RU94022040A - Gyrocoordinator of homing head - Google Patents

Gyrocoordinator of homing head

Info

Publication number
RU94022040A
RU94022040A RU94022040/28A RU94022040A RU94022040A RU 94022040 A RU94022040 A RU 94022040A RU 94022040/28 A RU94022040/28 A RU 94022040/28A RU 94022040 A RU94022040 A RU 94022040A RU 94022040 A RU94022040 A RU 94022040A
Authority
RU
Russia
Prior art keywords
rotor
value
gyrocoordinator
homing
bearings
Prior art date
Application number
RU94022040/28A
Other languages
Russian (ru)
Other versions
RU2077797C1 (en
Inventor
В.И. Бабичев
В.Я. Филимонов
Е.Я. Померанец
Г.Д. Розинов
Original Assignee
Конструкторское бюро приборостроения
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 Конструкторское бюро приборостроения filed Critical Конструкторское бюро приборостроения
Priority to RU94022040/28A priority Critical patent/RU2077797C1/en
Publication of RU94022040A publication Critical patent/RU94022040A/en
Application granted granted Critical
Publication of RU2077797C1 publication Critical patent/RU2077797C1/en

Links

Abstract

FIELD: rocket engineering. SUBSTANCE: invention refers to homing heads used in control systems of artillery guided projectiles. Gyrocoordinator of homing head of artillery guided projectile includes rotor put on internal gimbal suspension. Its internal frame carries optical system. Front end face surface of rotor has ring supporting element. Collar made on threaded bushing is mounted with clearance with respect to supporting element in direction of action of launch acceleration. Bushing is attached to internal frame of gimbal suspension which outer diameter is bigger than internal diameter is bigger than internal diameter of ring supporting element. Value of clearance is determined from relation δ < Δ < δ+δ, where Δ is clearance value; d is maximum value of play of rotor bearings; dis value of zone of elastic deformations of rotor bearings. Rigidity of external frame in direction of rotor axle does not exceed value R/Δ, where Ris permissible action on bearings of gimbal suspension. EFFECT: increased impact strength of gyrocoordinator of homing head of artillery projectile by unloading bearings of rotor and gimbal suspension against inertial load of internal frame and elements mounted in it.

Claims (1)

Относится к области управляемых снарядов, а именно - к головкам самонаведения, используемым в системах управления артиллерийских управляемых снарядов. Целью изобретения является повышение ударной прочности гирокоординатора головки самонаведения артиллерийского управляемого снаряда путем разгрузки опор ротора и карданова подвеса от инерционной нагрузки внутренней рамки и установленных на ней элементов. В гирокоординаторе головки самонаведения артиллерийского управляемого снаряда, содержащем ротор на внутреннем кардановом подвесе, во внутренней рамке которого установлена оптическая система, на передней торцевой поверхности ротора выполнен кольцевой опорный элемент, относительно которого с зазором в направлении действия стартового ускорения установлен бурт, выполненный на резьбовой втулке, закрепленной на внутренней рамке карданова подвеса, наружный диаметр которого больше внутреннего диаметра кольцевого опорного элемента, величина зазора определена из соотношения, приведенного в описании.Refers to the area of guided missiles, namely, to the homing heads used in control systems of artillery guided shells. The aim of the invention is to increase the impact strength of the gyrocoordinator of the homing artillery guided projectile by unloading the supports of the rotor and cardan suspension from the inertial load of the inner frame and the elements installed on it. In the gyrocoordinator of the homing of an artillery guided projectile containing a rotor on an internal cardan suspension, an optical system is installed in the inner frame of the ring, an annular support element is made on the front end surface of the rotor relative to which a shoulder is made on the threaded sleeve with a gap in the direction of the starting acceleration, fixed on the inner frame of the cardan suspension, the outer diameter of which is larger than the inner diameter of the annular supporting element, ina gap determined from the relationship given in the description.
RU94022040/28A 1994-06-16 1994-06-16 GYRO-COORDINATOR RU2077797C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU94022040/28A RU2077797C1 (en) 1994-06-16 1994-06-16 GYRO-COORDINATOR

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU94022040/28A RU2077797C1 (en) 1994-06-16 1994-06-16 GYRO-COORDINATOR

Publications (2)

Publication Number Publication Date
RU94022040A true RU94022040A (en) 1996-06-20
RU2077797C1 RU2077797C1 (en) 1997-04-20

Family

ID=48434773

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94022040/28A RU2077797C1 (en) 1994-06-16 1994-06-16 GYRO-COORDINATOR

Country Status (1)

Country Link
RU (1) RU2077797C1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2621218C1 (en) * 2016-06-14 2017-06-01 Акционерное общество "Конструкторское бюро приборостроения им. академика А.Г. Шипунова" Gyrocoordinator of target-seeking head
RU181497U1 (en) * 2017-04-17 2018-07-17 Публичное акционерное общество "Тульский оружейный завод" CONTROLLED APPLIANCE

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2621218C1 (en) * 2016-06-14 2017-06-01 Акционерное общество "Конструкторское бюро приборостроения им. академика А.Г. Шипунова" Gyrocoordinator of target-seeking head
RU181497U1 (en) * 2017-04-17 2018-07-17 Публичное акционерное общество "Тульский оружейный завод" CONTROLLED APPLIANCE

Also Published As

Publication number Publication date
RU2077797C1 (en) 1997-04-20

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Legal Events

Date Code Title Description
PC43 Official registration of the transfer of the exclusive right without contract for inventions

Effective date: 20121213