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61. 发明专利

JP4112804B2 Spin stabilization flying object 有权
公开(公告)号：JP4112804B2
公开(公告)日：2008-07-02
申请号：JP2000511030
申请日：1998-08-24
申请人：プライメックステクノロジーズ,インコーポレイテッド
发明人：ホワイト、チャールズ、オー
IPC分类号： F42B8/12 , F42B10/48 , F42B10/22 , F42B10/26 , F42B10/54
CPC分类号： F42B10/22 , F42B10/48 , F42B10/54

62. 发明专利

JP3980021B2 Rotation angle measurement method of controlling the rotation flying object 有权
公开(公告)号：JP3980021B2
公开(公告)日：2007-09-19
申请号：JP2004286645
申请日：2004-09-30
申请人：多摩川精機株式会社
发明人：恒雄杉浦
IPC分类号： F42B10/26 , F42B10/66 , F42B15/01 , G01B7/30

63. 发明专利

JP3758257B2 Flying object of the control device 失效
公开(公告)号：JP3758257B2
公开(公告)日：2006-03-22
申请号：JP31503596
申请日：1996-11-26
申请人：三菱電機株式会社
发明人：誠一米山
IPC分类号： F42B10/26 , F42B15/01 , F42B10/66 , G05D1/12

64. 发明专利

JP2000065565A DEVICE FOR MEASURING ROTARY ANGLE OF ROTARY MISSILE AND ITS MEASURING METHOD 失效
公开(公告)号：JP2000065565A
公开(公告)日：2000-03-03
申请号：JP23582498
申请日：1998-08-21
申请人： KOMATSU MFG CO LTD
发明人： ONISHI TETSUYA , YAMAZAKI KATSUHIRO
IPC分类号： F42B10/26 , F42B10/66 , G01C1/00
摘要： PROBLEM TO BE SOLVED: To obtain a device and method for measuring a rotary angle of a rotary missile which is excellent in G-resistance and low-priced with a simple structure. SOLUTION: In a device and method for measuring a rotary angle of a rotary missile, an infrared rays detecting means 20 is provided in a rotary missile such as a cannonball, and emission energy surrounding the rotary missile is detected by this infrared rays detecting means 20, and also a reference position is calculated by a reference position calculating means 14 from a difference of a detection value based on a rotary angle of this emission energy, and the rotary angle of the rotary missile is calculated by a rotary angle calculating means 15 from comparison with this reference position, and the rotary angle of the rotary missile is measured.

65. 发明专利

JPH11264699A OPPOSING APPARATUS FOR DEPOLYING INTERCEPTING ELEMENT FROM SPIN STABILIZED ROCKET 失效
公开(公告)号：JPH11264699A
公开(公告)日：1999-09-28
申请号：JP34925698
申请日：1998-11-02
申请人： TRW INC
发明人： DAVID P SMITH , JANE M LYNN
IPC分类号： F41H11/02 , F41F7/00 , F42B10/26 , F42B12/60 , F42B15/01
摘要： PROBLEM TO BE SOLVED: To provide a defending unit against an enemy missile of a low production cost by reducing a danger to friend soldier in a battle area. SOLUTION: A non-explosive intercepting element 14 contained in a payload part 17 by a slidable sleeve assembly 16 retracted in a nose direction by a driving mechanism 21 is assembled as a nose of a spin stabilized rocket 10. At the time of shooting, a trigger releasing assembly 46 is operated after a programmed predetermined delay. A driving rod 26 is released by an operation of the releasing assembly. The sleeve assembly is urged by an urging fore of a compressed spring unit 30, moved forward together with a sleeve member 22. Thus, the intercepting element is separately projected at a predetermined angular speed by a centrifugal force of the rocket to form an intercepting cloud by a non-explosive element.

66. 发明专利

JP2743120B2 失效
公开(公告)号：JP2743120B2
公开(公告)日：1998-04-22
申请号：JP51599493
申请日：1993-11-26
IPC分类号： F42B10/26

67. 发明专利

JPH05187800A MISSILE 失效
公开(公告)号：JPH05187800A
公开(公告)日：1993-07-27
申请号：JP443992
申请日：1992-01-14
申请人： TOSHIBA CORP
发明人： UMIBE MASAHISA
IPC分类号： F42B10/26 , F42B12/02 , F42B15/01 , G01S13/88
摘要： PURPOSE:To obtain a missile in which directionality of a nose power can be incorporated in any direction with a simple structure. CONSTITUTION:A directional nose having one initiator cylinder is provided at a position apart from a center in a missile. Further, the missile has a circuit 21 for so calculating a rolling angle and a rolling direction of a body that directional nose power from target direction information collected by a seeker 20 coincides with a target direction.

68. 发明专利

JPH03221795A S, C BULLET 失效
公开(公告)号：JPH03221795A
公开(公告)日：1991-09-30
申请号：JP1605790
申请日：1990-01-29
申请人： SENDAI SHIGERU
发明人： SENDAI SHIGERU
IPC分类号： F42B10/26
摘要： PURPOSE:To improve the shooting range and shooting accuracy of a bullet by providing four grooves in the rear part of the bullet as a blade and setting the blade portion slantingly with respect to a straightforward direction. CONSTITUTION:A bullet 1 has a blade 2 and a groove 3, and the blade 2 is set slantingly with respect to the direction of the advancement of the bullet. The bullet 1 has in itself lift by undergoing pneumatic resistance by the blade. Further, it flies in a natural rotational motion to a target to improve shooting accuracy.

69. 发明专利

JPH0225698A MEASURING DEVICE FOR POSITION OF ROLL 失效
公开(公告)号：JPH0225698A
公开(公告)日：1990-01-29
申请号：JP12270789
申请日：1989-05-16
申请人： BOFORS AB
发明人： RARUSUUERIKU SUKAIERURUNDO
IPC分类号： F41G7/00 , F41G7/24 , F41G7/30 , F42B10/26
摘要： PURPOSE: To transmit angular information in a simple and definite mode to a projectile, a missile, or the like, by an arrangement wherein a polarized radiation includes at least two mutually phase-interlocked radiation components of specified wavelength relationship superposed to have an asymmetric waveform. CONSTITUTION: A transmitter 2 having direct relationship with a launching point transmits a polarized electromagnetic radiation and a projectile has a receiving antenna 3 directed rearward. Based on a signal being produced when the polarized plane of radiation transmitting the roll position of the projectile corresponds to the polarized plane of the receiver, the roll position of the projectile can be measured at a relatively high accuracy but ambiguity of one half revolution is incident thereto. In order to achieve total ambiguity, the polarized microwave radiation includes two mutually fixed components of the wavelength relationship of 2:1 and/or multiples thereof. An asymmetric waveform is obtained when two transmitted microwave components are superposed. Ambiguity can be eliminated by the an asymmetric curve and the roll position of the projectile can be determined definitely.

70. 实用新型

JPS6317999U 失效
公开(公告)号：JPS6317999U
公开(公告)日：1988-02-05
申请号：JP11246186
申请日：1986-07-22
IPC分类号： F42B10/26 , F42B15/047

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