专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明专利

JP4560206B2 Guided missile for the rudder locking device 有权
公开(公告)号：JP4560206B2
公开(公告)日：2010-10-13
申请号：JP2000384410
申请日：2000-12-18
申请人：エルエフカー・レンクフルッグケルペルシステム・ゲゼルシャフト・ミット・ベシュレンクテル・ハフツング
发明人：ウォルター・ヘッツァー , エルンスト・レンツ
IPC分类号： F42B10/62 , F42B10/64
CPC分类号： F42B10/64

2. 发明专利

JP2003262500A DIRECTION AND ATTITUDE CONTROL DEVICE FOR FLYING OBJECT 审中-公开
公开(公告)号：JP2003262500A
公开(公告)日：2003-09-19
申请号：JP2002062877
申请日：2002-03-08
申请人： MITSUBISHI HEAVY IND LTD
发明人： SHINOHARA SATOSHI , NAKANISHI TERUO
IPC分类号： F42B10/66 , B64C15/02 , F42B10/62
摘要： PROBLEM TO BE SOLVED: To provide a control device solving nonconformity of a conventional control device, wherein the direction and the attitude are controlled by an aerodynamic steering vane and a thrust deflection body to be disposed after completing the control, such as being unusable for the flying body whose aerodynamic steering vane and thrust deflection body are separated from each other, in the direction and attitude control device for a flying object interlocking and simultaneously controlling the direction and the attitude of the flying object. SOLUTION: This direction and attitude control device for the flying body is provided with a support fixture which is provided in the outer circumferential surface of a machine body for installing the thrust deflection part and pivotally supports the rear end part of a joint swinging following to the aerodynamic vane, a support mount installed in the outer circumference of the thrust deflection vane and pivotally supporting an arm fixed to a rotary shaft of the thrust deflection vane, and a long transmission element disposed between the joint and the arm, transmitting the swinging of the aerodynamic steering vane to the thrust force deflection vane, and composed of a soft material. Thereby, this control device can be used for the flying body whose thrust deflection part and aerodynamic steering part are disposed in a largely separated state in the machine body axial direction and control the direction and the attitude in simultaneously controlling the aerodynamic steering vane with the thrust deflection body without impairing the control by the aerodynamic steering part in a regular flying. COPYRIGHT: (C)2003,JPO

3. 发明专利

JP3252360B2 失效
公开(公告)号：JP3252360B2
公开(公告)日：2002-02-04
申请号：JP3622791
申请日：1991-03-01
IPC分类号： F42B10/60 , F42B10/62 , F42B10/66

4. 发明专利

JP2001174197A RUDDER LOCKING SYSTEM FOR GUIDED MISSILE 失效
公开(公告)号：JP2001174197A
公开(公告)日：2001-06-29
申请号：JP2000384410
申请日：2000-12-18
申请人： LFK GMBH
发明人： WALTER HETZER , ERNST LENZ
IPC分类号： F42B10/62 , F42B10/64
摘要： PROBLEM TO BE SOLVED: To provide a rudder locking system for a guided missile, which system not only meets necessary spatial conditions but also is adapted to mechanical and thermal loads generated at a cruising speed of Mach 4. SOLUTION: In the rudder locking system for a guided missile, a rudder blade R is rotatably supported by an attachment fixed to the missile body on the axis of the rudder and which can be turned by a rubber driving lever. An attachment B comprises a bearing portion B1 having an at least partially cylindrical outside configuration B2 and a concave portion B3. The concave portion B3 engages with the missile-side end portion W1 of a rudder shaft W, which portion is formed in correspondence to the concave portion B3. Further the concave portion B3 and the rudder shaft W1 taper off in diameters d1 and d2 toward the missile, respectively, to provide a configuration advantageous for inserting a ramjet driven missile into a carrier having a concave portion of 41 mm wide for a conventional missile rubber blade.

5. 实用新型

JPH0429274Y2 失效
公开(公告)号：JPH0429274Y2
公开(公告)日：1992-07-15
申请号：JP16234984
申请日：1984-10-29
IPC分类号： B64C13/50 , F42B10/62 , F42B10/64 , G05D1/02 , G05D1/10

6. 实用新型

JPS6179796U JPS6179796U - 失效
公开(公告)号：JPS6179796U
公开(公告)日：1986-05-28
申请号：JP16118884
申请日：1984-10-26
IPC分类号： B64C9/02 , B64C13/24 , F42B10/62 , F42B10/64 , F42B15/027

7. 实用新型

JPS60111898U 失效
公开(公告)号：JPS60111898U
公开(公告)日：1985-07-29
申请号：JP20418483
申请日：1983-12-28
IPC分类号： B64C9/00 , F42B10/62 , F42B15/027

8. 发明专利

JPS6078898A MISSILE 失效
公开(公告)号：JPS6078898A
公开(公告)日：1985-05-04
申请号：JP18726483
申请日：1983-10-06
申请人： MITSUBISHI ELECTRIC CORP
发明人： KUROSAKI RIYUUJIROU
IPC分类号： B64C5/10 , B64C5/00 , F42B10/62

9. 发明专利

JPS58120099A GUIDANCE MISSILE 失效
公开(公告)号：JPS58120099A
公开(公告)日：1983-07-16
申请号：JP315682
申请日：1982-01-12
申请人： MITSUBISHI ELECTRIC CORP
发明人： YAMANE HIDEO
IPC分类号： F41G7/20 , F42B10/62

10. 发明专利

JPS5896309A AUTOMATIC STEERING SYSTEM FOR MISSILE 失效
公开(公告)号：JPS5896309A
公开(公告)日：1983-06-08
申请号：JP19505781
申请日：1981-12-03
申请人： MITSUBISHI ELECTRIC CORP
发明人： KIMURA KAZUMI
IPC分类号： B64C13/18 , F42B10/62 , F42B15/01 , G05D1/12
摘要： PURPOSE:To allow automatic steering over wide altitude and speed ranges and to improve the design flexibility of an automatic steering device by varying the value of the parameter of a control compensating filter according to the altitude and speed. CONSTITUTION:A missile-body sensor unit 1, digital computer 2, and angle detector for measuring the steering angle of a steering wing 4 are used to estimate the gain constant of the body transfer function of a missile and the value of the coefficient parameter on real-time basis. On the basis of the estimated values of said gain constant and coefficient parameter, the computer 2 performs the parameter calculation of a control compensating filter with time to feed the angular speed signal of the missile body back, and thus performs control so that a phase margin and a crossover angular frequency on the Bode diagram of the damping factor of a body damper loop closed-loop transfer function and position control loop open-loop function coincide with preset request values.

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式