CN207579919U - A kind of light airplane wing using collaborative optimization tooling - Google Patents
A kind of light airplane wing using collaborative optimization tooling Download PDFInfo
- Publication number
- CN207579919U CN207579919U CN201721636017.1U CN201721636017U CN207579919U CN 207579919 U CN207579919 U CN 207579919U CN 201721636017 U CN201721636017 U CN 201721636017U CN 207579919 U CN207579919 U CN 207579919U
- Authority
- CN
- China
- Prior art keywords
- strut
- pedestal
- credit
- fixed
- supporting rod
- 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.)
- Active
Links
Landscapes
- Toys (AREA)
Abstract
A kind of light airplane wing using collaborative optimization tooling, include the pedestal of rectangle frame rack-like, pedestal is left, right both sides are fixedly arranged in the middle of strut of drawing money on credit, the both ends of mandril are separately fixed at the strut upper end of drawing money on credit of pedestal both sides, it draws money on credit before strut, afterwards short supporting rod is fixed on the pedestal of both sides, one end of ox-hide band is fixed on the upper end of short supporting rod, the other end is fixed on the upper end for strut of drawing money on credit, the bottom end of the ox-hide band is distributed in the downside of short supporting rod, it draws money on credit the upper end of the strut and upper end of short supporting rod is respectively fixed with the first secure latch and second safety lock is buckled, one end hanging buckle of safety rope is on the first secure latch, the other end hanging buckle of safety rope is buckled in second safety lock；The Corner Strapped of pedestal is connected with wheel.It is simple in structure, and stability is good, and positioning security is good, storing, move and partly assembling convenient for light airplane wing using collaborative optimization.
Description
Technical field：
The utility model is related to the technical field of light aerocraft manufacturing equipment, more specifically to a kind of light aerocraft machine
Wing tooling.
Background technology：
Light-duty sport plane refers to maximum take-off weight and is less than 600 kilograms of aircraft, light aerocraft have it is light, safely, make
With require it is low, can be in meadow landing, easily operated, cheap advantage, due to its small volume, construction is relatively easy, by
Gradually it is applied to leisure and business travel.With the exploitation of novel synthetic material, the shell of light airplane wing using collaborative optimization is firmer, light
Ingeniously so that flight energy consumption and stability, the safety all highers of light aerocraft.The shell of light airplane wing using collaborative optimization is by polylith metal plate
What part was spliced, during wing storage, assembling and carrying, need accordingly to place the jig of wing, but existing control
Lamps structure is complicated, and stability is poor, it is difficult to meet the positioning needs of safety.
Utility model content：
The purpose of the utility model is to solve the deficiencies of the prior art, and provides a kind of light airplane wing using collaborative optimization tooling,
It is simple in structure, storing, move and partly assembling convenient for light airplane wing using collaborative optimization.
The technology solution of the utility model is as follows：
A kind of light airplane wing using collaborative optimization tooling, includes the pedestal of rectangle frame rack-like, and pedestal arranged on left and right sides is fixedly arranged in the middle of length
Supporting rod, the both ends of mandril are separately fixed at the strut upper end of drawing money on credit of pedestal both sides, consolidate on the pedestal of strut front and rear sides of drawing money on credit
Surely there is a short supporting rod, one end of ox-hide band is fixed on the upper end of short supporting rod, the other end is fixed on the upper end of strut of drawing money on credit, described
The bottom end of ox-hide band is distributed in the downside of short supporting rod, and the upper end of the upper end for strut of drawing money on credit and short supporting rod is respectively fixed with first
Secure latch and second safety lock button, on the first secure latch, the other end hanging buckle of safety rope exists one end hanging buckle of safety rope
Second safety lock is buckled；The Corner Strapped of pedestal is connected with wheel.
Preferably, the strut of drawing money on credit of the pedestal both sides is equipped with two, the inclined distribution of strut of drawing money on credit, pedestal homonymy
The top of two root long supporting rods is fixed together.
Preferably, the length of the ox-hide band is more than the spacing drawn money on credit between strut upper end and short post upper.
Preferably, the both ends of the safety rope are fixed with hook, and the hook at safety rope both ends is buckled respectively in the first safety
Lock and second safety lock are buckled.
The beneficial effects of the utility model are：
It is simple in structure, and stability is good, and positioning security is good, convenient for the storing of light airplane wing using collaborative optimization, moves and part group
Dress.
Description of the drawings：
Fig. 1 is the structure diagram of the utility model.
In figure：1st, pedestal；2nd, it draws money on credit strut；3rd, short supporting rod；4th, mandril；5th, ox-hide band；6th, the first secure latch；7th,
Two secure latch；8th, safety rope；9th, wheel.
Specific embodiment：
Embodiment：As shown in Figure 1, a kind of light airplane wing using collaborative optimization tooling, the pedestal 1 including rectangle frame rack-like, 1 left side of pedestal,
Right both sides are fixedly arranged in the middle of strut 2 of drawing money on credit, and the both ends of mandril 4 are separately fixed at 2 upper end of strut of drawing money on credit of 1 both sides of pedestal, long
Be fixed with short supporting rod 3 on the pedestal 1 of 2 front and rear sides of supporting rod, one end of ox-hide band 5 be fixed on the upper end of short supporting rod 3,
The other end is fixed on the upper end for strut 2 of drawing money on credit, and the bottom end of the ox-hide band 5 is distributed in the downside of short supporting rod 3, strut 2 of drawing money on credit
Upper end and the upper end of short supporting rod 3 be respectively fixed with the first secure latch 6 and second safety lock button 7, one end of safety rope 8 is hung
It is buckled on the first secure latch 6, the other end hanging buckle of safety rope 8 is on second safety lock button 7；The Corner Strapped of pedestal 1 has company
It is connected to wheel 9, the universal guide wheel that wheel 9 is depressurized using buffering.
Preferably, the strut 2 of drawing money on credit of 1 both sides of pedestal is equipped with two, 2 inclined distribution of strut of drawing money on credit, and pedestal 1 is same
The top of two root long supporting rods 2 of side is fixed together.
Preferably, the length of the ox-hide band 5 is more than the spacing between 3 upper end of 2 upper end of strut and short supporting rod of drawing money on credit.
Preferably, the both ends of the safety rope 8 are fixed with hook, and the hook at 8 both ends of safety rope is buckled respectively in the first peace
On full lock 6 and second safety lock button 7.
Operation principle：The utility model is the tooling of light airplane wing using collaborative optimization, and light airplane wing using collaborative optimization is placed in ox by use
On belt 5, ox-hide band can play the role of buffering, and wing is protected to prevent from damaging, while can fix safety rope 8, safety
Rope 8 can prevent wing dropping and fall.
The embodiment rather than limits the present invention the utility model is illustrated.Any this field
Technical staff can modify, therefore this practicality to the embodiment under the spirit and scope without prejudice to the utility model
Novel rights protection scope, should be as listed by the claim of the utility model.
Claims (4)
1. a kind of light airplane wing using collaborative optimization tooling, the pedestal (1) including rectangle frame rack-like, it is characterised in that：Pedestal (1) left and right two
Side is fixedly arranged in the middle of strut of drawing money on credit (2), and the both ends of mandril (4) are separately fixed on the strut of drawing money on credit (2) of pedestal (1) both sides
It holds, is fixed with short supporting rod (3) on the pedestal (1) of strut of drawing money on credit (2) front and rear sides, one end of ox-hide band (5) is fixed on short branch
The upper end of strut (3), the other end are fixed on the upper end of strut of drawing money on credit (2), and the bottom end of the ox-hide band (5) is distributed in short supporting rod
(3) downside, the upper end of strut of drawing money on credit (2) and the upper end of short supporting rod (3) are respectively fixed with the first secure latch (6) and second
Secure latch (7), one end hanging buckle of safety rope (8) is on the first secure latch (6), and the other end hanging buckle of safety rope (8) is
On two secure latch (7)；The Corner Strapped of pedestal (1) is connected with wheel (9).
2. a kind of light airplane wing using collaborative optimization tooling according to claim 1, it is characterised in that：The length of pedestal (1) both sides
Supporting rod (2) is equipped with two, strut of drawing money on credit (2) inclined distribution, the top of the two root long supporting rods (2) of pedestal (1) homonymy
It is fixed together.
3. a kind of light airplane wing using collaborative optimization tooling according to claim 1, it is characterised in that：The length of the ox-hide band (5)
More than the spacing between strut of drawing money on credit (2) upper end and short supporting rod (3) upper end.
4. a kind of light airplane wing using collaborative optimization tooling according to claim 1, it is characterised in that：The both ends of the safety rope (8)
Hook is fixed with, the hook at safety rope (8) both ends is buckled respectively on the first secure latch (6) and second safety lock button (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721636017.1U CN207579919U (en) | 2017-11-30 | 2017-11-30 | A kind of light airplane wing using collaborative optimization tooling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721636017.1U CN207579919U (en) | 2017-11-30 | 2017-11-30 | A kind of light airplane wing using collaborative optimization tooling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207579919U true CN207579919U (en) | 2018-07-06 |
Family
ID=62734436
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721636017.1U Active CN207579919U (en) | 2017-11-30 | 2017-11-30 | A kind of light airplane wing using collaborative optimization tooling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207579919U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111137341A (en) * | 2019-12-30 | 2020-05-12 | 四川航泰航空装备有限公司 | Integrated unmanned aerial vehicle wing bracket for assembling, unloading and transporting |
-
2017
- 2017-11-30 CN CN201721636017.1U patent/CN207579919U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111137341A (en) * | 2019-12-30 | 2020-05-12 | 四川航泰航空装备有限公司 | Integrated unmanned aerial vehicle wing bracket for assembling, unloading and transporting |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207579919U (en) | A kind of light airplane wing using collaborative optimization tooling | |
| CN205451617U (en) | Catapult | |
| CN203079483U (en) | Crash-resisting elevator carriage | |
| CN205455454U (en) | Portable fishing cage | |
| CN203073360U (en) | Hauling notebook computer bag | |
| CN202077749U (en) | Light draw-bar box | |
| CN209225205U (en) | For loading and unloading the Portable handcart of winding wheel | |
| CN204250107U (en) | A kind of fortune bar car | |
| CN206172440U (en) | Liftable a device for delivery of reel material | |
| CN206624612U (en) | A kind of construction high-altitude hanging basket | |
| CN207417369U (en) | A kind of takeaway box | |
| CN203187336U (en) | Large blue printing machine | |
| CN212047852U (en) | Unmanned aerial vehicle horn beta structure | |
| CN219278400U (en) | Container with protective structure | |
| CN204333756U (en) | A kind of earth connection special high-altitude knapsack | |
| CN204173875U (en) | A kind of fork truck loads the auxiliary mould of glass casing | |
| CN204341130U (en) | There is the field operations Multifunction tow shrinking pull bar | |
| CN204452697U (en) | Ride mountain region bicycle back seat baggages in a kind of open air | |
| CN211223832U (en) | Composite material telescopic airstairs | |
| CN207174630U (en) | A kind of device of artificial transporting flat plate component | |
| CN203187209U (en) | Lead transporting and paying-off truck | |
| CN202449201U (en) | Bag structure for hot air aerostat | |
| CN213950323U (en) | Railway freight container lifting appliance | |
| CN208069726U (en) | A kind of easy tape roll transport device | |
| CN206813339U (en) | A kind of unmanned plane flies hand protection mechanism |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190722 Address after: 312500 No. 1 Aofeng Road, Xinchang Industrial Park, Xinchang County, Shaoxing City, Zhejiang Province Patentee after: Wanfeng Aircraft Industry Co., Ltd. Address before: 312500 No. 1 Aofeng Road, Xinchang Industrial Park, Xinchang County, Shaoxing City, Zhejiang Province Patentee before: Wanfeng Aviation Industry Co Ltd |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220223 Address after: 312500 No.1-3 (building 1-5), Aofeng Road, Wozhou Town, Xinchang County, Shaoxing City, Zhejiang Province Patentee after: Zhejiang Wanfeng Aircraft Manufacturing Co.,Ltd. Address before: 312500 No.1 Aofeng Road, Xinchang Industrial Park, Xinchang County, Shaoxing City, Zhejiang Province Patentee before: Wanfeng Aircraft Industry Co.,Ltd. |
|
| TR01 | Transfer of patent right |