CN109515754A - A kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure - Google Patents
A kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure Download PDFInfo
- Publication number
- CN109515754A CN109515754A CN201910031516.5A CN201910031516A CN109515754A CN 109515754 A CN109515754 A CN 109515754A CN 201910031516 A CN201910031516 A CN 201910031516A CN 109515754 A CN109515754 A CN 109515754A
- Authority
- CN
- China
- Prior art keywords
- gas
- rocket
- supporting plate
- bay section
- high volume
- 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
- 238000006073 displacement reaction Methods 0.000 claims abstract description 7
- 238000006243 chemical reaction Methods 0.000 claims abstract description 4
- 230000013011 mating Effects 0.000 claims abstract description 4
- 238000009434 installation Methods 0.000 abstract description 9
- 239000007789 gas Substances 0.000 description 55
- 238000010586 diagram Methods 0.000 description 6
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 239000007921 spray 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
-
- 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
Abstract
The present invention relates to gas cylinders group installing area more particularly to a kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structures.The structure includes gas support and hoop component, gas support includes gas support lower end supporting plate, straight tube is vertically connected between gas support upper end supporting plate and its gas support lower end supporting plate and gas support upper end supporting plate, multiple gas cylinders are set on the supporting plate of gas support lower end and place notch, and gas support upper end supporting plate corresponds to gas cylinder and places and lateral Displacement notch is arranged on notch, gas cylinder is placed by the mating reaction that gas cylinder places notch and lateral Displacement notch, the upper end of gas cylinder is clamped hoop component, the one or both ends of hoop component and one end of telescopic rod are hinged, the telescopic rod other end is hinged with gas support upper end supporting plate.The present invention solves the difficulty of existing high volume accounting rocket rocket body bay section installation high pressure gas cylinder group, realizes effective fixed and installation of the high pressure gas tank of cold air propulsion system in bay section.
Description
Technical field
The present invention relates to gas cylinders group installing area more particularly to a kind of high volume accounting rocket rocket body bay section gas cylinders group installations
Structure.
Background technique
Cold air propulsion system is usually by gas tank, four part group of voltage-regulating system, pipe-line system and thruster system
At.When work, the propellant (the usually inert gases such as helium) in high pressure tank is depressurized by depressurized system, then passes through pipe
Road system is transported to thruster entrance, and thruster sprays cold air and generates thrust.
Different from the low pressure tank (generally no greater than 0.5MPa) of rocket system, the gas tank pressure of cold air propulsion system
Bigger (being generally greater than 23MPa).Also, cold air propulsion system is generally used for satellite system, less to be applied to rocket system
System.Therefore, the high pressure gas of cold air propulsion system is then fitted into fixation firstly the need of being stored in special high pressure gas cylinder group
In the narrow bay section rocket body of size.Since the volume of high pressure gas cylinder group has already taken up most of space of bay section, then so
Rocket rocket body bay section installation high pressure gas tank (i.e. gas cylinders group) of high volume accounting is more difficult.
Summary of the invention
To solve the above-mentioned problems, the present invention provides existing high volume accounting rocket rocket body bay section installation high pressure gas cylinder group
Difficulty realizes effective fixed and installation of the high pressure gas tank of cold air propulsion system in bay section.
This is practical to use the novel technical solution taken to achieve the above object are as follows:
A kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure, which includes gas support and clip group
Part, the gas support include gas support lower end supporting plate, gas support upper end supporting plate and its gas support lower end supporting plate with
It is vertically connected with straight tube between the supporting plate of gas support upper end, multiple gas cylinder placing grooves are set on the supporting plate of the gas support lower end
Mouthful, and gas support upper end supporting plate corresponds to gas cylinder and places and lateral Displacement notch is arranged on notch, places notch and side by gas cylinder
Gas cylinder is placed to the mating reaction of spacing edge-cut, the upper end of the gas cylinder is clamped hoop component, and the one of the hoop component
End or both ends and one end of telescopic rod are hinged, and the telescopic rod other end is hinged with gas support upper end supporting plate.
As a further improvement, multiple floors are respectively set in the both ends for being vertically connected with straight tube, it is every two adjacent
Gas cylinder limit space can be formed between floor.
As a further improvement, the structure further includes rocket rocket body cabin, rocket rocket body cabin be arranged with outside multiple gas cylinders
Portion.
As a further improvement, rocket rocket body cabin is in-flanges structure, petal-shaped is processed into lower end.
As a further improvement, rocket rocket body cabin includes shell, multiple main supports are set on the inside of described shell one end
Seat, the gas support lower end supporting plate are connected with multiple main support bases, and gas support upper end supporting plate passes through multiple limits
Seat is connected with case inside.
As a further improvement, the limit base is loose-leaf structure, one end is connected with case inside, the other end and gas cylinder
Pedestal upper end supporting plate is connected.
As a further improvement, gas cylinder, which places notch, is set as 5 notches.
As a further improvement, being set as pasting aviation rubber slab on the inside of the hoop component.
The present invention solves the difficulty of existing high volume accounting rocket rocket body bay section installation high pressure gas cylinder group, realizes that cold air pushes away
Into effective fixed and installation of the high pressure gas tank in bay section of system.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention.
Fig. 2 is the structural schematic diagram of hoop component of the present invention.
Fig. 3 is the structural schematic diagram of gas support of the present invention.
Fig. 4 is the structural schematic diagram in rocket rocket body of the present invention cabin.
Fig. 5 is the structural schematic diagram of limit base of the present invention.
Fig. 6 is invention components installation procedure schematic diagram.
Specific embodiment
A specific embodiment of the invention is made a detailed explanation with reference to the accompanying drawing.
As shown in figures 1 to 6, a kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure, which includes rocket arrow
Body cabin 10, gas support 1 and hoop component 2, the gas support 1 include gas support lower end supporting plate 3, gas support upper end
It is vertically connected with straight tube 5 between supporting plate 4 and its gas support lower end supporting plate 3 and gas support upper end supporting plate 4, described connects up and down
Multiple floors 9 are respectively set in the both ends for connecing straight tube 5, can form gas cylinder limit space between every two adjacent floor 9；The gas
5 gas cylinders are set on the supporting plate of bottle rack lower end and place notch, and the corresponding gas cylinder of gas support upper end supporting plate 4 is placed and is arranged on notch
Lateral Displacement notch places gas cylinder 7, rocket rocket body cabin by the mating reaction that gas cylinder places notch and lateral Displacement notch
10 be arranged with outside 5 gas cylinders；Rocket rocket body cabin 10 is in-flanges structure, and petal-shaped is processed into lower end；The rocket
Rocket body cabin 10 includes shell, is arranged multiple main support bases 11 on the inside of described shell one end, the gas support lower end supporting plate 3 with
Multiple main support bases 11 are connected, and gas support upper end supporting plate 4 is connected by multiple limit bases 12 with case inside；Described
The upper end of gas cylinder 7 is clamped hoop component 2, and the one or both ends of the hoop component 2 and one end of telescopic rod 8 are hinged, institute
8 other end of telescopic rod stated is hinged with gas support upper end supporting plate 4.It is set as pasting aviation rubber on the inside of the hoop component
Offset plate.
Claims (8)
1. a kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure, it is characterised in that: the structure includes gas support
And hoop component, the gas support include under gas support lower end supporting plate, gas support upper end supporting plate and its gas support
It is vertically connected with straight tube between end supporting plate and gas support upper end supporting plate, multiple gas cylinders are set on the supporting plate of the gas support lower end
Notch is placed, and gas support upper end supporting plate corresponds to gas cylinder and places and lateral Displacement notch is arranged on notch, passes through gas cylinder placing groove
Gas cylinder is placed in the mating reaction of mouth and lateral Displacement notch, and the upper end of the gas cylinder is clamped hoop component, the clip group
The one or both ends of part and one end of telescopic rod are hinged, and the telescopic rod other end is mutually cut with scissors with gas support upper end supporting plate
It connects.
2. a kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure according to claim 1, it is characterised in that:
Multiple floors are respectively set in the both ends for being vertically connected with straight tube, and it is empty that gas cylinder limit can be formed between every two adjacent floor
Between.
3. a kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure according to claim 1, it is characterised in that:
The structure further includes rocket rocket body cabin, rocket rocket body cabin be arranged with outside multiple gas cylinders.
4. a kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure according to claim 3, it is characterised in that:
Rocket rocket body cabin is in-flanges structure, and petal-shaped is processed into lower end.
5. a kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure according to claim 3, it is characterised in that:
Rocket rocket body cabin includes shell, and multiple main support bases, the gas support lower end branch are arranged on the inside of described shell one end
Plate is connected with multiple main support bases, and gas support upper end supporting plate is connected by multiple limit bases with case inside.
6. a kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure according to claim 5, it is characterised in that:
The limit base is loose-leaf structure, and one end is connected with case inside, and the other end is connected with gas support upper end supporting plate.
7. a kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure described in -6 any one according to claim 1,
It is characterized by: gas cylinder, which places notch, is set as 5 notches.
8. a kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure described in -6 any one according to claim 1,
It is characterized by: aviation rubber slab is pasted in the inside setting of the hoop component.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910031516.5A CN109515754A (en) | 2019-01-14 | 2019-01-14 | A kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910031516.5A CN109515754A (en) | 2019-01-14 | 2019-01-14 | A kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109515754A true CN109515754A (en) | 2019-03-26 |
Family
ID=65798944
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910031516.5A Pending CN109515754A (en) | 2019-01-14 | 2019-01-14 | A kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109515754A (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030015623A1 (en) * | 2001-07-19 | 2003-01-23 | Aerojet-General Corporation | Solid rocket motor bolted thrust takeout structure |
| US20140290212A1 (en) * | 2013-03-27 | 2014-10-02 | Lockheed Martin Corporation | Reactants sprayed into plasma flow for rocket propulsion |
| CN204279982U (en) * | 2014-09-26 | 2015-04-22 | 中国运载火箭技术研究院 | A kind of at orbit aerocraft tank connecting device |
| CN105620775A (en) * | 2014-10-31 | 2016-06-01 | 中国航空工业集团公司西安飞机设计研究所 | Heading installation structure for gas cylinder of aircraft |
| CN105674053A (en) * | 2014-11-19 | 2016-06-15 | 中国航空工业集团公司西安飞机设计研究所 | Lateral-directional single-hoop mounting structure for airplane gas cylinder |
| CN107284695A (en) * | 2017-06-19 | 2017-10-24 | 北京零壹空间科技有限公司 | A kind of tank fixing device for installing |
| CN206750165U (en) * | 2017-05-03 | 2017-12-15 | 陕西飞机工业（集团）有限公司 | A kind of mounting bracket of aircraft bottle |
| CN107651221A (en) * | 2017-07-28 | 2018-02-02 | 上海宇航系统工程研究所 | The strong maneuverable spacecraft configuration of hollow big carrying |
| CN109094820A (en) * | 2018-07-11 | 2018-12-28 | 上海空间推进研究所 | Ring plate stove formula composite material main force support structure part |
| CN209467353U (en) * | 2019-01-14 | 2019-10-08 | 北京星际荣耀空间科技有限公司 | A kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure |
-
2019
- 2019-01-14 CN CN201910031516.5A patent/CN109515754A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030015623A1 (en) * | 2001-07-19 | 2003-01-23 | Aerojet-General Corporation | Solid rocket motor bolted thrust takeout structure |
| US20140290212A1 (en) * | 2013-03-27 | 2014-10-02 | Lockheed Martin Corporation | Reactants sprayed into plasma flow for rocket propulsion |
| CN204279982U (en) * | 2014-09-26 | 2015-04-22 | 中国运载火箭技术研究院 | A kind of at orbit aerocraft tank connecting device |
| CN105620775A (en) * | 2014-10-31 | 2016-06-01 | 中国航空工业集团公司西安飞机设计研究所 | Heading installation structure for gas cylinder of aircraft |
| CN105674053A (en) * | 2014-11-19 | 2016-06-15 | 中国航空工业集团公司西安飞机设计研究所 | Lateral-directional single-hoop mounting structure for airplane gas cylinder |
| CN206750165U (en) * | 2017-05-03 | 2017-12-15 | 陕西飞机工业（集团）有限公司 | A kind of mounting bracket of aircraft bottle |
| CN107284695A (en) * | 2017-06-19 | 2017-10-24 | 北京零壹空间科技有限公司 | A kind of tank fixing device for installing |
| CN107651221A (en) * | 2017-07-28 | 2018-02-02 | 上海宇航系统工程研究所 | The strong maneuverable spacecraft configuration of hollow big carrying |
| CN109094820A (en) * | 2018-07-11 | 2018-12-28 | 上海空间推进研究所 | Ring plate stove formula composite material main force support structure part |
| CN209467353U (en) * | 2019-01-14 | 2019-10-08 | 北京星际荣耀空间科技有限公司 | A kind of high volume accounting rocket rocket body bay section gas cylinders group mounting structure |
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