CN202126318U - 阻尼弹簧载荷感觉器 - Google Patents

阻尼弹簧载荷感觉器 Download PDF

Info

Publication number
CN202126318U
CN202126318U CN2011202489692U CN201120248969U CN202126318U CN 202126318 U CN202126318 U CN 202126318U CN 2011202489692 U CN2011202489692 U CN 2011202489692U CN 201120248969 U CN201120248969 U CN 201120248969U CN 202126318 U CN202126318 U CN 202126318U
Authority
CN
China
Prior art keywords
damping
spring
load sensor
spring load
piston
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
CN2011202489692U
Other languages
English (en)
Inventor
马起跃
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BEIJING ROCKY AEROSPACE TECHNOLOGY DEVELOPMENT CO., LTD.
Original Assignee
BEIJING SJC DESIGN TECHNOLOGY Co Ltd
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 BEIJING SJC DESIGN TECHNOLOGY Co Ltd filed Critical BEIJING SJC DESIGN TECHNOLOGY Co Ltd
Priority to CN2011202489692U priority Critical patent/CN202126318U/zh
Application granted granted Critical
Publication of CN202126318U publication Critical patent/CN202126318U/zh
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Fluid-Damping Devices (AREA)

Abstract

本实用新型公开了阻尼弹簧载荷感觉器,由弹簧载荷感觉器和阻尼筒组成,弹簧载荷感觉器的活塞上有阻尼孔,弹簧载荷感觉器内部装满阻尼油,阻尼孔均布在活塞上,阻尼孔大小可调。本实用新型简化结构,提高无源控制的操纵杆力模拟的逼真度。

Description

阻尼弹簧载荷感觉器
技术领域
本实用新型涉及弹簧载荷感觉器,尤其是阻尼弹簧载荷感觉器。
背景技术
地面飞行模拟器用的无源控制的操纵杆力,是用弹簧载荷感觉器。为有阻尼力的感觉,一般是在弹簧载荷感觉器旁并联一个阻尼筒。存在的主要问题是阻尼力不可调,结构复杂,模拟逼真度不高。
实用新型内容
本实用新型提供了阻尼弹簧载荷感觉器,它简化了结构,提高无源控制的操纵杆力模拟的逼真度。
本实用新型提供了阻尼弹簧载荷感觉器,由弹簧载荷感觉器和阻尼筒组成,弹簧载荷感觉器的活塞上有阻尼孔,弹簧载荷感觉器内部装满阻尼油。
优选方案为阻尼孔均布在活塞上。
优选方案为阻尼孔大小可调。
本实用新型提供了阻尼弹簧载荷感觉器,结构简洁,没有干扰,阻尼孔大小可调,模拟逼真度高,也可用于汽车或其他装置模拟操纵力的产生。
附图说明
图1本实用新型结构图;
具体实施方式
下面结合附图及具体实施方式,对本实用新型作进一步详细的说明。
实施例1
阻尼弹簧载荷感觉器,由弹簧载荷感觉器(1)和阻尼筒(2)组成,弹簧载荷感觉器的活塞上(3)有阻尼孔(4),弹簧载荷感觉器内部装满阻尼油,阻尼孔均布在活塞上,阻尼孔大小可调。操纵杆运动时带动活塞运动,压缩弹簧,产生弹簧力;同时液体流过阻尼孔,根据操纵杆的运动速度产生相应的阻尼力。弹簧载荷感觉器和阻尼筒合而为一后,结构简洁,没有干扰,阻尼孔大小可调,模拟逼真度高。也可用于汽车或其他装置模拟操纵力的产生。
以上内容是结合本实用新型的结构和工作过程对其所作的进一步详细说明,不能认定本实用新型的具体实施只局限于这些说明。对于本实用新型所属技术领域的普通技术人员来说,在不脱离本实用新型构思的前提下,还可以做出若干简单推演或替换,都应当视为属于本实用新型的保护范围。

Claims (3)

1.阻尼弹簧载荷感觉器,由弹簧载荷感觉器和阻尼筒组成,其特征在于:弹簧载荷感觉器的活塞上有阻尼孔,弹簧载荷感觉器内部装满阻尼油。
2.根据权利要求1所述的阻尼弹簧载荷感觉器,其特征在于:所述的阻尼孔均布在活塞上。
3.根据权利要求1或2所述的阻尼弹簧载荷感觉器,其特征在于:所述的阻尼孔大小可调。
CN2011202489692U 2011-07-15 2011-07-15 阻尼弹簧载荷感觉器 Expired - Fee Related CN202126318U (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011202489692U CN202126318U (zh) 2011-07-15 2011-07-15 阻尼弹簧载荷感觉器

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011202489692U CN202126318U (zh) 2011-07-15 2011-07-15 阻尼弹簧载荷感觉器

Publications (1)

Publication Number Publication Date
CN202126318U true CN202126318U (zh) 2012-01-25

Family

ID=45489383

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2011202489692U Expired - Fee Related CN202126318U (zh) 2011-07-15 2011-07-15 阻尼弹簧载荷感觉器

Country Status (1)

Country Link
CN (1) CN202126318U (zh)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106601070A (zh) * 2016-12-16 2017-04-26 中仿智能科技(上海)股份有限公司 一种飞行器侧杆模拟装置

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106601070A (zh) * 2016-12-16 2017-04-26 中仿智能科技(上海)股份有限公司 一种飞行器侧杆模拟装置

Similar Documents

Publication Publication Date Title
CN204592129U (zh) 用于航拍器的云台减震装置
CN104123404B (zh) 一种起落架建模方法
Zonta Medieval Hebrew translations of philosophical and scientific texts: A chronological table
CN102779438B (zh) 一种模拟飞机全动作仿真飞行机械执行系统
CN104298804A (zh) 一种飞行载荷设计方法
ATE539959T1 (de) Vorrichtung zum filtern der vibrationen die von einem flugzeug, insbesondere einem helikopter, an ein gerät übertragen werden
CN201086822Y (zh) 无人飞机起落架后跪式减震装置
CN202126318U (zh) 阻尼弹簧载荷感觉器
CN202502629U (zh) 飞行人员躯体正负压训练装置
CN103366614A (zh) 飞行人员躯体正负压训练装置
CN203989892U (zh) 基于3-rcu并联机构的被动4d座椅
CN103640694A (zh) 一种缓冲减载拦阻钩钩臂
CN203260222U (zh) 一种用于航海器和飞行器的三自由度模拟运动平台
CN203552497U (zh) 液压弹射训练模拟器
CN204137320U (zh) 无人植保机起落架
CN202275529U (zh) 六自由度运动模拟器
CN205302714U (zh) 一种用于飞行模拟器座舱的液压振动装置
CN104792490A (zh) 一种风洞颤振模型外挂物侧摆频率和偏航频率解耦装置
CN205770133U (zh) 起落架减震装置
CN205140373U (zh) 一种飞行模拟器仿真中央杆操纵机构
CN204215592U (zh) 一种仿真抖震平台
CN202690862U (zh) 起落架缓冲器活门装置
CN206826934U (zh) 一种无人机螺旋翼的伸缩型保护装置
CN202280779U (zh) 具有较强抗震性的汽车前减振器
Shi Improved landing-gear design for flexible airplane

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: BEIJING HANGYU RONGKANG TECHNOLOGY DEVELOPMENT CO.

Free format text: FORMER OWNER: BEIJING SJC DESIGN TECHNOLOGY CO., LTD.

Effective date: 20140708

C41 Transfer of patent application or patent right or utility model
COR Change of bibliographic data

Free format text: CORRECT: ADDRESS; FROM: 100029 XICHENG, BEIJING TO: 100040 SHIJINGSHAN, BEIJING

TR01 Transfer of patent right

Effective date of registration: 20140708

Address after: 100040, room 3, building 3, building 30, 8306 Xing Xing street, Beijing, Shijingshan District

Patentee after: BEIJING ROCKY AEROSPACE TECHNOLOGY DEVELOPMENT CO., LTD.

Address before: 100029, room 419, Indira Steiker building, No. 25, middle third ring road, Xicheng District, Beijing

Patentee before: Beijing SJC Design 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: 20120125

Termination date: 20200715