CN2421705Y - Weightlessness simulator - Google Patents

Weightlessness simulator Download PDF

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Publication number
CN2421705Y
CN2421705Y CN 00229584 CN00229584U CN2421705Y CN 2421705 Y CN2421705 Y CN 2421705Y CN 00229584 CN00229584 CN 00229584 CN 00229584 U CN00229584 U CN 00229584U CN 2421705 Y CN2421705 Y CN 2421705Y
Authority
CN
China
Prior art keywords
air
simulator
work chamber
cabin
null
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
Application number
CN 00229584
Other languages
Chinese (zh)
Inventor
杜江
孙元泉
杨一军
李麓
蔡浩
张继华
Original Assignee
No701 Research Inst No7 Inst China Shipping Heavy Industry Group Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by No701 Research Inst No7 Inst China Shipping Heavy Industry Group Corp filed Critical No701 Research Inst No7 Inst China Shipping Heavy Industry Group Corp
Priority to CN 00229584 priority Critical patent/CN2421705Y/en
Application granted granted Critical
Publication of CN2421705Y publication Critical patent/CN2421705Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a weightlessness simulator which comprises a work cabin, wherein, an air inlet is arranged on the lower end of the work cabin and is communicated with an air current power cabin, an air outlet is arranged on the upper end of the work cabin and is communicated with a circular air passage and an exhaust hole, and the lower end of the circular air passage is communicated with the air current power cabin. The simulator uses the principle of vertical wind tunnels, the air current power cabin provides wind power from 120 to 160 kilometers per hour, and the work cabin converts the potential energy of air into upward dynamic buoyancy for overcoming gravity and generating weightlessness. The utility model can be used in amusement places, military training, bailout training and popular science education.

Description

Null-g simulator
The utility model belongs to analogue means, suspension analogue means when being specifically related to people or object weightlessness.
Because human body or object are subjected to gravitational effect.Thereby human body or object can not be suspended in the air.And at present at recreation ground, aspects such as military training, parachuting training, section's general education education all do not have document openly to plant the weightless suspension analogue means of wind-tunnel.
The purpose of this utility model is to utilize a kind of weightless flight device of wind-tunnel principle design.
For realizing the purpose of this utility model, the inventor proposes following technical scheme, null-g simulator comprises work chamber, air inlet is established in the work chamber lower end, air inlet is connected with the air-flow piggyback pod, work chamber upper end sets out the air port, air outlet and circulation air path and vent port mutually, the circulation air path lower end communicates with the air-flow piggyback pod.
This simulator utilizes the vertical wind tunnel principle, and the air-flow piggyback pod provides the wind-force of 120~160 kilometers speed per hours, and work chamber becomes the potential energy of gas into moving buoyancy upwards, thereby overcome gravity, produce weightlessness, the people is risen up in the air, make human body suspension, lifting to experience the weightlessness of space sensation.This simulator can be used for recreation ground, military training, parachuting training and Popular Science Education.
Accompanying drawing null-g simulator configuration diagram.
Embodiment
The outward appearance of the null-g simulator of present embodiment is a space shuttle and three pieces of rockets, and one piece of main rocket (fuel compartment) and two pieces of side rockets (roll booster) are interconnected between them, and space shuttle is operation pulpit (not shown).
The main as shown in the figure rocket of simulator structure 1 stage casing is a work chamber 2, and catch net 3 is established on work chamber 2 tops, and wall and bottom are provided with flexibility neonychium 4 all around, establishes guiding messenger 5 in the work chamber 2.Air inlet 6 is established in work chamber 2 lower ends, and air inlet 6 is connected with air-flow piggyback pod 7.
Air-flow piggyback pod 7 comprises the blower fan 12 by cushion socket 13 location, the diffusion tube 10 that communicates with main air duct 11, and rectiblock 9 and wind collection 8 are established in diffusion tube 10 tops, and wind collection 8 outlets are over against the air inlet 6 of work chamber 24.
The air outlet 14 of work chamber 2 upper ends communicates with circulation air path 15 and vent port 16, exhaust box 20.Circulation air path 15 is a section of side rocket 19, and its lower end communicates with air-flow piggyback pod 7, is provided with fair water fin 17 in it.Also establish fair water fin 18 in the main air duct 11.

Claims (4)

1, null-g simulator, it comprises work chamber, it is characterized in that the work chamber lower end establishes air inlet, and air inlet is connected with the air-flow piggyback pod, and the work chamber upper end sets out the air port, and air outlet communicates with circulation air path and vent port, and the circulation air path lower end communicates with the air-flow piggyback pod.
2, null-g simulator according to claim 1 is characterized in that the air-flow piggyback pod comprises the blower fan by the cushion socket location, the diffusion tube that communicates with main air duct, and diffusion tube top is provided with rectiblock and wind collection, and the wind collection outlet is over against the air inlet of work chamber.
3, weightless according to claim 1 mould is with device, it is characterized in that work chamber top establishes catch net, and wall and bottom are provided with the flexibility neonychium all around.
4, as null-g simulator as described in the claim 1,2, it is characterized in that being provided with fair water fin in the circulation air path, establish fair water fin in the main air duct.
CN 00229584 2000-04-05 2000-04-05 Weightlessness simulator Expired - Fee Related CN2421705Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 00229584 CN2421705Y (en) 2000-04-05 2000-04-05 Weightlessness simulator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 00229584 CN2421705Y (en) 2000-04-05 2000-04-05 Weightlessness simulator

Publications (1)

Publication Number Publication Date
CN2421705Y true CN2421705Y (en) 2001-02-28

Family

ID=33592840

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 00229584 Expired - Fee Related CN2421705Y (en) 2000-04-05 2000-04-05 Weightlessness simulator

Country Status (1)

Country Link
CN (1) CN2421705Y (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105405333A (en) * 2015-12-08 2016-03-16 中国人民解放军空军空降兵学院 Parachuting escape simulation training system and escape simulation training method thereof
CN106601065A (en) * 2017-02-02 2017-04-26 佛山市三水区希望火炬教育科技有限公司 Underwater suspended cabin for simulating space weightless state special for teenager science popularization education
CN106652729A (en) * 2017-03-17 2017-05-10 佛山市三水区希望火炬教育科技有限公司 Special simulation capsule system for national defense and aerospace education of youngsters
CN107481577A (en) * 2017-08-23 2017-12-15 芜湖超源力工业设计有限公司 A kind of space flight training weightless flight device
WO2020211508A1 (en) * 2019-04-16 2020-10-22 于毅欣 Immersive suspension method and apparatus based on virtual reality technology

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105405333A (en) * 2015-12-08 2016-03-16 中国人民解放军空军空降兵学院 Parachuting escape simulation training system and escape simulation training method thereof
CN106601065A (en) * 2017-02-02 2017-04-26 佛山市三水区希望火炬教育科技有限公司 Underwater suspended cabin for simulating space weightless state special for teenager science popularization education
CN106652729A (en) * 2017-03-17 2017-05-10 佛山市三水区希望火炬教育科技有限公司 Special simulation capsule system for national defense and aerospace education of youngsters
CN107481577A (en) * 2017-08-23 2017-12-15 芜湖超源力工业设计有限公司 A kind of space flight training weightless flight device
WO2020211508A1 (en) * 2019-04-16 2020-10-22 于毅欣 Immersive suspension method and apparatus based on virtual reality technology

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
ASS Succession or assignment of patent right

Owner name: DU JIANG

Free format text: FORMER OWNER: NO.701 INST., NO.7 ACADEMY, CHINA SHIPPING HEAVY INDUSTRY GROUP CORP.

Effective date: 20041224

C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20041224

Address after: 430060 Hubei city of Wuhan province Wuchang Ziyang Road No. 268

Patentee after: Du Jiang

Address before: 430060 Hubei city of Wuhan province Wuchang Ziyang Road No. 268

Patentee before: No.701 Research Inst., No.7 Inst., China Shipping Heavy Industry Group Corp.

C19 Lapse of patent right due to non-payment of the annual fee
CF01 Termination of patent right due to non-payment of annual fee