CN207791190U - Tripod is fixed on a kind of adjustable ground for space shuttle - Google Patents
Tripod is fixed on a kind of adjustable ground for space shuttle Download PDFInfo
- Publication number
- CN207791190U CN207791190U CN201820146835.1U CN201820146835U CN207791190U CN 207791190 U CN207791190 U CN 207791190U CN 201820146835 U CN201820146835 U CN 201820146835U CN 207791190 U CN207791190 U CN 207791190U
- Authority
- CN
- China
- Prior art keywords
- limit baffle
- mounting base
- fixed
- space shuttle
- tripod
- 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.)
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Abstract
The utility model is related to a kind of adjustable ground for space shuttle to fix tripod, it is fixed on the mounting base (1) on ground, be slidably connected at the left limit baffle (4) of mounting base (1) side and is rotatably arranged on the right limit baffle (9) of mounting base (1) other end, when space shuttle is fixed, the tire of space shuttle is fastened in the limiting slot that left limit baffle (4), mounting base (1) and right limit baffle (9) are formed.Compared with prior art, the utility model fixes tripod with adjustable ground, passes through adjustable design, by way of adjusting, fixed suitable for various sizes of tire, applicability is wider, right limit baffle can put down and lift, and facilitate the positioning of tire and move freely, using simple.
Description
Technical field
The utility model is related to aviation appliance technologies, and in particular to a kind of adjustable ground for space shuttle
Fixed tripod.
Background technology
Aircraft refers to that the power plant with a tool or more tool engines generates the thrust advanced or pulling force, by consolidating for fuselage
Determine wing and generate lift, in the aircraft for overweighting air of endoatmosphere flight.Aircraft is the most common type fixed-wing aviation
Device.The engine type used according to it can be divided into jet airplane and propeller aeroplane again.After aircraft utility model,
Aircraft has become the indispensable vehicles of modern civilization.Its deep change and people’s lives are affected, opened
People conquer blue sky history.
Aircraft usually requires positioning after landing and parks, and when air flowing is larger, is easy to shift in aircraft, original to fly
Machine positioning device is merely able to particular aircraft and proprietary tire positioning device, temporary repair is used such as matched tire cannot to be used fixed
Position equipment, then lead to not timely use.
Utility model content
The purpose of this utility model is exactly to provide a kind of scope of application to overcome the problems of the above-mentioned prior art
Tripod is fixed on the wide adjustable ground for space shuttle.
The purpose of this utility model can be achieved through the following technical solutions：It is a kind of to be used for the adjustable of space shuttle
Tripod is fixed on ground, which includes the mounting base for being fixed on ground, is slidably connected at the left limit gear of mounting base side
Plate and the right limit baffle for being rotatably arranged on the mounting base other end, when space shuttle is fixed, the tire card of space shuttle is set
In the limiting slot that left limit baffle, mounting base and right limit baffle are formed.The utility model passes through left limit baffle
It slides to adjust the width of limiting slot, so as to be suitable for various sizes of aero tyre.
Mounting base one end described in aircraft is equipped with the sliding slot of strip, along track length direction and positioned at sliding slot both sides
Mounting base is equipped with two rows of location holes, and the other end of the mounting base is equipped with accommodating groove, the inner wall both sides of the accommodating groove
Equipped with two pieces of positioning plates, the left limit barrier slides are connected in sliding slot, and the right limit flapper is mounted on accommodating groove
In.
The left limit baffle includes the sliding block of bottom, the block at top and the support that is arranged between sliding block and block
Plate, the sliding block match and are slidably connected in sliding slot with sliding slot, and the support plate is equipped with screw hole.Wherein, the material of sliding block
It is of fine quality to be selected as zinc-plated stainless steel, and reinforcing rib bar can be equipped between block and support plate, increase structural strength.
The distance between the thickness of the right limit baffle and two pieces of positioning plates match, right limit baffle bottom edge
One end is equipped with pin shaft hole, and is rotatablely connected by axis pin and mounting base, and the other end on right limit baffle bottom edge is equipped with limit
Position hole, and be fixedly connected with mounting base by bolt.When limit hole is not fixed by bolt and mounting base, at this point, whole
A right limit baffle is only connect by axis pin with mounting base, so right limit baffle can rotate；When limit hole passes through bolt
When being fixed with mounting base, there are two points to be fixed with mounting base on the bottom edge of right limit baffle, so entire right limit baffle is solid
It is fixed.
The side both sides that pin shaft hole one end is connect are equipped with bottom edge be equipped with limiting plate in the right limit baffle, it is described
The thickness of limiting plate is identical as positioning plate, and limiting plate is equipped with buffer spring.
Left limit baffle and the angle of right limit baffle and mounting base are obtuse angle in the limiting slot.
Compared with prior art, the beneficial effects of the utility model are embodied in：The space shuttle is solid with adjustable ground
Determine tripod, by adjustable design, by way of adjusting, fixed suitable for various sizes of tire, applicability is wider, right
Postive stop baffle can put down and lift, and facilitate the positioning of tire and move freely, using simple.
Description of the drawings
Fig. 1 is the general structure schematic diagram of the utility model；
Fig. 2 is the structural schematic diagram of the utility model mounting base；
Fig. 3 is the structural schematic diagram of the utility model left limit baffle；
Fig. 4 is the structural schematic diagram of the utility model right limit baffle.
Wherein, 1 is mounting base, and 2 be sliding slot, and 3 be location hole, and 4 be left limit baffle, and 5 be support plate, and 6 be sliding block, 7
It is positioning plate for accommodating groove, 8,9 be right limit baffle, and 10 be pin shaft hole, and 11 be limit hole, and 12 be limiting plate, and 13 be buffering elastic
Spring, 14 be handle, and 15 be block, and 16 be reinforcing rib bar, and 17 be limiting slot.
Specific implementation mode
It elaborates below to the embodiments of the present invention, the present embodiment before being with technical solutions of the utility model
It puts and is implemented, give detailed embodiment and specific operating process, but the scope of protection of the utility model is unlimited
In following embodiments.
Embodiment 1
Tripod is fixed on a kind of adjustable ground for space shuttle, which includes the mounting base for being fixed on ground
1, it is slidably connected at the left limit baffle 4 of 1 side of mounting base and is rotatably arranged on the right limit gear of 1 other end of mounting base
Plate 9, when space shuttle is fixed, the tire of space shuttle is fastened on 9 shape of left limit baffle 4, mounting base 1 and right limit baffle
At limiting slot 17 in, as shown in Figure 1.
1 one end of aircraft mounting base is equipped with the sliding slot 2 of strip, along 2 length direction of sliding slot and positioned at 2 both sides of sliding slot
Mounting base 1 is equipped with two rows of location holes 3, and the other end of mounting base 1 is equipped with accommodating groove 7, and the inner wall both sides of accommodating groove 7 are equipped with
Two pieces of positioning plates 8, left limit baffle 4 are slidably connected in sliding slot 2, and right limit baffle 9 is rotatably installed in accommodating groove 7, such as Fig. 2
It is shown.
The sliding block 6 of left limit baffle 4 including bottom, the block 15 at top and it is arranged between sliding block 6 and block 15
Support plate 5, sliding block 6 match and are slidably connected in sliding slot 2 with sliding slot 2, and support plate 5 is equipped with screw hole.Wherein, sliding block 6
Material is preferably zinc-plated stainless steel, and reinforcing rib bar 16 can be equipped between block 15 and support plate 5, increases structural strength, such as Fig. 3
It is shown.
The distance between the thickness of right limit baffle 9 and two pieces of positioning plates 8 match, the one end on 9 bottom edge of right limit baffle
It is rotatablely connected equipped with pin shaft hole 10, and by axis pin and mounting base 1, the other end on 9 bottom edge of right limit baffle is equipped with limit hole
11, and be fixedly connected with mounting base 1 by bolt.When limit hole 11 is not fixed by bolt and mounting base 1, at this point,
Entire right limit baffle 9 is only connect by axis pin with mounting base 1, so right limit baffle 9 can rotate；When limit hole 11 is logical
When crossing bolt with the fixation of mounting base 1, there are two points and mounting base 1 to fix on the bottom edge of right limit baffle 9, so entirely right limit
Position baffle 9 is fixed.The side both sides that 10 one end of pin shaft hole is connect are equipped with bottom edge be equipped with limiting plate in right limit baffle 9
12, the thickness of limiting plate 12 is identical as positioning plate 8, and limiting plate 12 is equipped with buffer spring 13.The top of right limit baffle 9 is set
There is handle 14, as shown in figure 4,
The angle of left limit baffle 4 and right limit baffle 9 and mounting base 1 is obtuse angle in limiting slot 17.
Before use, ground opens up groove, the size for being slightly less than mounting base 1 of groove is circumferential at the upper end-face edge of groove
Shallower side slot is opened up, mounting base 1 is placed on groove so that the edge of mounting base 1 is embedded in the slot of side, and installs bottom
Plate 1 keeps horizontal with ground, by the quadrangle of mounting base 1 by being fixed in the side slot of groove upper end.When aircraft will need
When fixed, the bolt between limit hole 11 and mounting base 1 is removed, under gravity, right limit baffle 9 turns clockwise
It is dynamic so that limiting plate 12 is supported on 8 plate of positioning plate, and buffer spring 13 plays the role of buffering, to limiting plate 12 and installation
In the same plane, the tire of aircraft can enter left limit baffle 4 and right limit baffle 9 from right to left for the upper surface of bottom plate 1
Between, after adjusting position, right limit baffle 9 is lifted by handle 14, and bottom by limit hole 11 and is installed by caging bolt
Plate 1 is fixed, and aero tyre can not move under the action of left limit baffle 4 is with right limit baffle 9.When aircraft tire size compared with
When big or smaller, the bolt in support plate 5 is removed, transverse shifting left limit baffle 4 is adjusted to suitable position by support plate
5 are fixed with mounting base 1 again by positioning bolt.
Claims (6)
1. tripod is fixed on a kind of adjustable ground for space shuttle, which is characterized in that the tripod includes being fixed on ground
Mounting base (1), be slidably connected at the left limit baffle (4) of mounting base (1) side and be rotatably arranged on mounting base
(1) the right limit baffle (9) of the other end, when space shuttle is fixed, the tire of space shuttle is fastened on left limit baffle (4), peace
It fills in the limiting slot (17) that bottom plate (1) and right limit baffle (9) are formed.
2. tripod is fixed on a kind of adjustable ground for space shuttle according to claim 1, which is characterized in that institute
The sliding slot (2) that mounting base (1) one end is equipped with strip is stated, along sliding slot (2) length direction and positioned at the peace of sliding slot (2) both sides
It fills bottom plate (1) and is equipped with two rows of location holes (3), the other end of the mounting base (1) is equipped with accommodating groove (7), the accommodating groove
(7) inner wall both sides are equipped with two pieces of positioning plates (8), and the left limit baffle (4) is slidably connected in sliding slot (2), the right limit
Position baffle (9) is rotatably installed in accommodating groove (7).
3. tripod is fixed on a kind of adjustable ground for space shuttle according to claim 2, which is characterized in that institute
State left limit baffle (4) include the sliding block (6) of bottom, the block (15) at top and setting sliding block (6) and block (15) it
Between support plate (5), the sliding block (6) and sliding slot (2) match and are slidably connected in sliding slot (2), on the support plate (5)
Equipped with screw hole.
4. tripod is fixed on a kind of adjustable ground for space shuttle according to claim 2, which is characterized in that institute
The distance between the thickness of right limit baffle (9) and two pieces of positioning plates (8) is stated to match, right limit baffle (9) bottom edge
One end is equipped with pin shaft hole (10), and is rotatablely connected by axis pin and mounting base (1), right limit baffle (9) bottom edge it is another
One end is equipped with limit hole (11), and is fixedly connected with mounting base (1) by bolt.
5. tripod is fixed on a kind of adjustable ground for space shuttle according to claim 4, which is characterized in that institute
It states in right limit baffle (9) and is equipped with limiting plate (12), institute equipped with the side both sides that pin shaft hole (10) one end is connect with bottom edge
The thickness for stating limiting plate (12) is identical as positioning plate (8), and limiting plate (12) is equipped with buffer spring (13).
6. tripod is fixed on a kind of adjustable ground for space shuttle according to claim 1, which is characterized in that institute
It is obtuse angle to state the angle of left limit baffle (4) and right limit baffle (9) and mounting base (1) in limiting slot (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820146835.1U CN207791190U (en) | 2018-01-29 | 2018-01-29 | Tripod is fixed on a kind of adjustable ground for space shuttle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820146835.1U CN207791190U (en) | 2018-01-29 | 2018-01-29 | Tripod is fixed on a kind of adjustable ground for space shuttle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207791190U true CN207791190U (en) | 2018-08-31 |
Family
ID=63269271
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820146835.1U Expired - Fee Related CN207791190U (en) | 2018-01-29 | 2018-01-29 | Tripod is fixed on a kind of adjustable ground for space shuttle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207791190U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112644740A (en) * | 2020-12-31 | 2021-04-13 | 中国科学院长春光学精密机械与物理研究所 | Locking mechanism of aerospace device |
-
2018
- 2018-01-29 CN CN201820146835.1U patent/CN207791190U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112644740A (en) * | 2020-12-31 | 2021-04-13 | 中国科学院长春光学精密机械与物理研究所 | Locking mechanism of aerospace device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180831 Termination date: 20220129 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |