CN207550473U - For the attachment device and aerostatics in O-E Payload cabin - Google Patents
For the attachment device and aerostatics in O-E Payload cabin Download PDFInfo
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- CN207550473U CN207550473U CN201721661001.6U CN201721661001U CN207550473U CN 207550473 U CN207550473 U CN 207550473U CN 201721661001 U CN201721661001 U CN 201721661001U CN 207550473 U CN207550473 U CN 207550473U
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Abstract
The utility model provides a kind of attachment device and aerostatics for O-E Payload cabin.Attachment device is used to O-E Payload cabin being connected to aerostatics, and attachment device includes：The first flange being connect with O-E Payload cabin；The second flange being connect with the suspension holdfast of aerostatics；Wherein, first flange is equipped with the first fit structure, and second flange is equipped with the second fit structure, and the first fit structure is connect with the second fit structure so that first flange and second flange clamping connection.The technical solution of the utility model is convenient for connection O-E Payload cabin, and efficiency is higher.
Description
Technical field
The utility model is related to attachment device technical field, in particular to a kind of connection for O-E Payload cabin
Device and aerostatics.
Background technology
The problems such as due to the capsule skin machining tolerance of aerostatics or entirety adjustment, ground anchoring system may be caused to be carried with photoelectricity
The linking in lotus cabin occurs hanging, and hanging O-E Payload cabin is advantageously accounted for and the interference of ground anchoring system is asked although such
Topic, but also increase the degree difficult to install in O-E Payload cabin.
Specifically, in the prior art, attachment device is an overall structure, during assembling, is first mounted on attachment device
On the suspension holdfast of aerostatics, then, O-E Payload cabin is installed to attachment device, to realize connection suspension holdfast and photoelectricity
Load cabin purpose, between existing centainly in the horizontal direction and on vertical direction between O-E Payload cabin and attachment device
Every O-E Payload cabin is supported on a certain height by the mode therefore, it is necessary to be assisted using mechanical-assisted or manpower, is then operated
Personnel connect O-E Payload cabin and attachment device.In the prior art, such installation process needs to continue in two or three technician
It could be realized under assisting, it is less efficient, and there is higher risk in installation process, the erectility requirement to technical staff
It is higher.
Utility model content
The main purpose of the utility model is that a kind of attachment device and aerostatics for O-E Payload cabin is provided, with solution
The problem of certainly installation of O-E Payload cabin is inconvenient in the prior art, and efficiency is low.
To achieve these goals, one side according to the present utility model provides a kind of for O-E Payload cabin
Attachment device, attachment device are used to O-E Payload cabin being connected to aerostatics, and attachment device includes：It is connect with O-E Payload cabin
First flange；The second flange being connect with the suspension holdfast of aerostatics；Wherein, first flange is equipped with the first fit structure, the
Two flanges are equipped with the second fit structure, and the first fit structure is connect with the second fit structure so that first flange and second flange
Clamping connection.
Further, first flange includes the first sleeve, and attachment device is additionally included in the first sleeve radially, from first
Sleeve outer wall faces out the clamping protrusion of protrusion setting；Second flange is tubular structure, the second flange of tubular structure it is interior
Wall surface is equipped with the radially extending card slot of radial direction along second flange, wherein, clamping protrusion forms the first fit structure,
Radial direction card slot forms the second fit structure, and radial direction card slot coordinates with clamping protrusion so that first flange connects with second flange clamping
It connects.
Further the internal face of second flange is equipped with the escape groove extended along the radial direction of second flange, second
In the circumferential direction of flange, escape groove is disposed adjacent and communicates with each other with radial direction card slot, and escape groove is clamped protrusion for avoiding.
Further, the quantity for being clamped protrusion and the setting of radial direction card slot is respectively multiple, and multiple clamping protrusions are along the
The circumferential direction of one sleeve is angularly arranged at intervals, and multiple radial direction card slots are angularly arranged at intervals along the internal face of second flange,
Multiple clamping protrusions are respectively clamped into multiple radial direction card slots and form connection.
Further, clamping protrusion includes the first radial protrusion of the outer wall extension protrusion from the first sleeve, radially blocks
Slot includes the first mounting groove set from the internal face of second flange in radial direction perforation, and the first radial protrusion is caught in the first peace
Tankage and the side wall for being connected to the first mounting groove.
Further, clamping protrusion further includes the outer wall extension protrusion from the first sleeve and is connect with the first radial protrusion
The second radial protrusion, radial direction card slot further included from the internal face of second flange recessed the second mounting groove in radial directions,
Second mounting groove connects in the circumferential with the first mounting groove, and the second mounting groove has the radial direction for separating radial direction card slot and escape groove
Wall, the second radial protrusion enter the second mounting groove through the first mounting groove and are connected to radial wall.
Further, clamping protrusion is equipped with along first flange axially through the first pilot hole of setting, radial direction card slot
Bottom wall be equipped with along second flange axially through setting and second pilot hole that is correspondingly arranged with the first pilot hole, locking
Part is also cross the second pilot hole and the first pilot hole and is formed and is threadedly coupled first flange being locked in second flange.
Further, the surface towards O-E Payload cabin of first flange is equipped with multiple first mounting holes, second flange
The surface of the suspension holdfast towards aerostatics be equipped with the second mounting hole, wherein, the first mounting hole is for first flange to be connected
O-E Payload cabin is connected to, the second mounting hole is used to second flange being connected to suspension holdfast.
Further, first flange includes the first sleeve and in the first sleeve close to the side in O-E Payload cabin, and first
The annular flange of the week setting protruding upward of sleeve, the first mounting hole are opened in annular flange.
Other side according to the present utility model, provides a kind of aerostatics, and aerostatics is included filled with buoyance lift gas
Utricule, the suspension holdfast being connect with utricule and the O-E Payload cabin being set to below utricule, further include above-mentioned attachment device,
O-E Payload cabin is connect by attachment device with suspension holdfast.
Using the technical solution of the utility model, first flange is connected to O-E Payload cabin, second flange is connected to
The suspension holdfast of aerostatics, then again by first flange and second flange clamping connection, you can realize and connect O-E Payload cabin
To the purpose of suspension holdfast, the mode for being clamped connection is easy to operation, and an operating personnel can be completed, relative in the prior art
For the mode for needing machinery or personnel's auxiliary connection, program operation site environment demand is low, realizes O-E Payload cabin
The summary of installation, and improve the safety coefficient of installation process.
Description of the drawings
The accompanying drawings which form a part of this application are used to provide a further understanding of the present invention, this practicality
Novel illustrative embodiments and their description do not form the improper restriction to the utility model for explaining the utility model.
In the accompanying drawings：
Fig. 1 shows the first flange of the embodiment of attachment device according to the present utility model and the knot of second flange cooperation
Structure schematic diagram；
Fig. 2 shows the dimensional structure diagrams of the first flange of the attachment device of Fig. 1；
Fig. 3 shows the structure diagram in a direction of the second flange of the attachment device of Fig. 1；And
Fig. 4 shows the dimensional structure diagram of the second flange of the attachment device of Fig. 1.
Wherein, above-mentioned attached drawing is marked including the following drawings：
10th, first flange；11st, the first sleeve；12nd, annular flange；121st, the first mounting hole；13rd, it is clamped protrusion；131、
First radial protrusion；132nd, the second radial protrusion；133rd, the first pilot hole；20th, second flange；21st, the second mounting hole；22nd, diameter
To card slot；221st, the first mounting groove；222nd, the second mounting groove；223rd, the second pilot hole；23rd, escape groove.
Specific embodiment
It should be noted that in the absence of conflict, the feature in embodiment and embodiment in the application can phase
Mutually combination.The utility model will be described in detail below with reference to the accompanying drawings and embodiments.
As shown in Figures 1 to 4, a kind of attachment device for O-E Payload cabin is present embodiments provided, attachment device is used
In O-E Payload cabin is connected to aerostatics, attachment device includes：The first flange 10 being connect with O-E Payload cabin；With aerostatics
Suspension holdfast connection second flange 20；Wherein, first flange 10 is equipped with the first fit structure, and second flange 20 is equipped with
Second fit structure, the first fit structure is connect with the second fit structure so that first flange 10 and the clamping of second flange 20 connect
It connects.
By above-mentioned setting, first flange 10 is connected to O-E Payload cabin, second flange 20 is connected to aerostatics
Then first flange 10 and second flange 20 are clamped connection by suspension holdfast again, you can realize O-E Payload cabin is connected to it is outstanding
The purpose of hanging bracket, the mode for being clamped connection is easy to operation, and an operating personnel can be completed, relative to needing in the prior art
For machinery or personnel assist the mode of connection, program operation site environment demand is low, realizes the installation of O-E Payload cabin
Summary, and improve the safety coefficient of installation process.
Further, attachment device includes the first flange 10 being separately set and second flange 20, in this way, it is only necessary to one
Operating personnel support the O-E Payload cabin for being connected with first flange 10, and first flange 10 and second flange 20 are clamped connection,
Without other operating personnel's continued supports is allowed O-E Payload cabin again, which saves labour, and efficiency is higher.
Specifically, first flange 10 and second flange 20 are flat.After designing in this way, attachment device, photoelectricity carry
The overall height dimension of lotus cabin and suspension holdfast three will not be too high, can draw to avoid the interference of O-E Payload cabin and ground system
The problem of damage O-E Payload cabin risen.Therefore, above-mentioned setting meets the size requirement in the design of floating device assembly, also ensures
Summary and safety in installation process.
As depicted in figs. 1 and 2, in the embodiment of the utility model, first flange 10 includes the first sleeve 11, attachment device
It is additionally included in the first sleeve 11 radially, the clamping protrusion 13 of setting is outwardly protruded from 11 outside wall surface of the first sleeve；Second
Flange 20 is tubular structure, and the internal face of the second flange 20 of tubular structure, which is equipped with along the radial direction of second flange 20, to be extended
Radial direction card slot 22, wherein, clamping protrusion 13 formed the first fit structure, radial direction card slot 22 formed the second fit structure, diameter
Coordinate to card slot 22 with clamping protrusion 13 so that first flange 10 is connected with the clamping of second flange 20.
By above-mentioned setting, clamping protrusion 13 coordinates with radial direction card slot 22, limits first flange 10 in circumferential oneself
By spending, the stability that attachment device circumferentially coordinates ensure that；Meanwhile first sleeve 11 be hollow form cylinder, alleviate the
The weight of one flange 10, realizes the light-weight design of attachment device, saves raw material.
As shown in figure 4, in the embodiment of the utility model, the internal face of second flange 20 is equipped with along second flange 20
The escape groove 23 of radial direction extension, in the circumferential direction of second flange 20, escape groove 23 is disposed adjacent with radial direction card slot 22 and that
This connection, escape groove 23 are clamped protrusion 13 for avoiding.
By above-mentioned setting, first flange 10 is ensure that when coordinating installation with second flange 20, clamping can be protruded
Portion 13 stretches into escape groove 23, by rotating first flange 10 so that and the clamping entrance radial direction of protrusion 13 card slot 22 is simultaneously matched,
Realize the connection of first flange 10 and second flange 20.
As shown in figure 3, in the embodiment of the utility model, it is clamped the quantity difference that protrusion 13 and radial direction card slot 22 are set
To be multiple, multiple clamping protrusions 13 are angularly arranged at intervals along the circumferential direction of the first sleeve 11, and multiple radial direction card slots 22 are along the
The internal face of two flanges 20 is angularly arranged at intervals, and multiple clamping protrusions 13, which are respectively clamped into multiple radial direction card slots 22 and are formed, to be connected
It connects.
Preferably, multiple clamping protrusions 13 are set along the circumferential uniform intervals of the first sleeve 11, multiple radial direction card slots 22
It is set along the internal face uniform intervals of second flange 20.In this way, facilitate processing.Certainly, the replacement not provided in the utility model
In embodiment, multiple clamping protrusions 13 can also be along the even interval setting of circumferential asymmetry of the first sleeve 11 or multiple radial directions
Card slot 22 can not also be set along the internal face uniform intervals of second flange 20.
Preferably, the quantity of clamping protrusion 13 is four, outside wall surface of four clamping protrusions 13 along the first sleeve 11
Uniform intervals are set.
As shown in Figures 2 and 3, in the embodiment of the utility model, clamping protrusion 13 is stepped, and radial direction card slot 22 is
The step slot being adapted with stair-stepping clamping protrusion 13.
By above-mentioned setting, when assembling first flange 10 with second flange 20, clamping protrusion 13 can stablize cooperation
It is set as stepped in radial direction card slot 22, while by clamping protrusion 13, increases the contact area of connecting portion, the company of improving
The bonding strength of connection device.
Third mounting groove is formed between adjacent two clamping protrusions 13 in first flange 10, third mounting groove causes
When rotated, the cell wall of radial direction card slot 22 can rotate in third mounting groove to be passed through first flange 10, will not be to first flange
10 rotation causes to hinder, and ensure that the clamping of first flange 10 and second flange 20 connects.
As shown in Figures 2 and 3, in the embodiment of the utility model, clamping protrusion 13 is further included from the first sleeve 11
The second radial protrusion 132 that outer wall extension is protruded and connect with the first radial protrusion 131, radial direction card slot 22 are further included from the second method
The internal face of orchid 20 recessed the second mounting groove 222 in radial directions, the second mounting groove 222 and the first mounting groove 221 are in week
Connection upwards, the second mounting groove 222 have the radial wall for separating radial direction card slot 22 and escape groove 23, the second radial protrusion 132
Enter the second mounting groove 222 through the first mounting groove 221 and be connected to radial wall.
Specifically, in the present embodiment, the first radial protrusion 131 is more than second in the size radially of the first sleeve 11
For radial protrusion 132 in the size radially of the first sleeve 11, the depth dimensions of the first mounting groove 221 are more than the second mounting groove
222 depth dimensions.When installing this attachment device, after only need to first flange 10 and second flange 20 being carried out simple alignment,
First flange 10 is rotated, the first radial protrusion 131 is made to coordinate with the first mounting groove 221, the second radial protrusion 132 and the second installation
Slot 222 coordinates, and installation process is simple, easy to operate；The design of step structure can prevent rotation install when rotate it is excessive, really
Stair-stepping clamping protrusion 13 is protected with step slot corresponding position to coordinate.
As shown in Figure 3 and Figure 4, in the embodiment of the utility model, the first mounting groove 221 is the radial direction along second flange 20
The through slot of direction perforation setting, after first flange 10 is assembled to second flange 20, the first radial protrusion 131 is inserted into the first peace
To be limited in the circumferential to first flange in tankage 221.
By above-mentioned setting, effectively position of the first flange 10 in second flange 20 is defined, limits
The circumferential free degree of one flange 10, it is ensured that first flange 10 and the stability after the assembling of second flange 20；First radial protrusion
131 are inserted into the first mounting groove 221, increase the contact area of clamping protrusion 13 and radial direction card slot 22, improve connection dress
The bonding strength put, and the degree of freedom of first flange 10 in the circumferential is limited, first flange 10 is prevented out of second flange 20
Abjection.
As shown in Fig. 2, in the embodiment of the utility model, clamping protrusion 13 be equipped with along first flange 10 axially through
First pilot hole 133 of setting, the bottom wall of radial direction card slot 22 be equipped with along second flange 20 axially through setting and with the
The second pilot hole 223 that one pilot hole 133 is correspondingly arranged, locking member is also cross the second pilot hole 223 and the first pilot hole 133
And threaded connection is formed so that first flange 10 is locked in second flange 20.
By above-mentioned setting, first flange 10 and second flange 20 after clamping connection are further locked by locking member,
It further ensures that first flange 10 will not be detached from from second flange 20, ensure that the stability of attachment device, avoid photoelectricity
Load nacelle is fallen, and improves the safety coefficient of attachment device.
Specifically, the first pilot hole 133 and the second pilot hole 223 are through-hole, and locking member is bolt or pin etc..This
The connection mode of sample is simple in structure, easy to operation.
As shown in Fig. 2, in the embodiment of the utility model, the surface towards O-E Payload cabin of first flange 10 is equipped with
Multiple first mounting holes 121, the surface of the suspension holdfast towards aerostatics of second flange 20 are equipped with the second mounting hole 21,
In, the first mounting hole 121 is used to first flange 10 being connected to O-E Payload cabin, and the second mounting hole 21 is used for second flange 20
It is connected to suspension holdfast.
By the connectors such as above-mentioned setting, bolt pass through first flange 10 the first mounting hole 121 after with O-E Payload cabin
Connection, first flange 10 is fixed on O-E Payload cabin；Similarly, the tight lock parts such as bolt are passed through the of second flange 20
It is connect after two mounting holes 21 with the suspension holdfast of aerostatics, so as to which second flange 20 is fixed on suspension holdfast, it is ensured that even
Connection device realize connect before installation process summary, ensure that first flange 10 and O-E Payload cabin, second flange 20 with
The bonding strength of the suspension holdfast of aerostatics is avoided because the suspension holdfast of attachment device and O-E Payload cabin or aerostatics connects
It connects loosening, be detached from the problem of O-E Payload cabin is caused to fall.
As shown in Fig. 2, in the embodiment of the utility model, first flange 10 includes the first sleeve 11 and in first set
Cylinder 11 is close to the side in O-E Payload cabin, the annular flange 12 of the week setting protruding upward of the first sleeve 11, the first mounting hole 121
It is opened in annular flange 12.
Pass through above-mentioned setting so that first flange 10 and the connection in O-E Payload cabin are simple, easy to operate, to staff
Technology requirement it is low, the operating process time is short.
Preferably, annular flange 12 is an integral molding structure with the first sleeve 11, ensure that the intensity of first flange 10, side
Just it processes.
In the embodiment of the present invention, additionally provide a kind of aerostatics, aerostatics include the utricule filled with buoyance lift gas, with
The suspension holdfast of utricule connection and the O-E Payload cabin being set to below utricule, further include above-mentioned attachment device, O-E Payload
Cabin is connect by attachment device with suspension holdfast.
Specifically, the connectors such as bolt are connect after passing through the first mounting hole 121 of first flange 10 with O-E Payload cabin, with
First flange 10 is fixed on O-E Payload cabin；Similarly, the tight lock parts such as bolt are passed through to the second installation of second flange 20
It is connect behind hole 21 with the suspension holdfast of aerostatics, so as to which second flange 20 is fixed on suspension holdfast；Two flanges are fixed
After installing, it is only necessary to a technical staff, hold O-E Payload cabin, by the first flange 10 being fixed on O-E Payload cabin with
After fixed second flange 20 carries out simple alignment on suspension holdfast, rotation is fixed with the O-E Payload cabin of first flange 10, makes
The clamping protrusion 13 and the radial direction card slot 22 of second flange 20 of first flange 10 cooperate, and form phase fit structure；It connects
It, is locked the first pilot hole being clamped on protrusion 13 with the second pilot hole on 22 side wall of radial direction card slot using locking member
Tightly, the connection of O-E Payload nacelle and aerostatics hanger bracket is thus completed using the attachment device of the application.
It can be seen from the above description that the above embodiments of the present invention achieve the following technical effects：Connection
Second flange, by the second mounting hole in second flange, peace is fixed with locking member by the second flange in device with suspension holdfast
On suspension holdfast, the first flange in attachment device, by the first mounting hole in first flange, is used with O-E Payload cabin
First flange is fixedly mounted on O-E Payload cabin by locking member.Two flanges are respectively at aerostatics hanger bracket and O-E Payload cabin
It is connected, connection procedure is easy to operate, and bonding strength is high, and a technical staff is only needed to can be operated completion, and operation technique is simple,
Operating environment is required low.
After two flanges are fixedly mounted, technical staff holds O-E Payload cabin, will be fixed on O-E Payload cabin
After first flange carries out simple alignment with second flange fixed on suspension holdfast, the photoelectricity that rotation is fixed with first flange carries
Lotus cabin makes the clamping protrusion of first flange and the radial direction card slot of second flange cooperate, forms circumferential fit structure.Pass through
First flange and second flange clamping connection realize the summary of O-E Payload cabin installation, make the connection flat in O-E Payload cabin
Graduation avoids in installation process operating personnel and falls because of working at height and waits danger.
Then, using locking member by the second pilot hole on the first pilot hole and the radial direction card slot side wall that are clamped on protrusion
It is locked, completes the connection procedure of first flange and second flange, realize the suspension holdfast and O-E Payload of aerostatics
The connection in cabin.Entire connection procedure greatly reduce lead to operating personnel when hanging and O-E Payload nacelle fall wait it is hidden safely
Suffer from, improve the safety coefficient of installation process, realize the summary of installation process, it is low to the level requirement of technical staff, it is full
The foot design requirement of attachment device flattening, ensure that stability and peace that aerostatics suspension holdfast is connect with O-E Payload cabin
Quan Xing.
The above descriptions are merely preferred embodiments of the present invention, is not intended to limit the utility model, for this
For the technical staff in field, various modifications and changes may be made to the present invention.It is all in the spirit and principles of the utility model
Within, any modification, equivalent replacement, improvement and so on should be included within the scope of protection of this utility model.
Claims (10)
1. a kind of attachment device for O-E Payload cabin, the attachment device is used to the O-E Payload cabin being connected to floating
Device, which is characterized in that the attachment device includes：
The first flange (10) being connect with the O-E Payload cabin；
The second flange (20) being connect with the suspension holdfast of the aerostatics；
Wherein, the first flange (10) is equipped with the first fit structure, and the second flange (20) is equipped with the second cooperation and ties
Structure, first fit structure is connect with second fit structure so that the first flange (10) and the second flange
(20) clamping connection.
2. attachment device according to claim 1, which is characterized in that
The first flange (10) includes the first sleeve (11), and the attachment device is additionally included in the diameter of first sleeve (11)
Upwards, the clamping protrusion (13) of setting is outwardly protruded from the first sleeve (11) outside wall surface；
The second flange (20) is tubular structure, and the internal face of the second flange (20) of tubular structure is equipped with along described
The radially extending card slot of radial direction (22) of second flange (20), wherein, the clamping protrusion (13) forms described first
Fit structure, the radial direction card slot (22) form second fit structure, and the radial direction card slot (22) is protruded with the clamping
Portion (13) coordinates so that the first flange (10) is connected with the second flange (20) clamping.
3. attachment device according to claim 2, which is characterized in that the internal face of the second flange (20) is equipped with edge
The escape groove (23) of the radial direction extension of the second flange (20), it is described to keep away in the circumferential direction of the second flange (20)
Slot (23) is allowed to be disposed adjacent and communicate with each other with the radial direction card slot (22), the escape groove (23) is convex for avoiding the clamping
Go out portion (13).
4. attachment device according to claim 2, which is characterized in that the clamping protrusion (13) and the radial direction card slot
(22) setting quantity it is respectively multiple, it is multiple it is described clamping protrusions (13) along first sleeve (11) circumferential direction angularly
Ground is arranged at intervals, and multiple radial direction card slots (22) are angularly arranged at intervals along the internal face of the second flange (20), more
A clamping protrusion (13) is respectively clamped into multiple radial direction card slots (22) and forms connection.
5. attachment device according to claim 3, which is characterized in that the clamping protrusion (13) is including from described first
The first radial protrusion (131) of the outer wall extension protrusion of sleeve (11), the radial direction card slot (22) is including from the second flange
(20) the first mounting groove (221) that internal face is set in radial direction perforation, first radial protrusion (131) are caught in described
First mounting groove (221) and the side wall for being connected to first mounting groove (221).
6. attachment device according to claim 5, which is characterized in that the clamping protrusion (13) is further included from described the
The outer wall extension protrusion of one sleeve (11) and the second radial protrusion (132) being connect with first radial protrusion (131), it is described
Radial direction card slot (22) is further included from the internal face of the second flange (20) recessed the second mounting groove in radial directions
(222), second mounting groove (222) connects in the circumferential with first mounting groove (221), second mounting groove
(222) there is the radial wall for separating the radial direction card slot (22) and the escape groove (23), second radial protrusion (132)
Enter second mounting groove (222) through first mounting groove (221) and be connected to the radial wall.
7. attachment device according to claim 3, which is characterized in that the clamping protrusion (13) is equipped with along described the
Axially through the first pilot hole (133) of setting, the bottom wall of the radial direction card slot (22) is equipped with along described the one flange (10)
Two flanges (20) axially through setting and the second pilot hole (223) for being correspondingly arranged with first pilot hole (133), lock
Tight part is threadedly coupled also cross second pilot hole (223) and first pilot hole (133) and being formed with by described the
One flange (10) is locked in the second flange (20).
8. attachment device according to any one of claim 1 to 7, which is characterized in that the court of the first flange (10)
Multiple first mounting holes (121), the direction aerostatics of the second flange (20) are equipped with to the surface in O-E Payload cabin
The surface of suspension holdfast be equipped with the second mounting hole (21), wherein, first mounting hole (121) is for by first method
Blue (10) are connected to the O-E Payload cabin, and second mounting hole (21) is described for the second flange (20) to be connected to
Suspension holdfast.
9. attachment device according to claim 8, which is characterized in that the first flange (10) includes the first sleeve
(11) and in first sleeve (11) close to the side in the O-E Payload cabin, in the circumferential direction of first sleeve (11)
The annular flange (12) of setting is protruded above, first mounting hole (121) is opened in the annular flange (12).
10. a kind of aerostatics, the suspension holdfast that the aerostatics includes the utricule filled with buoyance lift gas, connect with the utricule
And it is set to the O-E Payload cabin below the utricule, which is characterized in that further include as described in any one of claim 1 to 9
Attachment device, the O-E Payload cabin is connect by the attachment device with the suspension holdfast.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721661001.6U CN207550473U (en) | 2017-12-01 | 2017-12-01 | For the attachment device and aerostatics in O-E Payload cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721661001.6U CN207550473U (en) | 2017-12-01 | 2017-12-01 | For the attachment device and aerostatics in O-E Payload cabin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207550473U true CN207550473U (en) | 2018-06-29 |
Family
ID=62677166
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721661001.6U Active CN207550473U (en) | 2017-12-01 | 2017-12-01 | For the attachment device and aerostatics in O-E Payload cabin |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207550473U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108713567A (en) * | 2018-08-07 | 2018-10-30 | 小熊电器股份有限公司 | A kind of dough mixing machine |
-
2017
- 2017-12-01 CN CN201721661001.6U patent/CN207550473U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108713567A (en) * | 2018-08-07 | 2018-10-30 | 小熊电器股份有限公司 | A kind of dough mixing machine |
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