CN105965207B - A kind of spherical tanks and its forming method - Google Patents
A kind of spherical tanks and its forming method Download PDFInfo
- Publication number
- CN105965207B CN105965207B CN201610345476.8A CN201610345476A CN105965207B CN 105965207 B CN105965207 B CN 105965207B CN 201610345476 A CN201610345476 A CN 201610345476A CN 105965207 B CN105965207 B CN 105965207B
- Authority
- CN
- China
- Prior art keywords
- crescent
- main body
- reinforcing rib
- cydariform main
- cydariform
- 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.)
- Expired - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
Landscapes
- Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Business, Economics & Management (AREA)
- Physics & Mathematics (AREA)
- Educational Administration (AREA)
- Educational Technology (AREA)
- General Physics & Mathematics (AREA)
- Arc Welding In General (AREA)
- Wind Motors (AREA)
Abstract
The present invention relates to simulator accessory technical fields, especially a kind of spherical tanks and its forming method, cydariform main body including spherical shape, cydariform main body includes shell and frame, and for outer cover suit on frame outer surface, shell left and right sides are respectively arranged with crescent component group, method is as follows: bending profile, it is cut by laser reinforcing rib, plasma cut water tower, cydariform main body and crescent component；Equal leg angle, channel steel and steel plate are welded with to spoke, wheel hub, crescent component, reinforcing rib in cydariform main body, cutting hatch door is carried out using plasma process；Deburring, Puttying, primer spray finally carry out topcoating.The invention enables cabin operation is more stable; simple process, arc-shaped structure stress are preferable; processing cost economy, crack resistance are high, make its bonding strength height, structure simple using plasma cut and carbon-dioxide protecting, manufacture easy to produce, while having very strong practicability.
Description
Technical field
The present invention relates to simulator accessory technical field, especially a kind of spherical tanks and its forming method.
Background technique
Flying virtual simulator from broadly, be exactly for simulated flight device fly machine.It such as simulates aircraft, lead
The device of the flights such as bullet, satellite, spaceship can all be referred to as flight simulator.It is can to reappear aircraft and aerial ring
Border and the simulator for being able to carry out operation.For in the narrow sense, exactly it is used to virtual analog aircraft flight and structure compares
The more complete device of sophisticated functions.If its aerolog relatively simple for structure and less function, it is known as flying
Training aids.Using flying virtual simulator, flight training is carried out, has and improves training effectiveness, saves training cost, guarantees flight
Safety, the advantages that reducing environmental pollution, therefore, whether Air Branch or space flight department, all increasingly pay attention to playing flight
The effect of virtual simulator.
Traditional spherical tanks, be all by bolt or it is common be welded, under the circumference of the high-speed rotation, bolt
Be easy to loosen, it is common be welded on high speed rotary motion in the case where the problem of also splitting, can all cause so certain
Safe suffering.The defect of traditional handicraft complexity higher cost is low corresponding with the configuration of the present invention is simple, manufacturing cost.
Summary of the invention
In view of the above-mentioned deficiencies in the prior art, the purpose of the present invention is to provide a kind of spherical tanks and its molding sides
Method, to solve the problems, such as traditional handicraft complexity higher cost.
In order to achieve the above objectives, the technical solution adopted by the present invention is that: a kind of spherical tanks, the cydariform master including spherical shape
Body, the cydariform main body include shell and frame, and the outer cover suit is on frame outer surface, the shell left and right sides point
It is not provided with the first crescent component group and the second crescent component group, the first crescent component group and the second crescent group
Part group is respectively welded on shell, and the shell front side is provided with hatch door, the frame by reinforcing rib in cabin, angle steel, channel steel and
Spoke is welded.
As preferred: the first crescent component group include two round pot shapes the first crescent moon parts assembling welding and
At the second crescent component group includes that the second crescent moon parts assembling of two round pot shapes is welded.
As preferred: the frame top and the bottom are respectively formed with first wheel and the second wheel hub, the shell upper and lower side point
It is not provided with the first air hole and the second air hole.
As preferred: the middle position of two the first crescent moon parts assemblings welding is formed with first shaft hole, two second month
The middle position of dental assembly assembly welding is formed with the second axis hole.
As preferred: the bulkhead of the cydariform main body uses stainless steel material system with a thickness of 1-5mm, the cydariform main body
At.
Another technical solution used in the present invention: a kind of spherical tanks forming method, the cydariform main body forming method:
(1) bending profile is cut by laser reinforcing rib, plasma cut water tower, cydariform main body and crescent component；(2) by equal leg angle,
Channel steel and steel plate are welded with spoke, wheel hub, crescent component, reinforcing rib in cydariform main body, and wherein welding manner uses dioxy
Change carbon protection weldering；(3) cutting hatch door is carried out using plasma process；(4) deburring, Puttying, primer spray finally carry out spray plane
Paint.
As preferred: the specification of the angle steel is 50*50*4, and the reinforcing rib in the cabin uses with a thickness of 6-8mm, width
For the steel plate of 25mm；The steel plate that the crescent component uses with a thickness of 3mm.
As preferred: the crescent group reinforcement member weld length 10-15mm, be spaced 60mm, the cydariform main body with
Reinforcing rib interval 150mm in cabin.
As preferred: being used between the channel steel and equal leg angle and be fully welded technique.
Beneficial effect of the present invention, cydariform main body two sides thin-walled of the invention is reinforced using profile, using spoke architecture, with type
Material connects, the arc-shaped reinforcing rib of design in cabin；Cydariform main body is connect with crescent component with screw, and side need to only dismantle a spiral shell
Dismantling can be completed in nail, so that cabin operation is more stable, simple process, arc-shaped structure stress are preferable, and processing cost economy resists
Fragility is high, makes its bonding strength height, structure simple using plasma cut and carbon-dioxide protecting, manufacture easy to produce, simultaneously
With very strong practicability.
Detailed description of the invention
Fig. 1 is flow chart of the invention；
Fig. 2 is structural schematic diagram of the invention；
Fig. 3 is main view of the invention；
Fig. 4 is left view of the invention；
Fig. 5 is perspective structure schematic diagram of the invention.
Specific embodiment
The embodiment of the present invention is described in detail below in conjunction with attached drawing, but the present invention can be defined by the claims
Implement with the multitude of different ways of covering.
As shown in Figures 1 to 5, a kind of spherical tanks,
Embodiment 1: the cydariform main body 1 including spherical shape, the cydariform main body 1 include shell 2 and frame 3, the shell 1
It is wrapped on the outer surface of frame 2,2 left and right sides of shell are respectively arranged with the first crescent component group 4 and second month
Thread form component group 13, the first crescent component group 4 and the second crescent component group 13 are respectively welded on shell 2, described
Hatch door 14 is provided on front side of shell 2, the frame 3 is welded by reinforcing rib 11, angle steel 12, channel steel and spoke 10 in cabin.
First crescent component group 4 includes that two 5 assembly of dental assembly in first month of round pot shape are welded, and described second month
13 groups of thread form component include that the second crescent moon parts assembling of two round pot shapes is welded.3 left and right part of frame is respectively formed with
One wheel hub 9 and the second wheel hub 15,2 upper and lower side of shell are respectively arranged with the first air hole 7 and the second air hole 8.Described in two
First month dental assembly 5 is assembled and middle position is formed with first shaft hole 17, two the second crescent moon parts assemblings and interposition
It sets and is formed with the second axis hole.The bulkhead of the cydariform main body 1 uses stainless steel material system with a thickness of 1-5mm, the cydariform main body 1
At.
The two sides thin-walled of cydariform main body is reinforced using profile, using spoke architecture, connect with profile, designs in cabin arc-shaped
Reinforcing rib；Cydariform main body is connect with crescent component with screw, and dismantling can be completed in the side screw that need to only dismantle.
A kind of spherical tanks forming method, the cydariform main body forming method: (1) bending profile is cut by laser reinforcing rib, etc.
Ion cuts water tower, cydariform main body and crescent component；(2) equal leg angle, channel steel and steel plate are welded in cydariform main body
Spoke, wheel hub, crescent component, reinforcing rib, wherein welding manner uses carbon-dioxide arc welding；(3) plasma process is used
Carry out cutting hatch door；(4) deburring, Puttying, primer spray finally carry out topcoating.
Further, the specification of the angle steel is 50*50*4, and the reinforcing rib in the cabin uses with a thickness of 6-8mm, width
For the steel plate of 25mm；The steel plate that the crescent component uses with a thickness of 3mm.
Further, the crescent group reinforcement member weld length 10-15mm, be spaced 60mm, the cydariform main body with
Reinforcing rib interval 150mm in cabin.
Further, it is used between the channel steel and equal leg angle and is fully welded technique.
Embodiment 2: the water tower of some spherical shapes is selected to be used as spherical tanks main body and equal leg angle, channel steel and steel plate conduct first
Then auxiliary part carries out cutting treating selvedge, equal leg angle, channel steel and steel plate are welded with spoke, wheel hub, the moon in cydariform main body
Thread form component, reinforcing rib complete the base configuration of spherical tanks.Cutting hatch door is finally carried out using plasma process；Deburring is scraped
Putty, primer spray finally carry out topcoating.
Crescent component reinforcing rib uses 3mm thick steel plate, width 35mm, all using laser cutting molding；Any direction is thrown
The bounce of shadow circle is not greater than 10mm；Two wheel hub concentricitys must not be lower than 2mm, need to be guaranteed using welding tooling), reinforcing rib.
Due to the adoption of the above technical scheme, the invention enables cabins to run more stable, simple process, arc-shaped structure stress
Preferably, processing cost economy, crack resistance are high, make its bonding strength height, structure letter using plasma cut and carbon-dioxide protecting
It is single, it relatively manufactures, while there is very strong practicability.
The above description is only a preferred embodiment of the present invention, is not intended to limit the scope of the invention, all utilizations
Equivalent structure or equivalent flow shift made by description of the invention and accompanying drawing content is applied directly or indirectly in other correlations
Technical field, be included within the scope of the present invention.
Claims (2)
1. a kind of spherical tanks, it is characterised in that: the cydariform main body including spherical shape, the cydariform main body include shell and frame,
For the outer cover suit on frame outer surface, the shell left and right sides are respectively arranged with the first crescent component group and second
Crescent component group, the first crescent component group and the second crescent component composition do not weld on the shell, the shell
Front side is provided with hatch door, and the frame is welded by reinforcing rib, angle steel, channel steel and spoke in cabin；The first crescent group
Part group includes that the first crescent moon parts assembling of two round pot shapes is welded, and the second crescent component group includes two round pots
Second crescent moon parts assembling of shape is welded；The frame top and the bottom are respectively formed with first wheel and the second wheel hub, described
Shell upper and lower side is respectively arranged with the first air hole and the second air hole；The middle position of two the first crescent moon parts assemblings welding
It is formed with first shaft hole, the middle position of two the second crescent moon parts assemblings welding is formed with the second axis hole；The cydariform main body
Bulkhead with a thickness of 1-5mm, the cydariform main body is made of stainless steel.
2. a kind of forming method of spherical tanks according to claim 1, it is characterised in that: cydariform main body molding side
Method: (1) bending profile is cut by laser reinforcing rib, plasma cut water tower, cydariform main body and crescent component；(2) corners such as general
Steel, channel steel and steel plate are welded with spoke, wheel hub, crescent component, reinforcing rib in cydariform main body, and wherein welding manner uses two
Carbonoxide protection weldering；(3) cutting hatch door is carried out using plasma process；(4) deburring, Puttying, primer spray, are finally sprayed
Finishing coat；
The specification of the angle steel is 50*50*4, and the reinforcing rib in the cabin uses with a thickness of 6-8mm, width as the steel plate of 25mm；
The steel plate that the crescent component uses with a thickness of 3mm；The crescent group reinforcement member weld length 10-15mm, interval
Reinforcing rib interval 150mm in 60mm, the cydariform main body and cabin；It is used between the channel steel and equal leg angle and is fully welded technique.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610345476.8A CN105965207B (en) | 2016-05-22 | 2016-05-22 | A kind of spherical tanks and its forming method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610345476.8A CN105965207B (en) | 2016-05-22 | 2016-05-22 | A kind of spherical tanks and its forming method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105965207A CN105965207A (en) | 2016-09-28 |
| CN105965207B true CN105965207B (en) | 2019-04-16 |
Family
ID=56956265
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610345476.8A Expired - Fee Related CN105965207B (en) | 2016-05-22 | 2016-05-22 | A kind of spherical tanks and its forming method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105965207B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113182748B (en) * | 2021-04-02 | 2023-02-28 | 北京卫星制造厂有限公司 | Spherical shell structure welding supporting tool and welding method for synchronous assembly fractal tailor-welding |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5490784A (en) * | 1993-10-29 | 1996-02-13 | Carmein; David E. E. | Virtual reality system with enhanced sensory apparatus |
| CN101221698B (en) * | 2008-01-22 | 2012-03-28 | 深圳市机场股份有限公司 | Airplane simulation cabin butted with special vehicle in airport |
| CN103192178A (en) * | 2012-01-04 | 2013-07-10 | 夏致俊 | Combined-type laser cutting machine |
| CN203437824U (en) * | 2013-08-30 | 2014-02-19 | 江西制氧机有限公司 | Semiautomatic cutting and welding combination tool of pressure vessel end socket |
| CN204759813U (en) * | 2015-06-15 | 2015-11-11 | 天津飞联科技有限公司 | Novel semi -closed emulation cockpit |
| CN105014199B (en) * | 2015-07-23 | 2017-03-15 | 西安交通大学 | A kind of CO2The transfer manner of droplet analogy method of gas shielded arc welding simulator |
| CN204926595U (en) * | 2015-09-08 | 2015-12-30 | 重庆幻羽科技有限公司 | Virtual reality simulator with three degrees of freedom |
| CN205959455U (en) * | 2016-05-22 | 2017-02-15 | 成都航训科技有限责任公司 | High -efficient low -cost eco -power spherical cabin |
-
2016
- 2016-05-22 CN CN201610345476.8A patent/CN105965207B/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN105965207A (en) | 2016-09-28 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US20180340492A1 (en) | Method for manufacturing and assembly of a thrust reverser cascade | |
| WO2019103830A3 (en) | Methods for manufacturing wind turbine rotor blade panels having printed grid structures | |
| CN105965207B (en) | A kind of spherical tanks and its forming method | |
| US20180015996A1 (en) | Friction stir welded wingtip torque box | |
| KR102618746B1 (en) | Rudder blade with a modular structure, segment for a rudder blade or for an apparatus for improving propulsion and method for manufacturing a rudder blade | |
| JP2017506185A (en) | Reverse thrust device cascade | |
| WO2008108826A3 (en) | Composite aircraft structures with hat stiffeners | |
| CN104260886B (en) | A kind of micro flapping wing air vehicle imitative feather cracking lift-rising mechanism | |
| DE3607789A1 (en) | PADDLE WHEEL FOR A CENTRIFUGAL PUMP OR THE LIKE AND METHOD FOR PRODUCING THE SAME | |
| CN202087447U (en) | Arc-shaped workpiece sprayer | |
| CN104696366B (en) | Hub bearing unit and correlation technique for vehicle | |
| CN205959455U (en) | High -efficient low -cost eco -power spherical cabin | |
| CN111112029B (en) | Multi-color workpiece and method for producing the same | |
| CN204871222U (en) | Top cap assembly structure | |
| JP2000192801A5 (en) | ||
| CN202356234U (en) | Spraying cover for aluminum alloy hub | |
| CN105653763B (en) | Pneumostatic bullet test model design method | |
| CN102358415A (en) | Method for inhibiting rocking movement of aerofoil of wing body assembly by using artificial perturbation of tip part | |
| CN107552341A (en) | A kind of method for the spraying of wheel hub chromatography | |
| CN105772973B (en) | A kind of economic forming method of three-jaw force transmission mechanism | |
| CN209438833U (en) | The pneumatic antifog paint cover of spray gun for paint Duckbill type | |
| KR20180006395A (en) | Modular propulsion unit nozzle | |
| US20160264181A1 (en) | Hemmed body panel for attachment to a body structure | |
| CN104369618A (en) | Vehicle wheel decoration cover | |
| CN105015778B (en) | Amphibious aircraft with wave inhibition groove outer plate |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20191224 Address after: 610041 No.1, floor 3, building 1, No.366, North Hupan Road, Tianfu new area, China (Sichuan) pilot Free Trade Zone, Chengdu, Sichuan Province Patentee after: FAME VISTA TECHNOLOGIES, LTD. Address before: 610000 Sichuan Province, Chengdu city Qingyang District Wen Jia Lu youth entrepreneurship Park 10 C1-2 Patentee before: CHENGDU HANGXUN TECHNOLOGY Co.,Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190416 |