, the airborne laser range finder that the utility model increase to arrange can meter calculate aircraft and runway between distance, and feed back to motor control module, motor control module judges, and by controlling the folding and unfolding height of motor adjusting piston bar, avoid the wearing and tearing of tire when take-off and landing, extended the service life of aircraft tyre.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
The specific embodiment
Below in conjunction with drawings and Examples, utility model is described in detail.
As shown in Figure 1, the undercarriage control device that the aircraft the utility model proposes is used, comprises control circuit part and mechanical driving mechanism, and mechanical driving mechanism comprises motor, energy disperser 1, piston rod 2 and coupling assembling; Control circuit partly has motor control module; On energy disperser 1, be provided with one for calculating the airborne laser range finder 3 of aircraft and runway height, airborne laser range finder 3 is connected with motor control module, and described motor control module is by the folding and unfolding height of airborne laser range finder control plunger bar 2.
In the utility model, airborne laser range finder 3 can meter calculate aircraft and runway between distance, and feed back to motor control module, motor control module carries out discriminatory analysis according to observed reading, and by controlling the folding and unfolding height of motor adjusting piston bar 2, the wearing and tearing of tire when take-off and landing have been avoided.
Above-described embodiment has only been expressed several embodiment of the present utility model, and it describes comparatively concrete and detailed, but can not therefore be interpreted as the restriction to the utility model the scope of the claims.It should be pointed out that for the person of ordinary skill of the art, without departing from the concept of the premise utility, can also make some distortion and improvement, these all belong to protection domain of the present utility model.Therefore, the utility model patent and protection domain should be as the criterion with appended claims.
Claims (1)
1. the undercarriage control device that aircraft is used, comprises control circuit part and mechanical driving mechanism, and mechanical driving mechanism comprises motor, energy disperser (1), piston rod (2) and coupling assembling; Described control circuit partly has motor control module; It is characterized in that: on described energy disperser, be provided with one for calculating the airborne laser range finder (3) of aircraft and runway height, described airborne laser range finder (3) is connected with motor control module, and described motor control module is by the folding and unfolding height of airborne laser range finder control plunger bar (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320436314.7U CN203512028U (en) | 2013-07-22 | 2013-07-22 | Undercarriage folding and unfolding device for airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320436314.7U CN203512028U (en) | 2013-07-22 | 2013-07-22 | Undercarriage folding and unfolding device for airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203512028U true CN203512028U (en) | 2014-04-02 |
Family
ID=50371001
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320436314.7U Expired - Fee Related CN203512028U (en) | 2013-07-22 | 2013-07-22 | Undercarriage folding and unfolding device for airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203512028U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105015788A (en) * | 2014-04-21 | 2015-11-04 | 哈尔滨飞机工业集团有限责任公司 | Landing gear |
| CN110395082A (en) * | 2018-04-25 | 2019-11-01 | 长城汽车股份有限公司 | Control method, system and the hovercar of hovercar |
-
2013
- 2013-07-22 CN CN201320436314.7U patent/CN203512028U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105015788A (en) * | 2014-04-21 | 2015-11-04 | 哈尔滨飞机工业集团有限责任公司 | Landing gear |
| CN110395082A (en) * | 2018-04-25 | 2019-11-01 | 长城汽车股份有限公司 | Control method, system and the hovercar of hovercar |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105667768A (en) | Unmanned aerial vehicle take-off or landing control system and control method | |
| RU2011146418A (en) | AIRCRAFT LIFTING INCREASE SYSTEM, AIRCRAFT SYSTEM AND SCREW AIRPLANE WITH LIFTING INCREASE SYSTEM | |
| CN205524527U (en) | Outer intelligent fin of hanging automatic rising of automobile | |
| CN102407938B (en) | Wing installed with variant wingtip winglet and working mode thereof | |
| CN103869821B (en) | Onboard automatic pesticide balancing system of agricultural unmanned aerial vehicle | |
| WO2012134701A3 (en) | Method of reducing fuel carried by an aircraft in flight | |
| CN202966654U (en) | Fixed wing unmanned aerial vehicle for engineer operation | |
| CN203512028U (en) | Undercarriage folding and unfolding device for airplane | |
| CN205418143U (en) | Sensing remote control 's rod -type arresting net device that takes off and land | |
| CN203143013U (en) | Aircraft plateau mooring device | |
| CN202848035U (en) | Electromagnetic type helicopter deck | |
| CN203428026U (en) | Small duct-type aircraft | |
| CN203889080U (en) | Vertical lifting holder device of unmanned aerial vehicle | |
| CN205273844U (en) | Many rotors independently receive and release undercarriage entirely | |
| CN205730366U (en) | A kind of wing horizontal tail full dynamic formula aircraft model plane | |
| CN102530257A (en) | Forced landing device for civil aircrafts | |
| CN202379089U (en) | Novel unmanned aerial vehicle | |
| CN203386409U (en) | Demonstration device for aircraft carrier arresting cable | |
| CN201343148Y (en) | Airplane forced landing cushioning platform | |
| CN105015788B (en) | A kind of undercarriage | |
| CN204737037U (en) | Aircraft consumes oily control system | |
| CN205499334U (en) | Light aircraft formula rudder that can ftracture | |
| CN105741612A (en) | Systemic method capable of quickly releasing take-off of short-medium range aircrafts | |
| CN202406908U (en) | Novel bird repelling electronic control system | |
| CN109131846A (en) | A kind of undercarriage hand steering gear |
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 |
Granted publication date: 20140402 Termination date: 20140722 |
|
| EXPY | Termination of patent right or utility model |