CN205109036U - All -wing aircraft model aircraft jettison device - Google Patents
All -wing aircraft model aircraft jettison device Download PDFInfo
- Publication number
- CN205109036U CN205109036U CN201520737273.4U CN201520737273U CN205109036U CN 205109036 U CN205109036 U CN 205109036U CN 201520737273 U CN201520737273 U CN 201520737273U CN 205109036 U CN205109036 U CN 205109036U
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- CN
- China
- Prior art keywords
- model
- stretch cord
- slide groove
- cell body
- aircraft
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- Expired - Fee Related
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Abstract
The utility model discloses an all -wing aircraft model aircraft jettison device, include: launch the handle, two slide groove bodies that the preceding end connection that launches the handle has tilt up to set up, the left and right sides of the preceding tip of every slide groove body all is provided with a guide pulley, is provided with the cable loop in the below of slide groove body trailing edge, is connected with the stretch cord on the cable loop, the slipping into of stretch cord in the guide pulley, the other end of stretch cord is arranged the trailing edge of the slide groove body in and is connected with model aircraft, is provided with electromagnetic switch at slide groove on physically, is provided with electric battery, switch and the automatic re -setting key of being connected with electromagnetic switch in launching the handle. The utility model discloses use the stretch cord as power, including the design of slide groove body end friction resistance, with fixed knot the about the synchronous release of electromagnetic switch, but launch pulling force freedom adjustment to the demand that cooperates different weight organisms to take off is solved and is flown the difficulty that the wing structure organism took off, removes the possibility of screw injury health when taking off simultaneously from, guarantees more that the aircraft horizontality goes up to the air.
Description
Technical field
The utility model relates to model field, is specifically related to a kind of all-wing aircraft model of an airplane catapult-launching gear.
Background technology
Design is found in practice by the model flight controller of specialty, the body of flying wing structure due to machine bottom surface be even surface, be not easy to the firm body of hand-held, simultaneously hand dish out body time, After-Body screw is easy to damage tractor driver, body ten thousand is likely made level not dish out when staff throws body simultaneously, so that operating difficulties, easy aircraft bombing.
Summary of the invention
The purpose of this utility model is to provide a kind of all-wing aircraft model of an airplane catapult-launching gear.
According to one side of the present utility model, provide a kind of all-wing aircraft model of an airplane catapult-launching gear, comprise: firing trigger, the leading section of described firing trigger is connected with two the slideway cell bodies being inclined upwardly and arranging, the left and right sides of the leading section of every bar slideway cell body is provided with a guide wheel, the below of described slideway cell body trailing edge is provided with sling, described sling is connected with stretch cord, described stretch cord slip in described guide wheel, the trailing edge that the other end of described stretch cord is placed in slideway cell body is connected with the model of an airplane, described slideway cell body is provided with electromagnetic switch, the battery be electrically connected with electromagnetic switch is provided with in described firing trigger, power switch and the key that automatically resets.
Further, the angle between described slideway cell body and firing trigger is 20 °.
Further, described slideway cell body is the cell body that aluminum material is made.
Further, also comprise tripod, the upper end of described tripod is connected with described firing trigger.
The beneficial effects of the utility model are: the utility model uses conventional stretch cord to be power, add the design of frictional resistance at the bottom of slideway cell body, with electromagnetic switch synchronous release left and right clip, launch pulling force can freely adjust, with the demand coordinating Different Weight body to take off, solve the difficulty that flying wing structure body takes off, remove the possibility of propeller injury health when taking off simultaneously from, more ensure the lift-off of aircraft level.
Accompanying drawing explanation
Fig. 1 is a kind of structural representation of all-wing aircraft model of an airplane catapult-launching gear.
Fig. 2 is the schematic diagram of assembling tripod.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in further detail.
Fig. 1 to Fig. 2 show schematically show according to a kind of all-wing aircraft model of an airplane catapult-launching gear of the present utility model.
A kind of all-wing aircraft model of an airplane catapult-launching gear that the present embodiment provides, refer to Fig. 1 to Fig. 2, comprise: firing trigger 001, the leading section of described firing trigger 001 is connected with two the slideway cell bodies 002 being inclined upwardly and arranging, the cell body that described slideway cell body 002 is made for aluminum material, angle specifically between slideway cell body 002 and firing trigger 001 is the elevation angle of 20 °, the left and right sides of the leading section of every bar slideway cell body 002 is provided with a guide wheel 003, the below of described slideway cell body 002 trailing edge is provided with sling 004, described sling 004 is connected with stretch cord 005, described stretch cord 005 slip in described guide wheel 003, the trailing edge that the other end of described stretch cord 005 is placed in slideway cell body 002 is connected with the model of an airplane, described slideway cell body 002 is provided with electromagnetic switch 006, the battery (not shown) be electrically connected with electromagnetic switch 006 is provided with in described firing trigger 001, power switch 007 and the key 008 that automatically resets, in addition tripod 009 is also comprised in the present embodiment, the upper end of described tripod 009 is connected with described firing trigger 001, tripod 009 freely can adjust height, in the present embodiment, all parts are dismountable structure, be convenient for carrying.
Workflow of the present utility model is: be connected with slideway cell body 002 below the body that need launch, again two guide wheels 003 of one end of stretch cord 005 through slideway cell body 002 front end to be moved to below body and to be connected with body, the other end of rope stretch cord 005 is connected with the sling 004 be provided with below slideway cell body 002, so produce forward pulling force at the process elastic force rope stretched 005 pair of body, in the same design of slideway cell body about 002, when body moves aluminium groove rear end to, with two electricity hereby switch fix body and do not skid off track, use parallel way connect two electricity hereby switch to power supply, handle is equipped with switch, when making it switch on power electricity hereby switch move down, body nature coordination ejects.
The beneficial effects of the utility model are: the utility model uses conventional stretch cord 005 to be power, add the design of slideway cell body 002 end frictional resistance, with electromagnetic switch 006 synchronous release left and right clip, launch pulling force can freely adjust, with the demand coordinating Different Weight body to take off, solve the difficulty that flying wing structure body takes off, remove the possibility of propeller injury health when taking off simultaneously from, more ensure the lift-off of aircraft level.
Finally should be noted that; above embodiment is only in order to illustrate the technical solution of the utility model; but not the restriction to the utility model protection domain; although done to explain to the utility model with reference to preferred embodiment; those of ordinary skill in the art is to be understood that; can modify to the technical solution of the utility model or equivalent replacement, and not depart from essence and the scope of technical solutions of the utility model.
Claims (4)
1. an all-wing aircraft model of an airplane catapult-launching gear, it is characterized in that, comprise: firing trigger, the leading section of described firing trigger is connected with two the slideway cell bodies being inclined upwardly and arranging, the left and right sides of the leading section of every bar slideway cell body is provided with a guide wheel, the below of described slideway cell body trailing edge is provided with sling, described sling is connected with stretch cord, described stretch cord slip in described guide wheel, the trailing edge that the other end of described stretch cord is placed in slideway cell body is connected with the model of an airplane, described slideway cell body is provided with electromagnetic switch, the battery be electrically connected with electromagnetic switch is provided with in described firing trigger, power switch and the key that automatically resets.
2. all-wing aircraft model of an airplane catapult-launching gear according to claim 1, is characterized in that, the angle between described slideway cell body and firing trigger is 20 °.
3. all-wing aircraft model of an airplane catapult-launching gear according to claim 1, is characterized in that, described slideway cell body is the cell body that aluminum material is made.
4. all-wing aircraft model of an airplane catapult-launching gear according to claim 1, is characterized in that, also comprise tripod, and the upper end of described tripod is connected with described firing trigger.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520737273.4U CN205109036U (en) | 2015-09-22 | 2015-09-22 | All -wing aircraft model aircraft jettison device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520737273.4U CN205109036U (en) | 2015-09-22 | 2015-09-22 | All -wing aircraft model aircraft jettison device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205109036U true CN205109036U (en) | 2016-03-30 |
Family
ID=55564685
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520737273.4U Expired - Fee Related CN205109036U (en) | 2015-09-22 | 2015-09-22 | All -wing aircraft model aircraft jettison device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205109036U (en) |
-
2015
- 2015-09-22 CN CN201520737273.4U patent/CN205109036U/en not_active Expired - Fee Related
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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: 20160330 Termination date: 20210922 |