CN102748999A - Carbon fiber layer shell reinforced supporting cabin - Google Patents
Carbon fiber layer shell reinforced supporting cabin Download PDFInfo
- Publication number
- CN102748999A CN102748999A CN2012102660187A CN201210266018A CN102748999A CN 102748999 A CN102748999 A CN 102748999A CN 2012102660187 A CN2012102660187 A CN 2012102660187A CN 201210266018 A CN201210266018 A CN 201210266018A CN 102748999 A CN102748999 A CN 102748999A
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- Prior art keywords
- carbon fiber
- shop
- layer
- truncated cone
- cabin body
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- 229920000049 Carbon (fiber) Polymers 0.000 title claims abstract description 122
- 239000004917 carbon fiber Substances 0.000 title claims abstract description 122
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 title claims abstract description 122
- 238000003825 pressing Methods 0.000 claims abstract description 7
- 230000002787 reinforcement Effects 0.000 claims description 34
- 239000002131 composite material Substances 0.000 claims description 10
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 9
- 229910052799 carbon Inorganic materials 0.000 claims description 9
- 230000000295 complement effect Effects 0.000 claims description 9
- 239000000835 fiber Substances 0.000 claims description 9
- 238000000748 compression moulding Methods 0.000 claims description 8
- 239000002184 metal Substances 0.000 claims description 6
- 238000000034 method Methods 0.000 claims description 6
- 238000004026 adhesive bonding Methods 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims 1
- 235000015842 Hesperis Nutrition 0.000 abstract 1
- 235000012633 Iberis amara Nutrition 0.000 abstract 1
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
- 230000003014 reinforcing effect Effects 0.000 abstract 1
- 238000010276 construction Methods 0.000 description 6
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000013016 damping Methods 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000008719 thickening Effects 0.000 description 2
- 230000002950 deficient Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
Images
Classifications
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- 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
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/641—Interstage or payload connectors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
The invention relates to a carbon fiber layer shell reinforced supporting cabin, comprising a carbon fiber layer frustum cabin body, a carbon fiber layer middle frame connected with an inner wall of the carbon fiber layer frustum cabin body, and a carbon fiber layer cap type reinforcing rib connected with an outer wall of the carbon fiber layer frustum cabin body; wherein the carbon fiber layer frustum cabin body comprises an upper end frame arranged on a top end thereof, a lower end frame arranged on a bottom end thereof, and a skin which is used for pressing and fixing the upper end frame and the lower end frame and is laid on the outer wall of the carbon fiber layer frustum cabin body. The carbon fiber layer shell reinforced supporting cabin provided by the invention can effectively increase carrying capacity of rockets, actively improve satellite-rocket vibration environment, solve the satellite-rocket vibration response coupling problem, ensure high precision of cabin body connection face, and enable outer surfaces of the cabin body to be smooth and beautiful.
Description
Technical field
The present invention relates to layer shell reinforcement supporting cabin, a kind of carbon fiber shop, refer in particular to a kind of layer shell reinforcement supporting cabin, carbon fiber shop that is applied to carrier rocket.
Background technology
When carrier rocket is launched an artificial satellite, need to use the supporting cabin that satellite and equipment component are erected, thereby realize the variation and the requirement of overall configuration layout of interface size.Model normally adopted the metal support cabin to realize this function in the past.Satisfy intensity and rigidity requirement because big weight cost need be paid in the metal support cabin, therefore, reduced the carrying capacity of rocket, and satellite and the rocket environment (vibration) is comparatively abominable.
Honeycomb sandwich construction is adopted in existing composite supporting cabin more; The type supporting cabin can better reduce the construction weight in supporting cabin; But because honeycomb sandwich construction end frame still adopts metal forging machine to add and forms; Simultaneously, operations such as honeycomb sandwich construction repairing can cause construction weight significantly to increase, and it is not fairly obvious that construction weight reduces amplitude.
Summary of the invention
The object of the present invention is to provide layer shell reinforcement supporting cabin, a kind of carbon fiber shop; It can effectively improve rocket carrying capacity, actively improves satellite and the rocket vibration environment, solves satellite and the rocket vibratory response coupled problem; Guarantee the high accuracy of cabin body joint face, and make the external mass color in cabin along attractive in appearance.
In order to achieve the above object; The present invention provides layer shell reinforcement supporting cabin, a kind of carbon fiber shop; It comprises: layer truncated cone cabin, carbon fiber shop body; Connect the carbon fiber shop layer middle boxes that is arranged on the body inwall of layer truncated cone cabin, said carbon fiber shop, and connect the carbon fiber shop layer shape for hat reinforcement that is arranged on the external wall in layer truncated cone cabin, said carbon fiber shop; Wherein, layer truncated cone cabin, a said carbon fiber shop body comprises the upper end frame that is arranged on its top, is arranged on the lower end frame of its bottom, and by press fit said upper end frame and lower end frame and be laid on the covering on layer external wall in truncated cone cabin of carbon fiber shop.
Layer truncated cone cabin, said carbon fiber shop body is processed by carbon fibre composite; Said carbon fiber shop layer middle boxes adopts carbon fibre composite to lay mold pressing and processes; Said carbon fiber shop layer shape for hat reinforcement adopts carbon fibre composite to lay and processes.
Said upper end frame comprises the first horizontal direct tube section that connects successively, vertically the direct tube section and the first awl section main body; The setting of aliging of the top of layer truncated cone cabin, the said first horizontal direct tube section and carbon fiber shop body; Applyings that be complementary of the top exterior walls of the said vertical direct tube section and the first awl section main body and layer truncated cone cabin, carbon fiber shop body, and said first an awl section main body is connected with covering and fixes.
Utilize former that upper end frame and covering are not had the integrated compression molding of connector, make covering by press fit described upper end frame and be laid on the outer wall of layer truncated cone cabin, carbon fiber shop body.
Said lower end frame comprises the second horizontal direct tube section and the second awl section main body that connects successively; The setting of aliging of the bottom of layer truncated cone cabin, the said second horizontal direct tube section and carbon fiber shop body; Applyings that be complementary of the bottom outer wall of the said second awl section main body and layer truncated cone cabin, carbon fiber shop body, and said second an awl section main body is connected with covering and fixes.
Utilize former that lower end frame and covering are not had the integrated compression molding of connector, make covering by press fit described lower end frame and be laid on the outer wall of layer truncated cone cabin, carbon fiber shop body.
Offer gathering hole on the body of layer truncated cone cabin, said carbon fiber shop; On said gathering hole, metal frame is installed.
Said carbon fiber shop layer middle boxes is zigzag, comprises the first frame ring, the second frame ring, the 3rd frame ring and the configuration frame ring that connect successively; The said second frame ring, the 3rd frame ring and configuration frame ring vertically are connected each other; Applyings that be complementary of the inwall of layer truncated cone cabin, the said first frame ring and carbon fiber shop body, and through glueing joint and riveted and fixed is arranged on the inwall of carbon fiber shop layer truncated cone cabin body.
Said carbon fiber shop layer middle boxes also comprises first fishplate bar and second fishplate bar, is arranged on the upper and lower surface of carbon fiber shop layer middle boxes respectively through riveted joint.
Layer truncated cone cabin body circumferentially is provided with said carbon fiber shop layer shape for hat reinforcement along the carbon fiber shop; The two bottom sides linkage section of this carbon fiber shop layer shape for hat reinforcement is fixedly installed on the outer surface of covering through splicing, and is connected with layer truncated cone cabin, carbon fiber shop body through riveted joint.
Layer shell reinforcement supporting cabin, carbon fiber provided by the present invention shop; Compared with prior art has following beneficial effect: adopt former upper end frame, lower end frame and covering not to be had the integrated compression molding of connector; Guarantee the high accuracy of cabin body joint face, and make the external mass color in cabin along attractive in appearance.In addition, the present invention adopts the version of carbon fiber shop layer shell reinforcement, and the weight saving in whole supporting cabin effectively improves carrying capacity more than 25%, and has the better damping effect.
Description of drawings
Fig. 1 is the outline drawing of carbon fiber shop layer truncated cone cabin body among the present invention;
Fig. 2 is the stereogram of carbon fiber shop layer truncated cone cabin body among the present invention;
Fig. 3 is the upper end frame sectional view of carbon fiber shop layer truncated cone cabin body among the present invention;
Fig. 4 is the lower end frame sectional view of carbon fiber shop layer truncated cone cabin body among the present invention;
Fig. 5 A is the former mold pressing sketch map of carbon fiber shop layer truncated cone cabin body among the present invention; Wherein, Fig. 5 B is the mold pressing sketch map of former and upper end frame, and Fig. 5 C is the mold pressing sketch map of former and lower end frame;
Fig. 6 is the sectional view of layer shape for hat reinforcement in carbon fiber shop among the present invention;
Fig. 7 is the sectional view of carbon fiber shop layer middle boxes among the present invention;
Fig. 8 is the assembling sketch map of carbon fiber shop layer middle boxes among the present invention;
Fig. 9 is the sketch map that is connected that carbon fiber is spread layer truncated cone cabin body and carbon fiber shop layer middle boxes among the present invention;
Figure 10 is the sketch map that is connected that carbon fiber is spread layer truncated cone cabin body and carbon fiber shop layer shape for hat reinforcement among the present invention.
The specific embodiment
Following according to Fig. 1～Figure 10, specify preferred embodiment of the present invention.
As depicted in figs. 1 and 2; Layer shell reinforcement supporting cabin, carbon fiber provided by the present invention shop; Comprise layer truncated cone cabin, carbon fiber shop body 1; Connect the carbon fiber shop layer middle boxes 2 that is arranged on body 1 inwall of layer truncated cone cabin, said carbon fiber shop, and connect the carbon fiber shop layer shape for hat reinforcement 3 that is arranged on body 1 outer wall of layer truncated cone cabin, said carbon fiber shop; Wherein, layer truncated cone cabin, a said carbon fiber shop body 1 comprises the upper end frame 101 that is arranged on its top, is arranged on the lower end frame 102 of its bottom, and by the said upper end of press fit frame 101 with lower end frame 102 and be laid on the covering 4 on body 1 outer wall of layer truncated cone cabin, carbon fiber shop.
As shown in Figure 3, said upper end frame 101 comprises the first horizontal direct tube section 11 that connects successively, vertically the direct tube section 12 and the first awl section main body 13; Wherein, the top of layer truncated cone cabin, the said first horizontal direct tube section 11 and carbon fiber shop body 1 setting of aliging; Applyings that be complementary of the top exterior walls of the said vertical direct tube section 12 and the first awl section main body 13 and layer truncated cone cabin, carbon fiber shop body 1, and the said first awl section main body 13 is successively decreased to be connected with covering 4 through the shop layer and is fixed.Shown in Fig. 5 A and Fig. 5 B, utilize 5 pairs of formers upper end frame 101 and covering 4 through the design of thickening degree, need not the integrated compression molding of other connectors, make covering 4 by the described upper end of press fit frame 101 and be laid on the outer wall of layer truncated cone cabin, carbon fiber shop body 1.
As shown in Figure 4, said lower end frame 102 comprises the second horizontal direct tube section 14 and the second awl section main body 15 that connects successively; Wherein, the bottom of layer truncated cone cabin, the said second horizontal direct tube section 14 and carbon fiber shop body 1 setting of aliging; Applyings that be complementary of the bottom outer wall of the said second awl section main body 15 and layer truncated cone cabin, carbon fiber shop body 1, and the said second awl section main body 15 is successively decreased to be connected with covering 4 through the shop layer and is fixed.Shown in Fig. 5 A and Fig. 5 C, utilize 5 pairs of lower end frames of former 102 and covering 4 through the design of thickening degree, need not the integrated compression molding of other connectors, make covering 4 by the described lower end of press fit frame 102 and be laid on the outer wall of layer truncated cone cabin, carbon fiber shop body 1.
As illustrated in figs. 1 and 2, also offer gathering hole 103 on layer truncated cone cabin, the said carbon fiber shop body 1; And can on said gathering hole 103, metal frame be installed according to actual needs.
Further, layer truncated cone cabin, said carbon fiber shop body 1 is processed by carbon fibre composite, and the appearance fairing is attractive in appearance.
As shown in Figure 7, said carbon fiber shop layer middle boxes 2 adopts carbon fibre composite to lay mold pressing and processes.This carbon fiber shop layer middle boxes 2 is zigzag, comprises the first frame ring 21 that connects successively, the second frame ring 22, the 3rd frame ring 23 and configuration frame ring 24; Wherein, the said second frame ring 22, the 3rd frame ring 23 vertically are connected with configuration frame ring 24 each other; As shown in Figure 9; The applying that is complementary of the inwall of the said first frame ring 21 and layer truncated cone cabin, carbon fiber shop body 1; And through glueing joint and riveted and fixed is arranged on the inwall of layer truncated cone cabin, carbon fiber shop body 1, thereby make whole carbon fiber shop layer middle boxes 2 and layer truncated cone cabin, a carbon fiber shop body 1 assembling integrator.
As shown in Figure 8, said carbon fiber shop layer middle boxes 2 also comprises first fishplate bar 25 and second fishplate bar 26, is arranged on the upper and lower surface of carbon fiber shop layer middle boxes 2 respectively through riveted joint.
Said carbon fiber shop layer shape for hat reinforcement 3 adopts carbon fibre composite to lay and processes.As shown in Figure 2, layer truncated cone cabin body 1 circumferentially is provided with said carbon fiber shop layer shape for hat reinforcement 3 along the carbon fiber shop.Like Fig. 6 and shown in Figure 10, the two bottom sides linkage section 31 of this carbon fiber shop layer shape for hat reinforcement 3 is fixedly installed on the outer surface of covering 4 through splicing, and is connected with layer truncated cone cabin, carbon fiber shop body 1 through riveted joint.
In sum; Layer shell reinforcement supporting cabin, carbon fiber provided by the present invention shop; Can effectively improve rocket carrying capacity, and can actively improve satellite and the rocket vibration environment, therefore overcome the big and undercoupling defective of satellite and the rocket vibration frequency of rocket supporting cabin structure weight in the prior art.
Compared with prior art, the invention has the beneficial effects as follows:, guarantee the high accuracy of cabin body joint face, and make the external mass color in cabin along attractive in appearance owing to adopt former that upper end frame, lower end frame and covering are not had the integrated compression molding of connector.In addition, the present invention adopts the version of carbon fiber shop layer shell reinforcement, and the weight saving in whole supporting cabin effectively improves carrying capacity more than 25%, and has the better damping effect.
Although content of the present invention has been done detailed introduction through above-mentioned preferred embodiment, will be appreciated that above-mentioned description should not be considered to limitation of the present invention.After those skilled in the art have read foregoing, for multiple modification of the present invention with to substitute all will be conspicuous.Therefore, protection scope of the present invention should be limited appended claim.
Claims (10)
1. a carbon fiber shop layer shell reinforcement supports the cabin; It is characterized in that; Comprise: carbon fiber shop layer truncated cone cabin body (1); Connect the carbon fiber shop layer middle boxes (2) that is arranged on layer truncated cone cabin body (1) inwall of said carbon fiber shop, and connect the carbon fiber shop layer shape for hat reinforcement (3) that is arranged on layer truncated cone cabin body (1) outer wall of said carbon fiber shop;
Said carbon fiber shop layer truncated cone cabin body (1) comprises the upper end frame (101) that is arranged on its top; Be arranged on the lower end frame (102) of its bottom, and by the said upper end of press fit frame (101) and lower end frame (102) and be laid on the covering (4) on carbon fiber shop layer truncated cone cabin body (1) outer wall.
2. layer shell reinforcement supporting cabin, carbon fiber as claimed in claim 1 shop is characterized in that said carbon fiber shop layer truncated cone cabin body (1) processed by carbon fibre composite; Said carbon fiber shop layer middle boxes (2) adopts carbon fibre composite to lay mold pressing and processes; Said carbon fiber shop layer shape for hat reinforcement (3) adopts carbon fibre composite to lay and processes.
3. layer shell reinforcement supporting cabin, carbon fiber as claimed in claim 2 shop is characterized in that said upper end frame (101) comprises the first horizontal direct tube section (11) that connects successively, vertically the direct tube section (12) and the first awl section main body (13);
The setting of aliging of the top of the said first horizontal direct tube section (11) and carbon fiber shop layer truncated cone cabin body (1);
Applyings that be complementary of the top exterior walls of the said vertical direct tube section (12) and the first awl section main body (13) and carbon fiber shop layer truncated cone cabin body (1), and said first an awl section main body (13) is connected with covering (4) and fixes.
4. layer shell reinforcement supporting cabin, carbon fiber as claimed in claim 3 shop; It is characterized in that; Utilize former (5) that upper end frame (101) and covering (4) are not had the integrated compression molding of connector, make covering (4) by the described upper end of press fit frame (101) and be laid on the outer wall of carbon fiber shop layer truncated cone cabin body (1).
5. layer shell reinforcement supporting cabin, carbon fiber as claimed in claim 2 shop is characterized in that, said lower end frame (102) comprises the second horizontal direct tube section (14) and the second awl section main body (15) that connects successively;
The setting of aliging of the bottom of the said second horizontal direct tube section (14) and carbon fiber shop layer truncated cone cabin body (1);
Applyings that be complementary of the bottom outer wall of the said second awl section main body (15) and carbon fiber shop layer truncated cone cabin body (1), and said second an awl section main body (15) is connected with covering (4) and fixes.
6. layer shell reinforcement supporting cabin, carbon fiber as claimed in claim 5 shop; It is characterized in that; Utilize former (5) that lower end frame (102) and covering (4) are not had the integrated compression molding of connector, make covering (4) by the described lower end of press fit frame (102) and be laid on the outer wall of carbon fiber shop layer truncated cone cabin body (1).
7. layer shell reinforcement supporting cabin, carbon fiber as claimed in claim 2 shop is characterized in that, offers gathering hole (103) on the said carbon fiber shop layer truncated cone cabin body (1); Go up the installation metal frame at said gathering hole (103).
8. layer shell reinforcement supporting cabin, carbon fiber as claimed in claim 2 shop; It is characterized in that; Said carbon fiber shop layer middle boxes (2) is zigzag, comprises the first frame ring (21), the second frame ring (22), the 3rd frame ring (23) and the configuration frame ring (24) that connect successively;
The said second frame ring (22), the 3rd frame ring (23) and configuration frame ring (24) vertically are connected each other;
Applyings that be complementary of the inwall of the said first frame ring (21) and carbon fiber shop layer truncated cone cabin body (1), and through glueing joint and riveted and fixed is arranged on the inwall of carbon fiber shop layer truncated cone cabin body (1).
9. layer shell reinforcement supporting cabin, carbon fiber as claimed in claim 8 shop; It is characterized in that; Said carbon fiber shop layer middle boxes (2) also comprises first fishplate bar (25) and second fishplate bar (26), is arranged on the upper and lower surface of carbon fiber shop layer middle boxes (2) respectively through riveted joint.
10. layer shell reinforcement supporting cabin, carbon fiber as claimed in claim 2 shop is characterized in that said carbon fiber shop layer shape for hat reinforcement (3) circumferentially is provided with along carbon fiber shop layer truncated cone cabin body (1); The two bottom sides linkage section (31) of this carbon fiber shop layer shape for hat reinforcement (3) is fixedly installed on the outer surface of covering (4) through splicing, and is connected with carbon fiber shop layer truncated cone cabin body (1) through riveted joint.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012102660187A CN102748999A (en) | 2012-07-30 | 2012-07-30 | Carbon fiber layer shell reinforced supporting cabin |
| PCT/CN2013/000097 WO2014019328A1 (en) | 2012-07-30 | 2013-01-30 | Carbon fiber layer thin shell reinforced supporting cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012102660187A CN102748999A (en) | 2012-07-30 | 2012-07-30 | Carbon fiber layer shell reinforced supporting cabin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102748999A true CN102748999A (en) | 2012-10-24 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012102660187A Pending CN102748999A (en) | 2012-07-30 | 2012-07-30 | Carbon fiber layer shell reinforced supporting cabin |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN102748999A (en) |
| WO (1) | WO2014019328A1 (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014019328A1 (en) * | 2012-07-30 | 2014-02-06 | 上海宇航系统工程研究所 | Carbon fiber layer thin shell reinforced supporting cabin |
| CN105269839A (en) * | 2015-11-25 | 2016-01-27 | 哈尔滨工业大学 | Method for preparing fibrous composite cap-type rib mold based on shape memory polymers |
| CN105466288A (en) * | 2015-11-20 | 2016-04-06 | 江西长江化工有限责任公司 | Cabin of conical rotary body structure and manufacturing method of cabin |
| CN105539879A (en) * | 2015-12-02 | 2016-05-04 | 上海宇航系统工程研究所 | Spatial box type cabin structure |
| CN108725844A (en) * | 2018-06-26 | 2018-11-02 | 北京蓝箭空间科技有限公司 | The control cabin structure of space launch vehicle |
| CN112061421A (en) * | 2020-09-24 | 2020-12-11 | 上海宇航系统工程研究所 | Multi-satellite parallel transmitting device based on auxiliary support |
| CN116518795A (en) * | 2023-07-03 | 2023-08-01 | 江苏亨睿航空工业有限公司 | Carbon fiber composite satellite supporting cabin and preparation method thereof |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN111252272B (en) * | 2020-02-26 | 2022-02-01 | 航天科工防御技术研究试验中心 | Vacuum vibration-proof cabin |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014019328A1 (en) * | 2012-07-30 | 2014-02-06 | 上海宇航系统工程研究所 | Carbon fiber layer thin shell reinforced supporting cabin |
| CN105466288A (en) * | 2015-11-20 | 2016-04-06 | 江西长江化工有限责任公司 | Cabin of conical rotary body structure and manufacturing method of cabin |
| CN105269839A (en) * | 2015-11-25 | 2016-01-27 | 哈尔滨工业大学 | Method for preparing fibrous composite cap-type rib mold based on shape memory polymers |
| CN105539879A (en) * | 2015-12-02 | 2016-05-04 | 上海宇航系统工程研究所 | Spatial box type cabin structure |
| CN108725844A (en) * | 2018-06-26 | 2018-11-02 | 北京蓝箭空间科技有限公司 | The control cabin structure of space launch vehicle |
| CN112061421A (en) * | 2020-09-24 | 2020-12-11 | 上海宇航系统工程研究所 | Multi-satellite parallel transmitting device based on auxiliary support |
| CN116518795A (en) * | 2023-07-03 | 2023-08-01 | 江苏亨睿航空工业有限公司 | Carbon fiber composite satellite supporting cabin and preparation method thereof |
| CN116518795B (en) * | 2023-07-03 | 2023-09-15 | 江苏亨睿航空工业有限公司 | Carbon fiber composite satellite supporting cabin and preparation method thereof |
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