CN208641747U - A kind of model plane empennage Quick Release connection structure - Google Patents
A kind of model plane empennage Quick Release connection structure Download PDFInfo
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- CN208641747U CN208641747U CN201821129485.4U CN201821129485U CN208641747U CN 208641747 U CN208641747 U CN 208641747U CN 201821129485 U CN201821129485 U CN 201821129485U CN 208641747 U CN208641747 U CN 208641747U
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- quick release
- empennage
- mounting groove
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- steering engine
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Abstract
The utility model relates to a kind of model plane empennage Quick Release connection structures, it includes Quick Release pedestal, Quick Release connector, steering engine and rotation connection component, one side of the Quick Release pedestal far from fuselage successively offers the first mounting groove and the second mounting groove along its length, steering engine is installed in the first mounting groove, Quick Release connector is installed in the second mounting groove, the upper and lower surface of Quick Release connector is respectively equipped with several positioning guide runners, the cell wall of second mounting groove is equipped with and the positioning one-to-one positioning convex strip of guide runner, being rotatablely connected component includes hinged-support and shaft seat, orthogonal two sides are respectively equipped with protruding shaft and hinged ear on shaft seat, the output end of steering engine is fixedly connected with one end of pull rod, waist hole is offered on pull rod, protruding shaft is caught in waist hole, hinged ear is hinged with hinged-support, steering engine can drive shaft seat and rudder face to rotate by pull rod.Advantage is, reasonable in design, can effectively realize Quick Release；The setting of steering engine position rationally, is conducive to be promoted stability when model plane flight.
Description
Technical field
The utility model belongs to aeromodelling aerocraft field, and in particular to a kind of model plane empennage Quick Release connection structure.
Background technique
General aircraft model is as manned aircraft, mainly by wing, empennage, fuselage, undercarriage, engine and control
System composition.Common model plane are again different from common manned aircraft or agricultural military unmanned air vehicle, in order to guarantee that fuselage is light, lead to
It is often made of a foam material, simultaneously because model plane easily fall collision, therefore for the ease of damaging the replacement of component, between each component
Usually using removable connection.Empennage is an important parts of model plane, and the swingable rudder face being arranged thereon can control aircraft flight
Direction.The shortcoming of existing model plane empennage has the following: disassembly and assembly structure design is unreasonable, does not consider to design auxiliary installation
Location structure and stress dismounting structure when auxiliary disassembly, therefore be not easy to fast assembling-disassembling；The mounting design of steering engine is unreasonable, existing
Some steering engines are generally disposed at the middle part of empennage to drive rudder face to rotate, for by compared with the light and relatively small foamed material of intensity
For manufactured empennage, middle part installs rudder face inconvenience fixation and dismounting and increases empennage weight.
Utility model content
The utility model provides a kind of model plane empennage Quick Release connection structure, it is intended to overcome model plane tail structure in the prior art
Design it is unreasonable caused by can not fast assembling-disassembling, steering engine installation site it is improper caused by difficult to install and empennage overall weight increase
The deficiencies of adding.
The technical solution that the utility model solves above-mentioned technical problem is as follows: a kind of model plane empennage Quick Release connection structure,
Including Quick Release pedestal, Quick Release connector, steering engine and rotation connection component, the one side of the Quick Release pedestal far from fuselage is along length
Direction successively offers the first mounting groove and the second mounting groove, and the steering engine is installed in first mounting groove, the Quick Release
Connector is installed in second mounting groove, if the one side of the Quick Release connector towards the second mounting groove slot bottom is equipped with
Dry buckle, the slot bottom of second mounting groove are equipped with the one-to-one blocked hole of several and described buckle, the Quick Release connector
Towards the U-shaped bayonet of empennage offered on one side for connecting empennage, if the upper and lower surface of the Quick Release connector is respectively equipped with
Dry positioning guide runner, the cell wall of second mounting groove are equipped with several and one-to-one convex of the positioning guide runner
Item, the rotation connection component include the hinged-support for connecting with empennage and the shaft seat for connecting with rudder face, and described turn
Orthogonal two sides are respectively equipped with protruding shaft and hinged ear on axle bed, and the output end of the steering engine and one end of pull rod are fixed
It connecting, offers waist hole on the pull rod, the protruding shaft is caught in the waist hole, and the hinged ear and the hinged-support are hinged,
The steering engine can drive rudder face to rotate by the pull rod and the shaft seat.
Based on the above technical solution, the utility model can also do following improvement.
Further, the Quick Release connector upper and lower surface is provided with turning up for auxiliary dismounting close to the side of the empennage
Side.
Beneficial effect using above-mentioned further scheme is that the flanging of setting auxiliary dismounting, height is slightly exceeding tail
The upper surface of the wing and Quick Release pedestal, bottle opener or block, then can be corresponding by it from flanging described in a side impaction when disassembly
It is removed from empennage or out of Quick Release pedestal the second mounting groove, when disassembly is more convenient.
Further, the shaft seat is equipped with the trapezoidal card slot for being clamped with one jiao of rudder face close to the side of the rudder face.
Beneficial effect using above-mentioned further scheme is to be clamped by a right angle of trapezoidal card slot and rudder face, benefit
It is replaceable after damage to be easy to disassemble.
Further, the hinged-support is equipped with close to the side of the empennage for the ladder link block with one jiao of the empennage
The stepped groove of clamping.
Beneficial effect using above-mentioned further scheme is connected by stepped groove ladder link block corresponding with one jiao of empennage
It connects, fixation and easy disassembly replacement.
Further, the steering engine two sides are equipped with lug, and the lug is equipped with through-hole, be equipped in the through-hole with it is described fast
Tear the screw of whorl of base connection open.
Beneficial effect using above-mentioned further scheme is the screw connected on the lug and lug that steering engine passes through two sides
It is connect with Quick Release pedestal, it is convenient for disassembly and assembly and firm.
Further, the side that the fast dismounting bottom seats against nearly fuselage is equipped with the groove for wrapping up the corresponding interconnecting piece of fuselage.
Beneficial effect using above-mentioned further scheme is that Quick Release pedestal is provided with the groove of package Fuselage connection, can
Bonding or interference fit, it is easy for installation.
Further, the Quick Release pedestal, Quick Release connector, hinged-support and shaft seat are made of rigid plastics.
Beneficial effect using above-mentioned further scheme is, small using density different from fuselage and empennage and intensity is slightly worse
Foam, connector because to carry relatively large power or attachment screw etc., therefore rigid plastics should be used, it is preferable to use polyethylene,
Polycarbonate or polypropylene.
Compared with prior art, the utility model has the beneficial effects that
It can effectively realize that the Quick Release of empennage and fuselage is connect with the cooperation of Quick Release connector by Quick Release pedestal, Quick Release connects
The positioning convex strip positioned on guide runner and Quick Release pedestal on fitting corresponds, and can guarantee quick location and installation during installation, fastly
Tear open on connector be provided with auxiliary disassembly flanging, by flanging apply active force can easily by Quick Release connector from
It is removed on empennage and/or Quick Release pedestal, i.e., the utility model is reasonable in design, can effectively realize Quick Release；Quick Release connector
Upper connection steering engine is located at one end of empennage and rudder face, and the middle part connection in Non-traditional Techniques, on the one hand saves in empennage
The trouble of steering engine fixed structure is arranged in middle part, does not on the other hand also increase the weight of empennage itself, is conducive to promote model plane flight
When stability.
Detailed description of the invention
Fig. 1 is a kind of explosive view of model plane empennage Quick Release connection structure provided by the utility model；
Fig. 2 is the structure after model plane empennage Quick Release connection structure side provided by the utility model and empennage and rudder face assembling
Schematic diagram；
Fig. 3 is the amplified schematic diagram of Quick Release connector in Fig. 1；
Fig. 4 is the amplified schematic diagram of shaft seat in Fig. 1.
In attached drawing, parts list represented by the reference numerals are as follows:
1. Quick Release pedestal；2. Quick Release connector；3. steering engine；4. hinged-support；5. shaft seat；20. buckle；21. positioning slide guide
Slot；22. flanging；23.U shape bayonet；50. protruding shaft；51. hinged ear；52. trapezoidal card slot.
Specific embodiment
The principles of the present invention and feature are described below in conjunction with attached drawing, example is served only for explaining that this is practical
It is novel, it is not intended to limit the scope of the utility model.
As shown in Figures 1 to 4, the utility model provides a kind of model plane empennage Quick Release connection structure comprising Quick Release pedestal 1,
Quick Release connector 2, steering engine 3 and rotation connection component, the one side of the Quick Release pedestal 1 far from fuselage are successively opened along its length
Equipped with the first mounting groove and the second mounting groove, the steering engine 3 is installed in first mounting groove, and the Quick Release connector 2 is pacified
Loaded in second mounting groove, the one side of the Quick Release connector 2 towards the second mounting groove slot bottom is equipped with several buckles
20, the slot bottom of second mounting groove is equipped with several and 20 one-to-one blocked holes of the buckle, 2 court of Quick Release connector
To the U-shaped bayonet 23 of empennage offered on one side for connecting empennage, if the upper and lower surface of the Quick Release connector 2 is respectively equipped with
Dry positioning guide runner 21, the cell wall of second mounting groove are equipped with several and described positioning correspondingly of positioning guide runner 21
Raised line, the rotation connection component includes the hinged-support 4 for connecting with empennage and the shaft seat for connecting with rudder face 5, institute
It states orthogonal two sides on shaft seat 5 and is respectively equipped with protruding shaft 50 and hinged ear 51, the output end and pull rod of the steering engine 3
One end be fixedly connected, waist hole is offered on the pull rod, the protruding shaft 50 is caught in the waist hole, the hinged ear 51 and institute
It is hinged to state hinged-support 4, the steering engine 3 can drive rudder face to rotate by the pull rod and the shaft seat 5.
It should be noted that the connection of Quick Release connector and Quick Release pedestal is interference fit, that is, it is clamped, Quick Release connector
The connection of U-shaped bayonet and empennage is also interference fit, stronger in order to be clamped, the second peace of U-shaped bayonet inner wall and Quick Release pedestal
Settable anti-skid chequer on the cell wall of tankage.
Further, 2 upper and lower surface of Quick Release connector is provided with turning up for auxiliary dismounting close to the side of the empennage
Side 22.
It should be noted that the surface 1-2mm for being higher by its neighbouring stabilizing surfaces and Quick Release pedestal of flanging, so as to fast
It is hit when tearing open from tools such as side bottle openers and applies active force.
Further, the shaft seat 5 is equipped with the trapezoidal card slot for being clamped with one jiao of rudder face close to the side of the rudder face
52。
Further, the hinged-support 4 is equipped with close to the side of the empennage for connecting with one jiao of the empennage of ladder
The stepped groove of block clamping.
Further, 3 two sides of steering engine are equipped with lug, and the lug is equipped with through-hole, be equipped in the through-hole with it is described
The screw that Quick Release pedestal 1 is threadedly coupled.
It should be noted that steering engine is in the first mounting groove or clamping, but because it is electrical components, when work
Have vibration and stress be more complex, thus in order to guarantee its can stable operation, consider two sides install additional lug and with screw by its
It is fixed in the first mounting groove.
Further, the Quick Release pedestal 1 is equipped with the groove for wrapping up the corresponding interconnecting piece of fuselage close to the side of fuselage.
Further, the Quick Release pedestal 1, Quick Release connector 2, hinged-support 4 and shaft seat 5 are made of rigid plastics.
The above is only the preferred embodiment of the present invention, is not intended to limit the utility model, all practical at this
Within novel spirit and principle, any modification, equivalent replacement, improvement and so on should be included in the guarantor of the utility model
Within the scope of shield.
Claims (7)
1. a kind of model plane empennage Quick Release connection structure, which is characterized in that including Quick Release pedestal (1), Quick Release connector (2), steering engine
(3) and rotation connection component, the Quick Release pedestal (1) successively offer the first installation far from the one side of fuselage along its length
Slot and the second mounting groove, the steering engine (3) are installed in first mounting groove, and the Quick Release connector (2) is installed on described
In second mounting groove, the one side of the Quick Release connector (2) towards the second mounting groove slot bottom is equipped with several buckles (20), institute
The slot bottom for stating the second mounting groove is equipped with several and described buckle (20) one-to-one blocked hole, Quick Release connector (2) court
To the U-shaped bayonet (23) of empennage offered on one side for connecting empennage, the upper and lower surface of the Quick Release connector (2) is set respectively
There are several positioning guide runners (21), the cell wall of second mounting groove is equipped with several a pair of with the positioning guide runner (21) one
The positioning convex strip answered, the rotation connection component include hinged-support (4) for connecting with empennage and for connecting with rudder face
Shaft seat (5), upper orthogonal two sides of shaft seat (5) are respectively equipped with protruding shaft (50) and hinged ear (51), described
The output end of steering engine (3) is fixedly connected with one end of pull rod, and waist hole is offered on the pull rod, and the protruding shaft (50) is caught in described
In waist hole, hingedly, the steering engine (3) passes through the pull rod and the shaft seat for the hinged ear (51) and the hinged-support (4)
(5) the rudder face rotation is driven.
2. a kind of model plane empennage Quick Release connection structure according to claim 1, which is characterized in that the Quick Release connector
(2) upper and lower surface is provided with the flanging (22) of auxiliary dismounting close to the side of the empennage.
3. a kind of model plane empennage Quick Release connection structure according to claim 1, which is characterized in that the shaft seat (5) is leaned on
The side of the nearly rudder face is equipped with the trapezoidal card slot (52) for being clamped with one jiao of rudder face.
4. a kind of model plane empennage Quick Release connection structure according to claim 1, which is characterized in that the hinged-support (4) is leaned on
The side of the nearly empennage is equipped with the stepped groove for the ladder link block clamping with one jiao of the empennage.
5. a kind of model plane empennage Quick Release connection structure according to any one of claims 1 to 4, which is characterized in that the rudder
Machine (3) two sides are equipped with lug, and the lug is equipped with through-hole, is equipped in the through-hole and is threadedly coupled with the Quick Release pedestal (1)
Screw.
6. a kind of model plane empennage Quick Release connection structure according to any one of claims 1 to 4, which is characterized in that described fast
Pedestal (1) is torn open close to the side of fuselage equipped with the groove for wrapping up the corresponding interconnecting piece of fuselage.
7. a kind of model plane empennage Quick Release connection structure according to any one of claims 1 to 4, which is characterized in that described fast
Pedestal (1), Quick Release connector (2), hinged-support (4) and shaft seat (5) is torn open to be made of rigid plastics.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821129485.4U CN208641747U (en) | 2018-07-17 | 2018-07-17 | A kind of model plane empennage Quick Release connection structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821129485.4U CN208641747U (en) | 2018-07-17 | 2018-07-17 | A kind of model plane empennage Quick Release connection structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208641747U true CN208641747U (en) | 2019-03-26 |
Family
ID=65784641
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821129485.4U Active CN208641747U (en) | 2018-07-17 | 2018-07-17 | A kind of model plane empennage Quick Release connection structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208641747U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112278240A (en) * | 2020-11-06 | 2021-01-29 | 湖南浩天翼航空技术有限公司 | Small-sized fixed wing unmanned aerial vehicle empennage quick dismounting mechanism and using method thereof |
-
2018
- 2018-07-17 CN CN201821129485.4U patent/CN208641747U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112278240A (en) * | 2020-11-06 | 2021-01-29 | 湖南浩天翼航空技术有限公司 | Small-sized fixed wing unmanned aerial vehicle empennage quick dismounting mechanism and using method thereof |
| CN112278240B (en) * | 2020-11-06 | 2021-12-28 | 湖南浩天翼航空技术有限公司 | Small-sized fixed wing unmanned aerial vehicle empennage quick dismounting mechanism and using method thereof |
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