CN107323700A - Number for satellite bearing cylinder passes relay antenna and installs panel assembly - Google Patents
Number for satellite bearing cylinder passes relay antenna and installs panel assembly Download PDFInfo
- Publication number
- CN107323700A CN107323700A CN201710359393.9A CN201710359393A CN107323700A CN 107323700 A CN107323700 A CN 107323700A CN 201710359393 A CN201710359393 A CN 201710359393A CN 107323700 A CN107323700 A CN 107323700A
- Authority
- CN
- China
- Prior art keywords
- plectane
- relay antenna
- securing member
- panel assembly
- bearing cylinder
- 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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
- H01Q1/22—Supports; Mounting means by structural association with other equipment or articles
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
- H01Q1/288—Satellite antennas
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Support Of Aerials (AREA)
Abstract
It is used for the number biography relay antenna installation panel assembly of satellite bearing cylinder the invention discloses a kind of, it includes loaded cylinder lower end frame, number biography relay antenna and installs board component, securing member, cross reinforcement, installation plectane, installation plectane outer connector；Cross reinforcement is orthogonal to be connected to installation plectane top surface；The material of cross reinforcement is lead-covering and aluminium honeycomb core；Cross reinforcement is connected by securing member with installing plectane top surface；Cross reinforcement is connected with securing member；Plectane outer connector is installed to be connected by securing member with loaded cylinder lower end frame；Loaded cylinder lower end frame is connected with securing member；Plectane outer connector is installed to be connected with securing member；Number passes relay antenna and installs board component installed in installation plectane bottom surface；The material for installing plectane is carbon fiber skin and aluminium honeycomb core；The present invention adds cross-rib structure using carbon fiber skin aluminium honeycomb core, has the advantages that bonding strength rigidity is big, light weight.
Description
Technical field
Relay antenna is passed the present invention relates to a kind of number, and board component, more particularly to a kind of number for satellite bearing cylinder are installed
Pass relay antenna and panel assembly is installed.
Background technology
It is a kind of structural member for being used to install satellite data transmission relay antenna that number, which passes relay antenna and installs board component, positioned at load
Cylinder bottom, is connected by fastener with loaded cylinder lower end frame；Number passes relay antenna installation board component and ensure that several crossings after day
Rigidity and intensity that line is installed, cause number to pass the problem of relay antenna is nowhere installed while solving satellite arrangement space deficiency.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of number for satellite bearing cylinder and pass relay antenna installing plate
Device, is used for installing number biography relay antenna in satellite bearing cylinder.
The present invention is to solve above-mentioned technical problem by following technical proposals：A kind of number biography for satellite bearing cylinder
Relay antenna installs panel assembly, and it includes loaded cylinder lower end frame, number and passes relay antenna installation board component, securing member, cross
Reinforcement, installation plectane, installation plectane outer connector；The material of cross reinforcement is lead-covering and aluminium honeycomb core, and cross adds
Strengthening tendons is connected by securing member with installing plectane top surface；Cross reinforcement is connected with securing member；Plectane outer is installed
Connector is connected with loaded cylinder lower end frame by securing member；Loaded cylinder lower end frame is connected with securing member；Plectane is installed
Outer connector is connected with securing member；Number passes relay antenna and installs board component installed in installation plectane bottom surface；Plectane is installed
Material be carbon fiber skin and aluminium honeycomb core；Number passes relay antenna installation board component and is connected with loaded cylinder lower end frame.
Preferably, the installation plectane external diameter is 848mm, and thickness is 40mm.
Preferably, the carbon fiber skin for installing plectane is multilayer laying, is 0.1mm per thickness degree.
Preferably, the cross reinforcement is orthogonal is connected to installation plectane top surface.
Preferably, the cross Rib Thickness is 20mm, and height 100mm, quantity is 3.
Preferably, the installation plectane outer connector is to connect loaded cylinder lower end frame.
Preferably, the lead-covering thickness is 0.3mm.
Preferably, the bottom surface for installing plectane provides interface and passes relay antenna installation board component to install number.
The positive effect of the present invention is：Installation board component provided by the present invention, using carbon fiber skin aluminium honeybee
Nest core adds cross-rib structure, has the advantages that bonding strength rigidity is big, light weight；Relay antenna is passed to installing plate component bottom plane number
Interface is adjusted, so that it may is met the demand that different instruments or unit are installed, is added arrangement space, improve space availability ratio；Peace
Fill the carbon fiber laying number of plies and cross-rib height of plectane and after thickness slightly adjusts, installation board component rigidity can be changed and strong
Degree, the different instrument of adaptation or unit are installed, and with higher versatility, application prospect is extensive.
Brief description of the drawings
Fig. 1 is the sectional view of the number biography relay antenna installation panel assembly for satellite bearing cylinder.
Fig. 2 is the structural representation of the number biography relay antenna installation panel assembly for satellite bearing cylinder.
Embodiment
Present pre-ferred embodiments are provided below in conjunction with the accompanying drawings, to describe technical scheme in detail.
As depicted in figs. 1 and 2, the present invention passes relay antenna installation panel assembly for the number of satellite bearing cylinder includes loaded cylinder
Lower end frame 1, number pass relay antenna install board component 2, securing member 3, cross reinforcement 4, install plectane 5, install plectane outside
Along connector 6；The material of cross reinforcement 4 is lead-covering and aluminium honeycomb core；Cross reinforcement 4 passes through securing member 3 and peace
Fill the connection of the top surface of plectane 5, it is ensured that whole number passes rigidity and intensity that relay antenna installs board component 2；Cross reinforcement 4 is with being connected
Fastener 3 is connected；Plectane outer connector 6 is installed to be connected by securing member 3 with loaded cylinder lower end frame 1；Loaded cylinder lower end
Frame 1 is connected with securing member 3；Plectane outer connector 6 is installed to be connected with securing member 3；Number passes relay antenna installing plate
Component 2, which is arranged on, installs the bottom surface of plectane 5, realizes and utilizes the arrangement space in loaded cylinder cylinder；The material for installing plectane 5 is carbon fiber
Covering and aluminium honeycomb core；Number passes relay antenna installation board component 2 and is connected with loaded cylinder lower end frame 1.
Installation plectane 5 external diameter is 848mm, and thickness is 40mm, such light weight.
The carbon fiber skin for installing plectane 5 is multilayer laying, is 0.1mm per thickness degree, can totally 10 layers, and connection is more
Firmly, convenient use.
The cross reinforcement 4 is orthogonal to be connected to the installation top surface of plectane 5 to strengthen installing strength and stiffness in the plate of plectane 5.
The thickness of cross reinforcement 4 is 20mm, and height 100mm, quantity is 3, so connects powerful, convenient use.
The bottom surface for installing plectane 5 provides interface and passes relay antenna installation board component 2 to install number, so improves
Space availability ratio.
The lead-covering thickness is 0.3mm, so cost-effective.
The present invention adds cross reinforcement mode to form loaded cylinder number crossing after day using carbon fiber skin aluminium honeycomb core plectane
Line installs board component, installs plectane and is directly connected to loaded cylinder lower end frame；Using adjustment install plectane 5 carbon fiber laying quantity,
Cross Rib Thickness and height, number crossing changes after antennal interface can meet the connection requirement that different instruments are installed, and raising is defended
The utilization rate of star arrangement space.
Advantages of the present invention：The connection that number passes relay antenna installation panel assembly and loaded cylinder lower end frame is simple and reliable, in plate
By the type of attachment of cross reinforcement, with enough rigidity, intensity；The use for preferably meeting number biography relay antenna will
Ask, be significant for satellite spatial utilization rate；As long as to installing plectane laying quantity, cross reinforcement height and thickness
Degree is suitably adjusted, with regard to that can meet the carrying needs that different instruments are installed, so as to improve the adaptability for installing board component.Ten
Font reinforcement is used to strengthen installing strength and stiffness in plectane plate.
Particular embodiments described above, technical problem, technical scheme and beneficial effect to the solution of the present invention are carried out
It is further described, should be understood that the specific embodiment that the foregoing is only of the invention, be not limited to
The present invention, within the spirit and principles of the invention, any modification, equivalent substitution and improvements done etc. should be included in this
Within the protection domain of invention.
Claims (8)
1. a kind of number for satellite bearing cylinder passes relay antenna and installs panel assembly, it is characterised in that it includes loaded cylinder lower end
Frame, number pass relay antenna and install board component, securing member, cross reinforcement, installation plectane, installation plectane outer connector；
The material of cross reinforcement is lead-covering and aluminium honeycomb core；Cross reinforcement is connected by securing member with installing plectane top surface
Connect；Cross reinforcement is connected with securing member；Plectane outer connector is installed and passes through securing member with loaded cylinder lower end frame
Connection；Loaded cylinder lower end frame is connected with securing member；Plectane outer connector is installed to be connected with fastener；Number passes relay antenna
Board component is installed and is arranged on installation plectane bottom surface；The material for installing plectane is carbon fiber skin and aluminium honeycomb core；Number crossing is after day
Line is installed board component and is connected with loaded cylinder lower end frame.
2. the number for satellite bearing cylinder passes relay antenna and installs panel assembly as claimed in claim 1, it is characterised in that described
It is 848mm to install plectane external diameter, and thickness is 40mm.
3. the number for satellite bearing cylinder passes relay antenna and installs panel assembly as claimed in claim 1, it is characterised in that described
The carbon fiber skin for installing plectane is multilayer laying, is 0.1mm per thickness degree.
4. the number for satellite bearing cylinder passes relay antenna and installs panel assembly as claimed in claim 1, it is characterised in that described
Cross reinforcement is orthogonal to be connected to installation plectane top surface.
5. the number for satellite bearing cylinder passes relay antenna and installs panel assembly as claimed in claim 1, it is characterised in that described
Cross Rib Thickness is 20mm, and height 100mm, quantity is 3.
6. the number for satellite bearing cylinder passes relay antenna and installs panel assembly as claimed in claim 1, it is characterised in that described
Plectane outer connector is installed to connect loaded cylinder lower end frame.
7. the number for satellite bearing cylinder passes relay antenna and installs panel assembly as claimed in claim 1, it is characterised in that described
Lead-covering thickness is 0.3mm.
8. the number for satellite bearing cylinder passes relay antenna and installs panel assembly as claimed in claim 1, it is characterised in that described
The bottom surface for installing plectane provides interface to install number biography relay antenna installation board component.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710359393.9A CN107323700A (en) | 2017-05-19 | 2017-05-19 | Number for satellite bearing cylinder passes relay antenna and installs panel assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710359393.9A CN107323700A (en) | 2017-05-19 | 2017-05-19 | Number for satellite bearing cylinder passes relay antenna and installs panel assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107323700A true CN107323700A (en) | 2017-11-07 |
Family
ID=60192553
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710359393.9A Pending CN107323700A (en) | 2017-05-19 | 2017-05-19 | Number for satellite bearing cylinder passes relay antenna and installs panel assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107323700A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005167402A (en) * | 2003-11-28 | 2005-06-23 | Toshiba Corp | Lens antenna apparatus |
| CN102372092A (en) * | 2010-08-17 | 2012-03-14 | 上海卫星工程研究所 | Configuration for low-earth-orbit remote sensing satellite and mounting method thereof |
| CN105122972B (en) * | 2008-05-30 | 2013-01-02 | 上海卫星工程研究所 | For the low remanent magnetism structural slab of satellite |
| CN104260903A (en) * | 2014-09-16 | 2015-01-07 | 上海卫星工程研究所 | Propelling module structure with independent high-rail satellite platform function |
| CN105870579A (en) * | 2016-03-30 | 2016-08-17 | 上海卫星工程研究所 | Installation structure of data transmission relay antenna |
| RU2617018C1 (en) * | 2015-12-09 | 2017-04-19 | Российская Федерация, от имени которой выступает Федеральное космическое агентство | Service system module |
| CN206141845U (en) * | 2016-11-09 | 2017-05-03 | 上海卫星工程研究所 | High rigidity high stability that can bear many fuel conduit head can support |
| CN106628259A (en) * | 2016-11-16 | 2017-05-10 | 上海卫星工程研究所 | Serial type high-rigidity integrated bearing structure |
-
2017
- 2017-05-19 CN CN201710359393.9A patent/CN107323700A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005167402A (en) * | 2003-11-28 | 2005-06-23 | Toshiba Corp | Lens antenna apparatus |
| CN105122972B (en) * | 2008-05-30 | 2013-01-02 | 上海卫星工程研究所 | For the low remanent magnetism structural slab of satellite |
| CN102372092A (en) * | 2010-08-17 | 2012-03-14 | 上海卫星工程研究所 | Configuration for low-earth-orbit remote sensing satellite and mounting method thereof |
| CN104260903A (en) * | 2014-09-16 | 2015-01-07 | 上海卫星工程研究所 | Propelling module structure with independent high-rail satellite platform function |
| RU2617018C1 (en) * | 2015-12-09 | 2017-04-19 | Российская Федерация, от имени которой выступает Федеральное космическое агентство | Service system module |
| CN105870579A (en) * | 2016-03-30 | 2016-08-17 | 上海卫星工程研究所 | Installation structure of data transmission relay antenna |
| CN206141845U (en) * | 2016-11-09 | 2017-05-03 | 上海卫星工程研究所 | High rigidity high stability that can bear many fuel conduit head can support |
| CN106628259A (en) * | 2016-11-16 | 2017-05-10 | 上海卫星工程研究所 | Serial type high-rigidity integrated bearing structure |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107323700A (en) | Number for satellite bearing cylinder passes relay antenna and installs panel assembly | |
| CN208036328U (en) | Multifunctional trolley | |
| CN103963360A (en) | Honeycomb sandwich plate and frame bottom surface integrated structure | |
| CN205476791U (en) | A cross arm mounting structure for overhead transmission line | |
| CN203309364U (en) | Bonded automobile tube bundle fixing support | |
| CN103448918A (en) | Composite end frame spliced with bearing cylinder body fibers and bearing cylinder | |
| CN104362046B (en) | A kind of guide assembly loaded in mixture suitable for different model breaker and its transition frame | |
| CN209642231U (en) | NFMC corrosion resistant composite coining coloured silk reinforced plastic cable bridge frame | |
| CN207776352U (en) | A kind of floor and connector | |
| CN205652211U (en) | A vehicle that is used for installing installation crossbeam of power assembly and has it | |
| CN203351734U (en) | Antenna of elevator control device | |
| CN204823582U (en) | Composite set of rope fastening and spandrel girder | |
| CN205345054U (en) | C support connnection board and have its C post subassembly | |
| CN208698704U (en) | A kind of novel cabin safety box installing mechanism | |
| CN205736831U (en) | Car door support and there is its vehicle | |
| CN207045674U (en) | A kind of monoblock type airstair | |
| CN220584972U (en) | Single-sheath super five-class data cable | |
| CN205669294U (en) | Improve steel section jointing structure | |
| CN203686915U (en) | Lantern steel wire fixing structure | |
| CN208883250U (en) | A kind of high intensity escalator handrail | |
| CN207826003U (en) | A kind of novel seat fixation proximate matter | |
| CN208477491U (en) | A kind of touch module | |
| CN214834337U (en) | SPC impregnated paper composite floor | |
| CN207053136U (en) | Aircraft high current cable immobilizing structure | |
| CN206116026U (en) | Large -scale pyramid with fixed mounting rope |
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: 20171107 |