CN107381322A - A kind of satellite fairing assembly hanging basket - Google Patents
A kind of satellite fairing assembly hanging basket Download PDFInfo
- Publication number
- CN107381322A CN107381322A CN201710557263.6A CN201710557263A CN107381322A CN 107381322 A CN107381322 A CN 107381322A CN 201710557263 A CN201710557263 A CN 201710557263A CN 107381322 A CN107381322 A CN 107381322A
- Authority
- CN
- China
- Prior art keywords
- semi
- ring frame
- abutted flange
- hanger
- hanging basket
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
- B66C1/00—Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles
- B66C1/10—Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles by mechanical means
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Load-Engaging Elements For Cranes (AREA)
Abstract
The present invention relates to a kind of satellite fairing assembly hanging basket, including the first half baskets that are oppositely arranged and are symmetric and the second half baskets, the first half baskets include semi-ring frame on concentric first time semi-ring frame and first, and semi-ring frame is fixedly connected by circumferentially spaced multiple first tie-beams on first time semi-ring frame and first；The second half baskets include semi-ring frame on concentric second time semi-ring frame and second, and semi-ring frame is fixedly connected by circumferentially spaced multiple second tie-beams on second time semi-ring frame and second；It is equipped with the carrying beam assembly for connecting satellite fairing assembly on first time semi-ring frame and second time semi-ring frame, hanger is equipped with semi-ring frame on semi-ring frame and second on first.It has the advantages of simple in construction, easy to use, adjustment is convenient, connection is reliable, practical, and the fast and reliable connection with satellite fairing assembly can be achieved, and improves the stability and security of lifting.
Description
Technical field
The present invention relates to a kind of suspender, and in particular to a kind of hanging basket for being used to lift satellite fairing assembly, belongs to and defends
Star lift-off technology field.
Background technology
In space industry, assembling of the satellite at launching site usually requires to be lifted.For satellite fairing assembly
Speech, because shape of product is special, is relatively large in diameter, and tie point is more, and the operation convenience and connection reliability to suspender all carry
More strict requirements are gone out.Existing suspender often reaches above-mentioned requirement, is mainly manifested in cumbersome, adjustment not
Just it is unreliable etc., to connect, and can not ensure the stability and security of the lifting of satellite fairing assembly.
The content of the invention
It is an object of the invention to provide a kind of satellite fairing assembly hanging basket, and it has simple in construction, easy to use, tune
The advantages of whole convenient, connection is reliable, practical, the fast and reliable connection with satellite fairing assembly can be achieved, improve
The stability and security of lifting.
To solve suspender of the prior art its existing cumbersome, adjustment inconvenience, connection is insecure states problem, this
A kind of satellite fairing assembly hanging basket provided is provided, including the first half baskets that are oppositely arranged and are symmetric and the second half
Basket, the first half basket include semi-ring frame on concentric first time semi-ring frame and first, semi-ring on first time semi-ring frame and first
Frame is fixedly connected by circumferentially spaced multiple first tie-beams；The second half basket includes second time concentric semi-ring
Semi-ring frame on frame and second, semi-ring frame passes through circumferentially spaced multiple second tie-beams on second time semi-ring frame and second
It is fixedly connected；The carrying for connecting satellite fairing assembly is equipped with first time semi-ring frame and second time semi-ring frame
Beam assembly, hanger is equipped with semi-ring frame on semi-ring frame and second on described first.
Further, a kind of satellite fairing assembly hanging basket of the present invention, wherein, the upper and lower side of the first half basket both sides
Be correspondingly provided with the first abutted flange and the second abutted flange, the upper and lower sides of the second half basket both sides be correspondingly provided with the 3rd abutted flange and
4th abutted flange；When the first half baskets and the second half basket docking, first abutted flange and the second abutted flange are corresponding with the
Three abutted flanges and the 4th abutted flange are fixedly connected by connecting bolt.
Further, a kind of satellite fairing assembly hanging basket of the present invention, wherein, first abutted flange and the 3rd pair
Offer the first horizontal locating slot and the second vertical locating slot on the interface of acting flange, first locating slot and the
Two locating slots are semi-cylindrical, right in the first abutted flange or the first locating slot and the second locating slot on the 3rd abutted flange
The first locating dowel and the second locating dowel should be embedded with.
Further, a kind of satellite fairing assembly hanging basket of the present invention, wherein, second abutted flange and the 4th pair
Offer the 3rd horizontal locating slot and the 4th vertical locating slot on the interface of acting flange, the 3rd locating slot and the
Four locating slots are semi-cylindrical, right in the second abutted flange or the 3rd locating slot and the 4th locating slot on the 4th abutted flange
The 3rd locating dowel and the 4th locating dowel should be embedded with.
Further, a kind of satellite fairing assembly hanging basket of the present invention, wherein, the carrying beam assembly is held including first
Carrier beam component and the second carrying beam assembly, the first carrying beam assembly include the first installation set, the first carrier bar, first wedge
Iron, the first end cap and the first tight fixed bolt, first installation set are provided with the first through hole comprising a sloped sidewall and make it solid
Due in the first mounting hole that first time semi-ring frame or second time semi-ring frame open up, the first carrier bar from the first installation set first
Passed through in through hole, the first drift is placed between the first carrier bar and the sloped sidewall of first through hole, and the first end cap is fixed on first
In installation set and the first carrier bar is set to be stretched out from the first end cap, the first tight fixed bolt spinning covers in first end and makes itself and first
Drift is relative；The second carrying beam assembly includes the second installation set, two the second carrier bars, two the second drifts, the second ends
Lid and two the second tight fixed bolts, second installation set are provided with two the second through holes comprising a sloped sidewall and fix it
In the second mounting hole that first time semi-ring frame or second time semi-ring frame open up, two the second carrier bars are corresponding from the second installation set
Two the second through holes in pass through, two the second drifts are correspondingly placed in inclination of two the second carrier bars with corresponding second through hole
Between side wall, the second end cap is fixed in the second installation set and two the second carrier bars is stretched out from the second end cap, two second
Tight fixed bolt spinning is on the second end cap and makes it corresponding relative with two the second drifts.
Further, a kind of satellite fairing assembly hanging basket of the present invention, wherein, under first time semi-ring frame and second
The first carrying beam assembly and the second carrying beam assembly on semi-ring frame are respectively provided with two, and make first on both to carry beam assembly
It is symmetric with the second carrying beam assembly.
Further, a kind of satellite fairing assembly hanging basket of the present invention, wherein, the hanger includes the first hanger and the
Two hangers, the first hanger on first on semi-ring frame and second on semi-ring frame are respectively provided with three and make the first hanger on both be in
It is symmetrical；The second hanger on first on semi-ring frame and second on semi-ring frame is respectively provided with two and makes the second hanger on both
It is symmetric；Wherein, the first hanger hangs the first half baskets and the second half baskets for sky, and the second hanger is used to lift by crane hanging basket and satellite
Radome fairing assembly.
Further, a kind of satellite fairing assembly hanging basket of the present invention, wherein, on described first on semi-ring frame and second
The auxiliary connecting hole for connecting satellite fairing assembly is additionally provided with semi-ring frame, aids in that auxiliary connection is installed in connecting hole
Bolt.
Further, a kind of satellite fairing assembly hanging basket of the present invention, wherein, on described first on semi-ring frame and second
The upper auxiliary connecting hole of semi-ring frame is respectively provided with four and the both sides for making auxiliary connecting hole correspondingly be distributed in the second hanger.
A kind of satellite fairing assembly hanging basket of the present invention compared with prior art, has advantages below：The present invention passes through
Relative distribution is set and in symmetrical the first half basket and the second half baskets, allows the first half baskets to include first time concentric semi-ring frame and the
Semi-ring frame on one, and semi-ring frame on first time semi-ring frame and first is consolidated by circumferentially spaced multiple first tie-beams
Fixed connection；Allow the second half baskets to include semi-ring frame on concentric second time semi-ring frame and second, and make second time semi-ring frame and second
Upper semi-ring frame is fixedly connected by circumferentially spaced multiple second tie-beams, and in first time semi-ring frame and the second lower half
The carrying beam assembly for connecting satellite fairing assembly is respectively provided with ring frame, the semi-ring frame on semi-ring frame and second on first
On be respectively provided with hanger.Thus just constitute it is a kind of it is simple in construction, easy to use, adjustment is convenient, the reliable satellite fairing of connection
Assembly hanging basket.In actual applications, the first half baskets and the second half baskets are sling respectively first, are allowed under first time semi-ring frame and second
Carrying beam assembly on semi-ring frame is connected with satellite fairing assembly respectively, then allows the first half baskets and the second half basket connections again
It is fixed, satellite fairing assembly can be hung finally by the hanger on semi-ring frame on semi-ring frame and second on first
Dress.The present invention is advantageous to adjustment tie point position by allowing hanging basket to use to include the split-type structural of the first half baskets and the second half baskets
Put, improve the convenience of attended operation, and by allowing satellite fairing to be in hanging basket, ensure that the stability and peace of lifting
Quan Xing.
Shown embodiment is made further to a kind of satellite fairing assembly hanging basket of the present invention below in conjunction with the accompanying drawings
Describe in detail：
Brief description of the drawings
Fig. 1 is a kind of top view of satellite fairing assembly hanging basket of the present invention；
Fig. 2 is a kind of front view of satellite fairing assembly hanging basket of the present invention；
Fig. 3 be Fig. 2 in A to partial enlarged view；
Fig. 4 is B-B direction view in Fig. 3；
Fig. 5 is that location of C faces enlarged drawing in Fig. 2；
Fig. 6 is E-E direction views in Fig. 5；
Fig. 7 is that enlarged drawing is faced in D positions in Fig. 2；
Fig. 8 is F-F direction views in Fig. 7；
Fig. 9 is a kind of lifting view of satellite fairing assembly hanging basket of the present invention.
Embodiment
Firstly the need of explanation, the noun of locality such as heretofore described front, back, left, right, up, down simply enters with reference to the accompanying drawings
Capable description, in order to understand, not to technical scheme and be claimed scope progress limitation.
The embodiment of a kind of satellite fairing assembly hanging basket of the invention as shown in Figures 1 to 9, including set relatively
The first half baskets 1 putting and be symmetric and the second half baskets 2.The first half baskets 1 specifically include first time concentric He of semi-ring frame 11
Semi-ring frame 12 on first, allow on first time semi-ring frame 11 and first semi-ring frame 12 to pass through circumferentially spaced multiple first and connect
Beam 13 is connect to be fixedly connected.The second half baskets 2 specifically include semi-ring frame 22 on concentric second time semi-ring frame 21 and second, allow under second
Semi-ring frame 21 is fixedly connected with semi-ring frame 22 on second by circumferentially spaced multiple second tie-beams 23.Meanwhile
The carrying beam assembly for connecting satellite fairing assembly is respectively provided with first time semi-ring frame 11 and second time semi-ring frame 21,
On first hanger is respectively provided with semi-ring frame 12 and second on semi-ring frame 22.A kind of structure letter is just constituted by above structure setting
Satellite fairing assembly hanging basket single, easy to use, adjustment is convenient, connection is reliable, safe, practical.In reality
In, the first half baskets 1 and the second half baskets 2 are sling respectively first, allow on first time semi-ring frame 11 and second time semi-ring frame 21
Carrying beam assembly is connected with satellite fairing assembly respectively, then allows the first half baskets 1 and the second half baskets 2 to be connected again, most
Satellite fairing assembly can be lifted by the hanger on semi-ring frame 22 on semi-ring frame 12 and second on first afterwards.This
Invention is advantageous to adjustment tie point position by allowing hanging basket to use to include the split-type structural of the first half baskets 1 and the second half baskets 2,
The convenience of attended operation is improved, and by allowing satellite fairing to be in hanging basket, ensure that the stability and safety of lifting
Property.
As embodiment, upper and lower side of the present invention in the first half both sides of basket 1 has been correspondingly arranged the first abutted flange
14 and second abutted flange 15, the upper and lower side in the second half both sides of basket 2 has been correspondingly arranged the 3rd abutted flange 24 and the 4th docking
Flange 25.When the first half baskets 1 and the second half baskets 2 dock, make the first abutted flange 14 and the second abutted flange 15 corresponding with the 3rd
Abutted flange 24 is fixedly connected with the 4th abutted flange 25 by connecting bolt.
As prioritization scheme, present embodiment is on the interface of the first abutted flange 14 and the 3rd abutted flange 24
The first horizontal locating slot and the second vertical locating slot are provided with, allows the first locating slot and the second locating slot to use semicircle
Cylindricality, and be correspondingly embedded in the first locating slot and the second locating slot on the first abutted flange 14 or the 3rd abutted flange 24
First locating dowel 3 and the second locating dowel 4.This structure setting, it is fixed by first when the first half baskets 1 and the second half baskets 2 dock
The position locating dowel 4 of post 3 and second and its corresponding first locating slot and the second locating slot, can be achieved fast positioning, and determine because of first
The position locating dowel 4 of post 3 and second relation vertical each other, ensure that the degree of accuracy of positioning.Similarly, present embodiment is second
The 3rd horizontal locating slot and the vertical the 4th positioning are provided with the interface of the abutted flange 25 of abutted flange 15 and the 4th
Groove, the 3rd locating slot and the 4th locating slot is allowed to use semi-cylindrical, and in the second abutted flange 15 or the 4th abutted flange 25
On the 3rd locating slot and the 4th locating slot in be correspondingly embedded the 3rd locating dowel 5 and the 4th locating dowel 6, it is fixed to further increase
The convenience of position and the degree of accuracy.
As further prioritization scheme, present embodiment allows carrying beam assembly to include the first carrying beam assembly 7 and the
Two carrying beam assemblies 8, and allow the first carrying beam assembly 7 and the second carrying beam assembly 8 to use two kinds of different structure types.Its
In, the first carrying beam assembly 7 specifically includes the first installation set 71, the first carrier bar 72, the first drift 73, the first end cap 74 and the
One tight fixed bolt 75.Allow the first installation set 71 that the first through hole comprising a sloped sidewall is set and be secured to first time semi-ring
In the first mounting hole that frame 11 or second time semi-ring frame 21 open up, the first carrier bar 72 is allowed from the first through hole of the first installation set 71
In pass through, allow the first drift 73 to be arranged between the first carrier bar 72 and the sloped sidewall of first through hole, make the first end cap 74 solid
It is scheduled in the first installation set 71 and the first carrier bar 72 is stretched out from the first end cap 74, allows the spinning of the first tight fixed bolt 75 first
On end cap 74 and make it relative with the first drift 73.The second carrying beam assembly 8 is allowed to specifically include the second installation set 81, two second
82, two the second drifts 83 of carrier bar, the second end cap 84 and two the second tight fixed bolts 85, allow the second installation set 81 to set and include
Two the second through holes of one sloped sidewall are simultaneously secured to first time semi-ring frame 11 or second time semi-ring frame 21 open up second
In mounting hole, allow two the second carrier bars 82 are corresponding to be passed through from two the second through holes of the second installation set 81, allow two second
Drift 83 is correspondingly arranged between two the second carrier bars 82 and the sloped sidewall of corresponding second through hole, makes the second end cap 84 solid
It is scheduled in the second installation set 81 and two the second carrier bars 82 is stretched out from the second end cap 84, allows two the second tight fixed bolts 85 to revolve
On the second end cap 84 and make it corresponding relative with two the second drifts 83.The present invention is held by two kinds of structure types of setting
Carrier beam component, allow the first carrying beam assembly 7 that first carrier bar 72 is set, allow the second carrying beam assembly 8 to set two second
Carrier bar 82, and by setting link bolt hole and connecting bolt in the first carrier bar 72 and the second carrier bar 82 respectively, can fit
Multiple tie points on satellite fairing assembly are answered, ensure that connection, the steadiness of lifting and security.And whole with satellite
During flowing the connection of cover assembly, the first carrier bar can be made by unscrewing the first tight fixed bolt 75 and the second tight fixed bolt 85
72 and second carrier bar 82 move radially, and by screwing the corresponding top pressure of the first tight fixed bolt 75 and the second tight fixed bolt 85 the
One drift 73 and the second drift 83 can be achieved to fix the purpose of the first carrier bar 72 and the second carrier bar 82, have adjustment just
The advantages of victory, positioning precision, reliable connection, effectively increase connection, the convenient, flexible property and operating efficiency of lifting.
As embodiment, the present invention is by allowing first on first time semi-ring frame 11 and second time semi-ring frame 21 to hold
Carrier beam component 7 and second carries beam assembly 8 and is respectively provided with two, and makes first on both to carry the carrier bar of beam assembly 7 and second
Component 8 is symmetric, and connection, the stationarity of lifting and stress equalization has been effectively ensured.Meanwhile the present invention allows hanger to set
First hanger 91 and the second hanger 92, and allow the first hanger 91 and the second hanger 92 to use different structure type.And make
The first hanger 91 on one on semi-ring frame 12 and second on semi-ring frame 22 is respectively provided with three and makes the first hanger 91 on both be in
It is symmetrical.The second hanger 92 on first on semi-ring frame 12 and second on semi-ring frame 22 is allowed to be respectively provided with two and make on both
Second hanger 92 is symmetric.Wherein, the first hanger 91 hangs the first half baskets 1 and the second half baskets 2 for sky, and the second hanger 92 is used
In lifting hanging basket and satellite fairing assembly.
Present embodiment is provided with also on first on semi-ring frame 12 and second on semi-ring frame 22 to be used to connect satellite
The auxiliary connecting hole of radome fairing assembly, and auxiliary connecting bolt is mounted with connecting hole is aided in, by aiding in connecting bolt
It is connected with satellite fairing assembly, can further improve the stability and security of connection and lifting.In actual applications, originally
Invention generally allows semi-ring frame 12 on first to be respectively provided with four with the upper auxiliary connecting hole of semi-ring frame 22 on second and connect auxiliary
Hole is correspondingly distributed in the both sides of the second hanger 92, and this structure is ensureing on first the intensity of semi-ring frame 22 on semi-ring frame 12 and second
While, the steadiness of connection and the harmony of stress can be improved, practicality is stronger.
Above example is only the description carried out to the preferred embodiment of the present invention, and model not is claimed to the present invention
Enclose and be defined, on the premise of design spirit of the present invention is not departed from, technology of this area engineers and technicians according to the present invention
The various forms of deformations that scheme is made, it all should fall into the protection domain of claims of the present invention determination.
Claims (9)
1. a kind of satellite fairing assembly hanging basket, it is characterised in that including the first half baskets for being oppositely arranged and being symmetric
(1) and the second half baskets (2), the first half basket (1) includes semi-ring frame (12) on concentric first time semi-ring frame (11) and first,
Semi-ring frame (12) is fixed by circumferentially spaced multiple first tie-beams (13) on first time semi-ring frame (11) and first
Connection；The second half basket (2) includes semi-ring frame (22) on concentric second time semi-ring frame (21) and second, second time semi-ring frame
(21) it is fixedly connected with semi-ring frame (22) on second by circumferentially spaced multiple second tie-beams (23)；Described first
The carrying beam assembly for connecting satellite fairing assembly, institute are equipped with lower semi-ring frame (11) and second time semi-ring frame (21)
State and be equipped with hanger on semi-ring frame (22) on semi-ring frame (12) and second on first.
2. according to a kind of satellite fairing assembly hanging basket described in claim 1, it is characterised in that the first half basket (1)
The upper and lower side of both sides is correspondingly provided with the first abutted flange (14) and the second abutted flange (15), the second half basket (2) both sides up and down
End is correspondingly provided with the 3rd abutted flange (24) and the 4th abutted flange (25)；When the first half baskets (1) and the second half basket (2) docking,
First abutted flange (14) and the second abutted flange (15) correspond to and the 3rd abutted flange (24) and the 4th abutted flange
(25) it is fixedly connected by connecting bolt.
3. according to a kind of satellite fairing assembly hanging basket described in claim 2, it is characterised in that first abutted flange
(14) the first horizontal locating slot and the second vertical locating slot, institute and on the interface of the 3rd abutted flange (24) are offered
State the first locating slot and the second locating slot is semi-cylindrical, on the first abutted flange (14) or the 3rd abutted flange (24)
The first locating dowel (3) and the second locating dowel (4) are correspondingly embedded with one locating slot and the second locating slot.
4. according to a kind of satellite fairing assembly hanging basket described in claim 3, it is characterised in that second abutted flange
(15) the 3rd horizontal locating slot and the 4th vertical locating slot, institute and on the interface of the 4th abutted flange (25) are offered
It is semi-cylindrical to state the 3rd locating slot and the 4th locating slot, and on the second abutted flange (15) or the 4th abutted flange (25)
The 3rd locating dowel (5) and the 4th locating dowel (6) are correspondingly embedded with three locating slots and the 4th locating slot.
5. according to a kind of satellite fairing assembly hanging basket described in claim 4, it is characterised in that the carrying beam assembly bag
The first carrying beam assembly (7) and the second carrying beam assembly (8) are included, the first carrying beam assembly (7) includes the first installation set
(71), the first carrier bar (72), the first drift (73), the first end cap (74) and the first tight fixed bolt (75), first installation
Set (71) is provided with the first through hole comprising a sloped sidewall and is secured to first time semi-ring frame (11) or second time semi-ring frame
(21) in the first mounting hole opened up, the first carrier bar (72) passes through from the first through hole of the first installation set (71), first wedge
Iron (73) is placed in the first carrier bar (72) between the sloped sidewall of first through hole, and the first end cap (74) is fixed on the first installation set
(71) on and the first carrier bar (72) is made to be stretched out from the first end cap (74), the first tight fixed bolt (75) spinning is in the first end cap (74)
Above and make it relative with the first drift (73)；The second carrying beam assembly (8) include the second installation set (81), two second hold
Carrier beam (82), two the second drifts (83), the second end cap (84) and two the second tight fixed bolts (85), second installation set
(81) two the second through holes comprising a sloped sidewall are provided with and are secured to first time semi-ring frame (11) or second time semi-ring
In the second mounting hole that frame (21) opens up, two corresponding two the second through holes from the second installation set (81) of the second carrier bar (82)
In pass through, two the second drifts (83) are corresponding be placed in two the second carrier bars (82) and corresponding second through hole sloped sidewall it
Between, the second end cap (84) is fixed in the second installation set (81) and two the second carrier bars (82) is stretched from the second end cap (84)
Go out, two the second tight fixed bolt (85) spinnings are on the second end cap (84) and it is corresponded to two the second drifts (83) relatively.
6. according to a kind of satellite fairing assembly hanging basket described in claim 5, it is characterised in that first time semi-ring frame
(11) the first carrying beam assembly (7) and the second carrying beam assembly (8) and on second time semi-ring frame (21) are respectively provided with two, and make
The first carrying beam assembly (7) and the second carrying beam assembly (8) on both are symmetric.
7. according to a kind of satellite fairing assembly hanging basket described in claim 6, it is characterised in that the hanger includes first
Hanger (91) and the second hanger (92), the first hanger (91) on first on semi-ring frame (12) and second on semi-ring frame (22) are all provided with
Put three and be symmetric the first hanger (91) on both；On first on semi-ring frame (12) and second on semi-ring frame (22)
The second hanger (92) be respectively provided with two and be symmetric the second hanger (92) on both；Wherein, the first hanger (91)
The first half baskets (1) and the second half baskets (2) are hung for sky, the second hanger (92) is used to lift by crane hanging basket and satellite fairing assembly.
8. according to a kind of satellite fairing assembly hanging basket described in claim 7, it is characterised in that semi-ring frame on described first
(12) the auxiliary connecting hole for connecting satellite fairing assembly is additionally provided with and on second on semi-ring frame (22), aids in connecting hole
In auxiliary connecting bolt is installed.
9. according to a kind of satellite fairing assembly hanging basket described in claim 8, it is characterised in that semi-ring frame on described first
(12) four are respectively provided with the upper auxiliary connecting hole of semi-ring frame (22) on second and makes auxiliary connecting hole is corresponding to be distributed in second and hang
The both sides of ear (92).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710557263.6A CN107381322A (en) | 2017-07-10 | 2017-07-10 | A kind of satellite fairing assembly hanging basket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710557263.6A CN107381322A (en) | 2017-07-10 | 2017-07-10 | A kind of satellite fairing assembly hanging basket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107381322A true CN107381322A (en) | 2017-11-24 |
Family
ID=60333884
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710557263.6A Pending CN107381322A (en) | 2017-07-10 | 2017-07-10 | A kind of satellite fairing assembly hanging basket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107381322A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3459406A (en) * | 1967-09-25 | 1969-08-05 | Harmonic Reed Corp | Dome hoist |
| CN102849612A (en) * | 2012-03-31 | 2013-01-02 | 航天东方红卫星有限公司 | Multi-function combination lifting device for minisatellite |
| CN103030061A (en) * | 2012-12-28 | 2013-04-10 | 北京空间飞行器总体设计部 | Circular ring lifting tool based on satellite bearing cylinder lifting |
| CN103062538A (en) * | 2012-10-01 | 2013-04-24 | 徐州支点机电设备有限公司 | Flange with locating function |
| CN203638954U (en) * | 2013-11-04 | 2014-06-11 | 北京航天发射技术研究所 | Hanger for vertically hoisting fairing |
| CN104266856B (en) * | 2014-09-23 | 2016-08-31 | 北京强度环境研究所 | Two grades of band cover free boundaries and radome fairing built-in boundary implementation in vibration tower |
-
2017
- 2017-07-10 CN CN201710557263.6A patent/CN107381322A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3459406A (en) * | 1967-09-25 | 1969-08-05 | Harmonic Reed Corp | Dome hoist |
| CN102849612A (en) * | 2012-03-31 | 2013-01-02 | 航天东方红卫星有限公司 | Multi-function combination lifting device for minisatellite |
| CN103062538A (en) * | 2012-10-01 | 2013-04-24 | 徐州支点机电设备有限公司 | Flange with locating function |
| CN103030061A (en) * | 2012-12-28 | 2013-04-10 | 北京空间飞行器总体设计部 | Circular ring lifting tool based on satellite bearing cylinder lifting |
| CN203638954U (en) * | 2013-11-04 | 2014-06-11 | 北京航天发射技术研究所 | Hanger for vertically hoisting fairing |
| CN104266856B (en) * | 2014-09-23 | 2016-08-31 | 北京强度环境研究所 | Two grades of band cover free boundaries and radome fairing built-in boundary implementation in vibration tower |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107082354B (en) | Self-tipping type transports cage and its construction method | |
| CN205653036U (en) | Structure of wireless communication device integration installation | |
| CN103010940B (en) | Falling preventing device for lifting hook | |
| CN207614206U (en) | A kind of hanging rack for safety belt | |
| CN206720558U (en) | A kind of adjustable steel-reinforcement cage hanger | |
| CN107381322A (en) | A kind of satellite fairing assembly hanging basket | |
| CN103287964B (en) | Folding lifting appliance | |
| CN109958819A (en) | A kind of gas pipeline laying method and its supporting structure | |
| CN208479063U (en) | A kind of tower crane cable self-locking fixer | |
| CN209493231U (en) | Tool is turned in large-size machine general assembly | |
| CN209009975U (en) | A kind of self-balancing triangular hanging tool | |
| CN203237915U (en) | Folding lifting appliance | |
| CN206915557U (en) | A kind of suspending assembly | |
| CN205339897U (en) | Aerial -working safety of transformer substation takes linkage | |
| CN204324685U (en) | Interim hanger is used in a kind of novel short range lifting | |
| CN204355947U (en) | Large-scale without eye plate lifting beam device | |
| CN209430211U (en) | One kind hanging mould support device for shield end well to be closed | |
| CN209835621U (en) | Improved oil basin structure | |
| CN208792792U (en) | Prefabricated components hoisting structure and prefabricated components | |
| CN207158604U (en) | A kind of metro bogie boom hoisting | |
| CN203373736U (en) | Precast pile hoisting structure | |
| CN201851137U (en) | Forepole hoisting ring with movable opening | |
| CN106586822A (en) | Lifting tool | |
| CN208489612U (en) | A kind of cable testing bridge | |
| CN203878752U (en) | Connecting device for large steel beam and connecting plate |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20171124 |