CN206580464U - Suitable for the suspension bracket of the vertical assembling of Small General Aircraft front open type canopy - Google Patents
Suitable for the suspension bracket of the vertical assembling of Small General Aircraft front open type canopy Download PDFInfo
- Publication number
- CN206580464U CN206580464U CN201720081805.2U CN201720081805U CN206580464U CN 206580464 U CN206580464 U CN 206580464U CN 201720081805 U CN201720081805 U CN 201720081805U CN 206580464 U CN206580464 U CN 206580464U
- Authority
- CN
- China
- Prior art keywords
- suction cup
- main frame
- cup carrier
- canopy
- sucker
- 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
Landscapes
- Load-Engaging Elements For Cranes (AREA)
Abstract
A kind of suspension bracket suitable for the vertical assembling of Small General Aircraft front open type canopy, including base, support, hanging beam, canopy clamping device and posture levelling control module；The support is connected on base；The top of support connects the hanging beam；Slide rail and lifting motor are connected with hanging beam, the lifting rope of lifting motor connects the canopy clamping device；Lifting motor is slidably connected with slide rail；The canopy clamping device includes the main frame of square, and rotates the suction cup carrier being connected with main frame；Plane where the main frame is level；The suction cup carrier is with main frame link position on the diagonal of main frame；Multiple suckers are connected with the suction cup carrier, electric pushrod is connected between sucker and suction cup carrier, the end of electric pushrod is connected to sucker behind by ball head universal；Each sucker is in a center of symmetry around the center of gravity of suction cup carrier；Electrolevel is provided with suction cup carrier；The venthole connection asepwirator pump of sucker.This suspension bracket is easy to use, the assembling available for many types of canopy.
Description
Technical field
The utility model belongs to aircraft manufacturing technical field, is specifically that one kind is applied to Small General Aircraft front open type cockpit
Cover vertical assembling suspension bracket.
Background technology
Single seat or two-seater Small General Aircraft, are usually directly to open canopy, (can be airstair by boarding mechanism
Or set stepping on for main wing root to step on device) and enter cockpit, turn off canopy.And the opening ways of canopy are opened after also having
Formula, front open type and right hand model etc..The canopy opening ways of single seat type are more flexible, but for double seat cockpit arranged side by side,
Canopy opened before being mainly or after open.Due to aerodynamic demands and cockpit space requirement, canopy is bubble type, such seat
The rear portion of hatchcover is smaller, and the rotation link position of canopy is smaller, and the field of front vision of canopy is larger, also requires canopy
Front portion it is more smooth, and area is larger, suitable for front open type.In general, canopy is integral molding, and its material is high score
Sub- transparent material, its lower edge can be equipped with metal framework.When front open type canopy is installed, due to installation requirement, it is necessary to handle
Canopy, which is established, comes (i.e. metal framework nearly vertically face), at this time, it may be necessary to multiple person cooperational completion, is not easy to operation, and can
It can cause metal framework deformation.
The content of the invention
In order to solve the above problems, it is applied to Small General Aircraft front open type canopy the utility model proposes one kind vertical
The suspension bracket of assembling, it is characterized in that aligning control module including base, support, hanging beam, canopy clamping device and posture；The branch
Frame is connected on base；The top of support connects the hanging beam；Slide rail and lifting motor, the liter of lifting motor are connected with hanging beam
Drop rope and connect the canopy clamping device；Lifting motor is slidably connected with slide rail；
The canopy clamping device includes the main frame of square, and rotates the suction cup carrier being connected with main frame；The master
Plane where frame is level, and the corner of main frame connects the end of the lifting rope by isometric rope respectively；It is described to inhale
Plate rail and main frame link position are on the diagonal of main frame, and rotary shaft between them is parallel to plane where main frame and suction
Plane where plate rail；
Multiple suckers are connected with the suction cup carrier, electric pushrod is connected between sucker and suction cup carrier, electric pushrod
End is connected to sucker behind by ball head universal；Each sucker is in a center of symmetry around the center of gravity of suction cup carrier；In suction cup carrier
It is provided with electrolevel；The venthole connection asepwirator pump of sucker；
The posture levelling control module includes power supply and using single-chip microcomputer as the controller of core；The electrolevel
Data output end connects the data input pin of controller；The asepwirator pump control signal output of controller is connected by amplifying circuit
The control signal input of asepwirator pump；It is electronic that the electronic heap bar control signal output of controller connects each by amplifying circuit
The motor control signal input of push rod；Power supply is that electrolevel, controller, electric pushrod and lifting motor are powered.
This suspension bracket holds canopy (substantially vertically and ground, the deformation probability of frame is relatively low for canopy) using sucker,
And the isostructural center of gravity of canopy+suction cup carrier is adjusted by electric pushrod, suction cup carrier is stably connected with main frame, main frame and following
Part can be regarded as a stable entirety in mechanical analysis, (relative to inhale in the specific link position for being aided with four ropes
Plate rail), make them highly stable.In operation, if running into the fine setting situation that needs, manpower can do multi-angle to canopy
Action.
The base, support and hanging beam constitute " C " character form structure.Assembling when, base can below airframe,
Support is in the side of body, and hanging beam reserves personnel's working space of abundance above body.
Wheel is connected with by hydraulic stem on the base of the base；In the case where hydraulic stem is pressurized state, " L " shape pole is led to
Cross wheel connection ground；Under hydraulic stem top pressure release state, " L " shape pole directly contact face.Under the structure, it is easy to transhipment, makees
Industry state is the state in framework directly contact face, it is ensured that the stability of actual job.
Described power supply is battery, and battery is on base.Battery is heavier, positioned at the bottom of suspension bracket, further
Reduce overall center of gravity.
Compared with prior art, this suspension bracket is easy to use, the assembling available for many types of canopy.
Brief description of the drawings
Fig. 1 is the structural representation of this suspension bracket；
Fig. 2 is the side schematic view of this hanger portion；
Fig. 3 is the schematic top plan view of main frame；
Fig. 4 is the structural representation of suction cup carrier part；
In figure：It is base 1, support 2, hanging beam 3, lifting motor 4, lifting rope 5, main frame 6, suction cup carrier 7, rope 8, electronic
Push rod 9, ball head universal 10, electrolevel 11, hydraulic stem 12, wheel 13, sucker 14.
Embodiment
The technical program is further illustrated with embodiment below in conjunction with the accompanying drawings：
Such as Fig. 1, a kind of suspension bracket suitable for the vertical assembling of Small General Aircraft front open type canopy, including base, support,
Hanging beam, canopy clamping device and posture levelling control module；The support is connected on base；The top connection of support is described
Hanging beam；Slide rail and lifting motor (electric block) are connected with hanging beam, the lifting rope of lifting motor connects the canopy folder
Hold mechanism；Lifting motor is slidably connected with slide rail.
Such as Fig. 2, the base, support and hanging beam constitute " C " character form structure.
The canopy clamping device includes the main frame of square, and rotates the suction cup carrier being connected with main frame；The master
Plane where frame is level, and the corner of main frame connects the end of the lifting rope by isometric rope respectively；It is described to inhale
Plate rail and main frame link position are on the diagonal of main frame, and rotary shaft between them is parallel to plane where main frame and suction
Plane where plate rail；
Multiple suckers are connected with such as Fig. 4, the suction cup carrier, electric pushrod is connected between sucker and suction cup carrier, it is electronic
The end of push rod is connected to sucker behind by ball head universal；Each sucker is in a center of symmetry around the center of gravity of suction cup carrier；
Suction cup carrier is provided with electrolevel；The venthole connection asepwirator pump of sucker；
The posture levelling control module includes power supply and using single-chip microcomputer as the controller of core；The electrolevel
Data output end connects the data input pin of controller；The asepwirator pump control signal output of controller is connected by amplifying circuit
The control signal input of asepwirator pump；It is electronic that the electronic heap bar control signal output of controller connects each by amplifying circuit
The motor control signal input of push rod；Power supply is that electrolevel, controller, electric pushrod and lifting motor are powered.
Wheel is connected with by hydraulic stem on the base of the base；In the case where hydraulic stem is pressurized state, " L " shape pole is led to
Cross wheel connection ground；Under hydraulic stem top pressure release state, " L " shape pole directly contact face.
Described power supply is battery, and battery is on base.
Claims (4)
1. a kind of suspension bracket suitable for the vertical assembling of Small General Aircraft front open type canopy, it is characterized in that including base, support,
Hanging beam, canopy clamping device and posture levelling control module；The support is connected on base；The top connection of support is described
Hanging beam；Slide rail and lifting motor are connected with hanging beam, the lifting rope of lifting motor connects the canopy clamping device；Lifting
Motor is slidably connected with slide rail；
The canopy clamping device includes the main frame of square, and rotates the suction cup carrier being connected with main frame；The main frame institute
It is level in plane, the corner of main frame connects the end of the lifting rope by isometric rope respectively；The suction cup carrier
With main frame link position on the diagonal of main frame, and rotary shaft between them is parallel to plane where main frame and suction cup carrier
Place plane；
Multiple suckers are connected with the suction cup carrier, electric pushrod, the end of electric pushrod are connected between sucker and suction cup carrier
Sucker is connected to behind by ball head universal；Each sucker is in a center of symmetry around the center of gravity of suction cup carrier；Set in suction cup carrier
There is electrolevel；The venthole connection asepwirator pump of sucker；
The posture levelling control module includes power supply and using single-chip microcomputer as the controller of core；The data of the electrolevel
Output end connects the data input pin of controller；The asepwirator pump control signal output of controller connects air-breathing by amplifying circuit
The control signal input of pump；The electronic heap bar control signal output of controller connects each electric pushrod by amplifying circuit
Motor control signal input；Power supply is that electrolevel, controller, electric pushrod and lifting motor are powered.
2. suspension bracket according to claim 1, it is characterized in that the base, support and hanging beam constitute " C " character form structure.
3. suspension bracket according to claim 1, it is characterized in that being connected with wheel by hydraulic stem on the base of the base；
Hydraulic stem is under pressurized state, " L " shape pole connects ground by wheel；Under hydraulic stem top pressure release state, " L " shape pole is direct
Contact ground.
4. suspension bracket according to claim 1, it is characterized in that described power supply is battery, battery is on base.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720081805.2U CN206580464U (en) | 2017-01-22 | 2017-01-22 | Suitable for the suspension bracket of the vertical assembling of Small General Aircraft front open type canopy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720081805.2U CN206580464U (en) | 2017-01-22 | 2017-01-22 | Suitable for the suspension bracket of the vertical assembling of Small General Aircraft front open type canopy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206580464U true CN206580464U (en) | 2017-10-24 |
Family
ID=60110419
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720081805.2U Expired - Fee Related CN206580464U (en) | 2017-01-22 | 2017-01-22 | Suitable for the suspension bracket of the vertical assembling of Small General Aircraft front open type canopy |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206580464U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108100912A (en) * | 2017-12-21 | 2018-06-01 | 合肥市春华起重机械有限公司 | A kind of multifunctional small-size gantry crane |
| CN115202254A (en) * | 2022-07-08 | 2022-10-18 | 江西洪都航空工业集团有限责任公司 | Cabin cover opening and closing control circuit based on direct-current solid-state power controller |
-
2017
- 2017-01-22 CN CN201720081805.2U patent/CN206580464U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108100912A (en) * | 2017-12-21 | 2018-06-01 | 合肥市春华起重机械有限公司 | A kind of multifunctional small-size gantry crane |
| CN115202254A (en) * | 2022-07-08 | 2022-10-18 | 江西洪都航空工业集团有限责任公司 | Cabin cover opening and closing control circuit based on direct-current solid-state power controller |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206580464U (en) | Suitable for the suspension bracket of the vertical assembling of Small General Aircraft front open type canopy | |
| CN206749282U (en) | A kind of device for being used for the two sided mark to square plate | |
| CN202345908U (en) | Wing with movable wing surface | |
| CN203069095U (en) | Automobile front windshield installing position detection device | |
| CN204490330U (en) | The automatic loose bucket tool of vehicle frame | |
| CN205586472U (en) | Multi -functional electronic pole -climbing operation device | |
| CN205738057U (en) | The aircraft wing that a kind of Aero-Space are special | |
| CN206537391U (en) | A kind of installation lowering or hoisting gear of windshield | |
| CN205837167U (en) | A kind of composite integral tank Wing-Body Configurations attachment means | |
| CN205737796U (en) | Location, a kind of skylight lifting apparatus | |
| CN205076755U (en) | Cut deep water drum lift truck of fork | |
| CN106742044A (en) | Small General Aircraft Assembling Production management method | |
| CN204532766U (en) | A kind of Compressor Valve tool specially for attaching and detaching | |
| CN209022095U (en) | A kind of windshield transplanting assembly boosting manipulator | |
| CN102390521A (en) | Airfoil capable of producing standing vortex on surface | |
| CN209143591U (en) | A kind of lifting positioning mechanism | |
| CN206435930U (en) | A kind of engine cylinder cap air valve locking plate press-loading frock | |
| CN207208454U (en) | A kind of leading edge Krueger flap of unmanned plane | |
| CN206745985U (en) | A kind of aeromodelling airplane wing attachment structure | |
| CN106737408A (en) | Auxiliary mould when Automobile air strut is installed | |
| CN206278814U (en) | A kind of construction package for having locking and hoisting function concurrently | |
| CN208935752U (en) | A kind of electric vehicle muffler assembly connection frame | |
| CN206558150U (en) | The digital pipe devices of LED that a kind of suitable open air is used | |
| CN209581846U (en) | A kind of small drone wing rotation auxiliary tool | |
| CN107565434B (en) | A kind of breaker overturning auxiliary device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20171024 Termination date: 20190122 |