CN106184824A - A kind of integration primary load bearing tank structure - Google Patents
A kind of integration primary load bearing tank structure Download PDFInfo
- Publication number
- CN106184824A CN106184824A CN201610666903.2A CN201610666903A CN106184824A CN 106184824 A CN106184824 A CN 106184824A CN 201610666903 A CN201610666903 A CN 201610666903A CN 106184824 A CN106184824 A CN 106184824A
- Authority
- CN
- China
- Prior art keywords
- load bearing
- primary load
- tank
- bearing tank
- integration
- 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
- 230000010354 integration Effects 0.000 title claims abstract description 13
- 238000003466 welding Methods 0.000 claims abstract description 4
- 239000003380 propellant Substances 0.000 claims description 16
- 101710144202 Probable soluble pyridine nucleotide transhydrogenase Proteins 0.000 claims description 8
- 101710165942 Soluble pyridine nucleotide transhydrogenase Proteins 0.000 claims description 8
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
- 238000003860 storage Methods 0.000 claims description 2
- 230000014759 maintenance of location Effects 0.000 claims 1
- RTZKZFJDLAIYFH-UHFFFAOYSA-N Diethyl ether Chemical compound CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000008280 blood Substances 0.000 description 1
- 210000004369 blood Anatomy 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
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
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/402—Propellant tanks; Feeding propellants
-
- 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
Abstract
The invention discloses a kind of integration primary load bearing tank structure, including several primary load bearing tanks, connection is run through by welding manner between adjacent two primary load bearing tanks, it is equipped with bearing rod inside each primary load bearing tank, bearing rod upper end is connected with imitating load switchover frame through primary load bearing tank end face, lower end connects through primary load bearing tank bottom surface has the satellite and the rocket to connect ring, and bearing rod welds with primary load bearing tank.Primary load bearing tank integration is run through connection by the present invention, by bearing rod load, is connected to transversary by the combination of primary load bearing tank simultaneously, not only reduce the quality of main force support structure, and greatly strengthen the stability of structure, improve overall load performance, the more payload of portability.
Description
Technical field
The present invention relates to the spacecraft for field of deep space exploration, specifically a kind of integration primary load bearing tank knot
Structure.
Background technology
The spacecraft of current domestic existing field of deep space exploration, all uses main force support structure the most only with propelling module
Vertical design.It is very big that spacecraft becomes rail speed increment, therefore need to carry a large amount of propellant, and carrying capacity is limited, to payload
Cause greatly constraint.As a example by ether anode rail detector, traditional design load cabin quality must not exceed 1.2t.For reducing structure matter
Amount, improves the ability carrying payload, and effective ways are development integrated techniques, by main force support structure and propulsion system tank
Blend, common load bearing equipment installation, mechanical environment, thermal environment etc..
Primary load bearing tank is run through the integrated design of connection, outside completing its basic function storage propellant, not only
Disclosure satisfy that load demand, improve the mass ratio of propellant and propulsion system structure, and due to integrated design, enhancing finishes
The stability of structure.
Summary of the invention
In order to solve the problems referred to above, the invention provides a kind of integration primary load bearing tank structure.
The purpose of the present invention is achieved through the following technical solutions: a kind of integration primary load bearing tank structure, including some
Individual primary load bearing tank, runs through connection by welding manner between adjacent two primary load bearing tanks, and each primary load bearing tank is internal all
Being provided with bearing rod, bearing rod upper end is connected with imitating load switchover frame through primary load bearing tank end face, and lower end is store through primary load bearing
Bottom face connects has the satellite and the rocket to connect ring, and bearing rod welds with primary load bearing tank.
As preferably, described primary load bearing tank is 6, and described primary load bearing tank is the class spherical junctions such as spherical, elliposoidal
Structure.
As preferably, each primary load bearing tank all uses aluminum alloy materials.
As preferably, described primary load bearing tank is the first propellant of the electronic machine tank of three STHs, a STH
Tank and without the one in the second propellant tank of perforate, and adjacent two primary load bearing tank classifications are different.
As preferably, described electronic machine tank, the first propellant tank of a STH and the second propelling without perforate
Agent tank is respectively two.
Compared with prior art, the method have the advantages that
Primary load bearing tank integration is run through connection, by bearing rod load, is connected to horizontal stroke by the combination of primary load bearing tank simultaneously
To structure, not only reduce the quality of main force support structure, and greatly strengthen the stability of structure, improve overall force-bearing property
Can, the more payload of portability.
Accompanying drawing explanation
Fig. 1 is the overall structure schematic diagram of the embodiment of the present invention.
Fig. 2 is three kinds of primary load bearing tank structural representations of the present invention；
Wherein, a is electronic machine tank, and b is the first propellant tank, and c is the second propellant tank.
Fig. 3 is the bearing rod schematic diagram in the embodiment of the present invention；
Detailed description of the invention
Below in conjunction with specific embodiment, the present invention is described in detail.Following example will assist in the technology of this area
Personnel are further appreciated by the present invention, but limit the present invention the most in any form.It should be pointed out that, the ordinary skill to this area
For personnel, without departing from the inventive concept of the premise, it is also possible to make some deformation and improvement.These broadly fall into the present invention
Protection domain.
As shown in Figure 1-Figure 3, embodiments provide a kind of integration primary load bearing tank structure, main including several
Load tank, runs through connection by welding manner between adjacent two primary load bearing tanks, is equipped with inside each primary load bearing tank
Bearing rod 4, bearing rod 4 upper end is connected with imitating load switchover frame 5 through primary load bearing tank end face, and lower end passes primary load bearing tank
Bottom surface connects has the satellite and the rocket to connect ring 6, and bearing rod 4 welds with primary load bearing tank.
Described primary load bearing tank is 6, and described primary load bearing tank is the class spherical structures such as spherical, elliposoidal.
Each primary load bearing tank all uses aluminum alloy materials.
Described primary load bearing tank is the first propellant tank 2 and nothing of electronic machine tank 1, STH of three STHs
One in second propellant tank 3 of perforate, and adjacent two primary load bearing tank classifications are different.
First propellant tank 2 of described electronic machine tank 1, STH and the second propellant tank 3 without perforate
It is respectively two.
Originally it is embodied as primary load bearing tank integration is run through connection, by bearing rod load, simultaneously by primary load bearing tank group
Conjunction is connected to transversary, not only reduces the quality of main force support structure, and greatly strengthen the stability of structure, improves
Overall load performance, the more payload of portability.
Above the specific embodiment of the present invention is described.It is to be appreciated that the invention is not limited in above-mentioned
Particular implementation, those skilled in the art can make various deformation or amendment within the scope of the claims, this not shadow
Ring the flesh and blood of the present invention.
Claims (5)
1. an integrated primary load bearing tank structure, it is characterised in that include several primary load bearing tanks, adjacent two primary load bearing storages
Run through connection by welding manner between case, inside each primary load bearing tank, be equipped with bearing rod (4), bearing rod (4) upper end
Being connected with imitating load switchover frame (5) through primary load bearing tank end face, lower end connects through primary load bearing tank bottom surface has the satellite and the rocket even
T-Ring (6), bearing rod (4) welds with primary load bearing tank.
Integration primary load bearing tank structure the most according to claim 1, it is characterised in that described primary load bearing tank is 6,
Described primary load bearing tank is class spherical structure.
Integration primary load bearing tank structure the most according to claim 1, it is characterised in that each primary load bearing tank all uses
Aluminum alloy materials.
4. according to the integrated primary load bearing tank structure described in Claims 1-4, it is characterised in that described primary load bearing tank is
The electronic machine tank (1) of three STHs, first propellant tank (2) of a STH and the second propellant tank without perforate
(3) one in, and adjacent two primary load bearing tank classifications are different.
Integration primary load bearing tank structure the most according to claim 4, it is characterised in that described electronic machine tank (1),
First propellant tank (2) of one STH and the second propellant tank (3) without perforate are respectively two.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610666903.2A CN106184824A (en) | 2016-08-12 | 2016-08-12 | A kind of integration primary load bearing tank structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610666903.2A CN106184824A (en) | 2016-08-12 | 2016-08-12 | A kind of integration primary load bearing tank structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106184824A true CN106184824A (en) | 2016-12-07 |
Family
ID=57521450
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610666903.2A Pending CN106184824A (en) | 2016-08-12 | 2016-08-12 | A kind of integration primary load bearing tank structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106184824A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106837606A (en) * | 2017-03-30 | 2017-06-13 | 哈尔滨工业大学 | A kind of integral composite material tank structure |
| CN111470069A (en) * | 2020-04-08 | 2020-07-31 | 上海卫星工程研究所 | Lower end frame structure suitable for satellite bearing cylinder |
| CN111550327A (en) * | 2020-04-02 | 2020-08-18 | 上海空间推进研究所 | Connecting and supporting structure of spacecraft low-temperature storage tank and assembling method |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2340516C1 (en) * | 2007-06-22 | 2008-12-10 | Федеральное государственное унитарное предприятие "Научно-производственное объединение им. С.А. Лавочкина" | Upper-stage rocket and strong ring (2 versions) |
| CN203254077U (en) * | 2013-04-12 | 2013-10-30 | 中国航天科技集团公司长征机械厂 | Integrated automatic welding device for longitudinal seams and circular seam at bottom of storage tank |
| CN103482085A (en) * | 2013-08-12 | 2014-01-01 | 上海卫星工程研究所 | Force-bearing integrated structure with honeycomb-sandwich storage boxes |
| CN204223194U (en) * | 2014-10-28 | 2015-03-25 | 北京宇航系统工程研究所 | A kind of light thin-wall goalpost shape suspension type tank structure |
| CN105346732A (en) * | 2015-09-29 | 2016-02-24 | 上海卫星工程研究所 | Thin-wall light integrated storage tank installing device and implementation method |
-
2016
- 2016-08-12 CN CN201610666903.2A patent/CN106184824A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2340516C1 (en) * | 2007-06-22 | 2008-12-10 | Федеральное государственное унитарное предприятие "Научно-производственное объединение им. С.А. Лавочкина" | Upper-stage rocket and strong ring (2 versions) |
| CN203254077U (en) * | 2013-04-12 | 2013-10-30 | 中国航天科技集团公司长征机械厂 | Integrated automatic welding device for longitudinal seams and circular seam at bottom of storage tank |
| CN103482085A (en) * | 2013-08-12 | 2014-01-01 | 上海卫星工程研究所 | Force-bearing integrated structure with honeycomb-sandwich storage boxes |
| CN204223194U (en) * | 2014-10-28 | 2015-03-25 | 北京宇航系统工程研究所 | A kind of light thin-wall goalpost shape suspension type tank structure |
| CN105346732A (en) * | 2015-09-29 | 2016-02-24 | 上海卫星工程研究所 | Thin-wall light integrated storage tank installing device and implementation method |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106837606A (en) * | 2017-03-30 | 2017-06-13 | 哈尔滨工业大学 | A kind of integral composite material tank structure |
| CN111550327A (en) * | 2020-04-02 | 2020-08-18 | 上海空间推进研究所 | Connecting and supporting structure of spacecraft low-temperature storage tank and assembling method |
| CN111550327B (en) * | 2020-04-02 | 2021-06-04 | 上海空间推进研究所 | Connecting and supporting structure of spacecraft low-temperature storage tank and assembling method |
| CN111470069A (en) * | 2020-04-08 | 2020-07-31 | 上海卫星工程研究所 | Lower end frame structure suitable for satellite bearing cylinder |
| CN111470069B (en) * | 2020-04-08 | 2021-11-16 | 上海卫星工程研究所 | Lower end frame structure suitable for satellite bearing cylinder |
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| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161207 |
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| RJ01 | Rejection of invention patent application after publication |