CN104990457A - Direct drive type infrared imaging seeker position marker - Google Patents
Direct drive type infrared imaging seeker position marker Download PDFInfo
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- CN104990457A CN104990457A CN201510369382.XA CN201510369382A CN104990457A CN 104990457 A CN104990457 A CN 104990457A CN 201510369382 A CN201510369382 A CN 201510369382A CN 104990457 A CN104990457 A CN 104990457A
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- inner frame
- infrared imaging
- optical module
- position marker
- type infrared
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Abstract
The invention discloses a direct drive type infrared imaging seeker position marker. The direct drive type infrared imaging seeker position marker comprises a support, brackets, an inner frame, an optical assembly, an outer drive system and an inner drive system. The two brackets are fixed to the support in parallel. The inner frame is rotationally connected with vertical plates. The optical assembly is arranged in the inner frame and rotationally connected with the inner frame. The outer drive system drives the inner frame to rotate. The inner drive system drives the optical assembly to rotate. A rotary shaft of the inner frame is arranged perpendicularly to a rotary shaft of the optical assembly. Two first limiting pins are arranged on each bracket. The limiting pins limit the motion trail of the inner frame. The optical assembly is used for acquiring and transmitting images in real time.
Description
Technical field
The present invention relates to a kind of guidance technology, particularly a kind of direct-drive type Infrared Imaging Seeker position marker.
Background technology
Can form powerful, intensive fire net after rocket bomb transmitting, the firepower of effective compacting the other side, forms reliable support to the operation of ground forces.But owing to not adopting guidance technology, rocket projectile closeness is poor, scatters large, be difficult to effective striking point target, be mainly used in eliminating the other side's cluster armored target and the effective strength with lightweight armor protection.Since the nineties in 20th century, along with the development of precision guided weapon, the particularly development of precise guidance shell, conventional rocket projectile guidanceization is one of important development direction becoming following precision guided munition gradually also, and presents the vigorous growth impetus.
Rocket projectile guidanceization is the focus of guided munition development in recent years, and many countries are all in equipment in various degree or development, and the guidance technology of employing is various, and installation site and the guidance laws of guidance component are not quite similar.U.S.'s research starting in this respect comparatively early, and relies on it in the technical advantage in guidance field, by the rocket projectile of routine and bomb, has repacked plunderer's guided missile and JDAM bomb into, and has been used in the war in Iraq.Russia and some countries of Europe also expand research, are in experimental stage.Analyze from the guided rocket bullet of having shaped at present and developing, mainly apply semi-active laser guided, INS/GPS integrated navigation guidance technology; Less to the infrared imaging guidance technical research of rocket projectile both at home and abroad.
Summary of the invention
The object of the present invention is to provide a kind of direct-drive type Infrared Imaging Seeker position marker, the object of the detection of a target can be completed by automatic rotation.
A kind of direct-drive type Infrared Imaging Seeker position marker, comprises bearing, support, inner frame, optical module, outer drive system, interior drive system.Described support has two pieces, is parallelly fixed on bearing; Inner frame and riser are rotationally connected; Optical module to be placed in inner frame and to be rotationally connected with inner frame; Outer drive systems inner frame rotates; Interior drive systems optical module rotates; The turning cylinder of described inner frame is vertical with the turning cylinder of optical module to be arranged; Described support is provided with two the first spacer pins, described first spacer pin restriction inner frame movement locus; The effect of described optical module is carry out Real-time Collection to image and transmit.
Described outer drive system comprises and is arranged at outer motor on two pieces of parallel brackets and volta potential device respectively; Described outer motor shaft is connected with support respectively by bearing with volta potential device axle, and outer motor shaft is connected with inner frame with volta potential device axle.
Adopt above-mentioned direct-drive type Infrared Imaging Seeker position marker, described interior drive system comprises and is arranged at the relative both sides of inner frame respectively and motor and an inner potential device in be connected with optical module one.
Adopt above-mentioned direct-drive type Infrared Imaging Seeker position marker, inner frame is fixed one second spacer pin, optical component housings is provided with housing is provided with and coordinates with the second spacer pin and to limit the arc-shaped limit groove of optical module movement locus, described stopper slot and the second spacer pin are slidably matched, the radian of stopper slot is [30 °, 50 °].
The present invention compared with prior art has the following advantages: detection range is large, has accurate round-the-clock function, can work double tides, is a kind of guidance system of the round-the-clock detection of standard that can work under adverse weather condition; (2) Infrared Imaging Seeker has under various complicated tactical environment image processor, catches, identifies and the ability of tracking target, can realize " after launching no matter ".
Below in conjunction with Figure of description, the present invention is described further.
Accompanying drawing explanation
Fig. 1 is the main diagram of overall structure of the present invention.
Fig. 2 is the left diagram of overall structure of the present invention.
Fig. 3 is inner frame of the present invention and the first spacer pin combination schematic diagram.
Fig. 4 is position-limit mechanism schematic diagram in the present invention.
Fig. 5 is torque motor structure schematic diagram of the present invention.
Fig. 6 is optical assembly structure schematic diagram of the present invention.
Detailed description of the invention
Composition graphs 1 and Fig. 2, a kind of direct-drive type Infrared Imaging Seeker position marker, is made up of optical system and gyro system, comprises bearing 1, support 1-1, inner frame 9, optical module 5, outer drive system, interior drive system.Uniform six screwed holes of bearing 1 floor peripheral are connected with body; Described support 1-1 has two pieces, and parallel is fixed on bearing 1; Inner frame 9 and riser 1-1 are rotationally connected; Optical module 5 to be placed in inner frame 9 and to be rotationally connected with inner frame 9; Outer drive systems inner frame 9 rotates; Interior drive systems optical module 5 rotates; The turning cylinder of described inner frame 9 is vertical with the turning cylinder of optical module 5 to be arranged; Described support 1-1 is provided with two the first spacer pins 4, and described first spacer pin 4 limits inner frame 9 movement locus; The effect of described optical module 5 is carry out Real-time Collection to image and transmit.
Above-mentioned outer drive system and interior drive system form gyro system, make optical module can rotate the observation of certain limit.
Composition graphs 1, Fig. 2, Fig. 3, described outer drive system comprises and is arranged at outer motor 3 on two pieces of parallel bracket 1-1 and volta potential device 7 respectively; Described outer motor shaft 18 is fixed on support 1-1 by outer motor casing 2, and described volta potential device 7 is fixed on support 1-1 by outer motor casing 6; Described outer motor shaft 18 is connected with support 1-1 respectively by bearing 18 with volta potential device axle 20, and outer motor shaft 18 is connected with inner frame 9 with volta potential device axle 20.Inner frame 9 angle that motor shaft 18 and volta potential device axle 20 rotate for rotating shaft in addition under the restriction of the first spacer pin 4 is [-20 °, 20 °].
Composition graphs 1, Fig. 2 and Fig. 4, described interior drive system comprise be arranged at respectively inner frame 9 relatively both sides and be connected with optical module 5 one in motor 12 and an inner potential device 8; Described interior motor 12 is fixed on inner frame 9 by interior motor casing 11, and inner potential device 8 is fixed on inner frame 9 by inner potential device shell 8.Described interior motor shaft 10 is connected with inner frame 9 respectively by bearing with inner potential device axle 15, and interior motor shaft 10 is connected with optical module 5 with inner potential device axle 15.Inner frame 9 is fixed one second spacer pin 26, optical module 5 shell is provided with housing is provided with and coordinates with the second spacer pin 26 and to limit the arc-shaped limit groove 25 of optical module 5 movement locus, described stopper slot 25 and the second spacer pin 26 are slidably matched, the radian of stopper slot 25 is [30 °, 50 °].
Composition graphs 6, optical module comprises infrared lens 5-1, infrared lens is threadedly attached to upper cover 5-2, and upper cover is screwed on shell 5-3, and circuit board 5-5 is interconnected by plug-in unit button 5-6, focal plane 5-5 is fixing on circuit boards, circuit board hold-down screw 5-8 is connected to lower cover 5-4
Outer motor 3 and interior motor 12 are direct current torque motor, and torque motor comprises stator 28 and rotor 27, and stator 28 is fixed with motor housing, and rotor 27 is connected with motor shaft by screw, transmitting torque.
First balancing weight 19 is set bottom described optical module 5.
Second balancing weight 16 is set outside described inner potential device 8.
According to above-described embodiment, the performance parameter that the present invention reaches is as follows:
Operating temperature-10 DEG C to+50 DEG C;
The maximum outside diameter 124mm of frame mechanism, be highly no more than 150mm, weight is no more than 1500g;
Camera lens optical axis around the slewing area of interior motor shaft, outer motor rotation axis be ± 20 °;
Under being the condition of 0.18s in the acceleration 30g that withstands shocks, attack time, the unbalanced moments that in complete machine, housing motor bears is less than corresponding motor rated output torque 10%.
Claims (8)
1. a direct-drive type Infrared Imaging Seeker position marker, is characterized in that, comprising:
Bearing (1),
Be fixed on two pieces of parallel brackets (1-1) on bearing (1),
The inner frame (9) be rotationally connected with riser (1-1),
To be placed in inner frame (9) and the optical module (5) be rotationally connected with inner frame (9),
Drive the outer drive system that inner frame (9) rotates,
Drive the interior drive system that optical module (5) rotates;
The turning cylinder of described inner frame (9) is vertical with the turning cylinder of optical module (5) to be arranged;
Described support (1-1) is provided with two the first spacer pins (4), described first spacer pin (4) restriction inner frame (9) movement locus;
The effect of described optical module (5) is carry out Real-time Collection to image and transmit.
2. direct-drive type Infrared Imaging Seeker position marker according to claim 1, is characterized in that, described outer drive system comprises and is arranged at outer motor (3) on two pieces of parallel brackets (1-1) and volta potential device (7) respectively; Described outer motor shaft (18) is connected with support (1-1) respectively by bearing with volta potential device axle (20), and outer motor shaft (18) is connected with inner frame (9) with volta potential device axle (20).
3. direct-drive type Infrared Imaging Seeker position marker according to claim 2, it is characterized in that, inner frame (9) under the restriction of the first spacer pin (4) beyond motor shaft (18) and volta potential device axle (20) angle of rotating for rotating shaft be [-20 °, 20 °].
4. direct-drive type Infrared Imaging Seeker position marker according to claim 1, it is characterized in that, described interior drive system comprise be arranged at respectively inner frame (9) relatively both sides and be connected with optical module (5) one in motor (12) and an inner potential device (8); Described interior motor shaft (10) is connected with inner frame (9) respectively by bearing with inner potential device axle (15), and interior motor shaft (10) is connected with optical module (5) with inner potential device axle (15).
5. direct-drive type Infrared Imaging Seeker position marker according to claim 4, it is characterized in that, inner frame (9) is fixed one second spacer pin (26), optical module (5) shell is provided with housing is provided with and coordinates with the second spacer pin (26) and to limit the arc-shaped limit groove (25) of optical module (5) movement locus, described stopper slot (25) and the second spacer pin (26) are slidably matched, the radian of stopper slot (25) is [30 °, 50 °].
6. the direct-drive type Infrared Imaging Seeker position marker according to claim 2 or 4, is characterized in that, outer motor (3) and interior motor (12) are direct current torque motor.
7. direct-drive type Infrared Imaging Seeker position marker according to claim 1, is characterized in that, described optical module (5) bottom arranges the first balancing weight (19).
8. direct-drive type Infrared Imaging Seeker position marker according to claim 4, is characterized in that, arranges the second balancing weight (16) outside described inner potential device (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510369382.XA CN104990457A (en) | 2015-06-29 | 2015-06-29 | Direct drive type infrared imaging seeker position marker |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510369382.XA CN104990457A (en) | 2015-06-29 | 2015-06-29 | Direct drive type infrared imaging seeker position marker |
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| CN104990457A true CN104990457A (en) | 2015-10-21 |
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| CN201510369382.XA Pending CN104990457A (en) | 2015-06-29 | 2015-06-29 | Direct drive type infrared imaging seeker position marker |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106092088A (en) * | 2016-06-16 | 2016-11-09 | 上海航天控制技术研究所 | A kind of three axle Photoelectric Tracking and Aiming mechanisms based on rotating carrier |
| CN106482590A (en) * | 2016-11-15 | 2017-03-08 | 河北汉光重工有限责任公司 | A kind of miniaturization, lightweight Seeker Coordinator |
| CN106524833A (en) * | 2016-11-29 | 2017-03-22 | 贵州大学 | Target space angle position simulator and application method |
| CN106569205A (en) * | 2016-11-01 | 2017-04-19 | 河北汉光重工有限责任公司 | Co-aperture infrared/radar composite seeker |
| CN106927066A (en) * | 2017-03-20 | 2017-07-07 | 上海航天控制技术研究所 | A kind of five axle position markers |
| CN108100304A (en) * | 2017-12-20 | 2018-06-01 | 贵州航天电子科技有限公司 | A kind of object space Angle Position simulator |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2718501Y (en) * | 2003-12-15 | 2005-08-17 | 中国科学院西安光学精密机械研究所 | 2D precision tracking rotary table |
| CN101320280A (en) * | 2008-06-03 | 2008-12-10 | 中山市科力高自动化设备有限公司 | Two-coordinate torque feedback controller |
| CN101662668A (en) * | 2009-09-17 | 2010-03-03 | 天津市恩普电子设备有限公司 | Infrared light scanning omni-directional spherical pan head |
| CN102410785A (en) * | 2011-12-13 | 2012-04-11 | 林德福 | Turntable for semi-physical simulation of laser terminally guided projectile |
| CN102556359A (en) * | 2010-12-28 | 2012-07-11 | 中国科学院沈阳自动化研究所 | Airborne air-photo image-stabilizing cloud deck of unmanned aerial vehicle |
| CN102981510A (en) * | 2011-09-02 | 2013-03-20 | 中国航天科工集团第二研究院二０七所 | Small high-precision staring infrared electro-optical stabilization and tracking platform |
| CN202953150U (en) * | 2012-12-12 | 2013-05-29 | 山东省科学院海洋仪器仪表研究所 | Onboard laser imaging sight-stabilizing platform |
| CN203250853U (en) * | 2013-02-27 | 2013-10-23 | 宁波森富机电制造有限公司 | Three-axis stabilization mobile tracking mount of shipborne satellite antenna |
| CN203964781U (en) * | 2014-07-11 | 2014-11-26 | 金陵科技学院 | A kind of three axle artificial rotary tables |
| CN104360479A (en) * | 2014-11-27 | 2015-02-18 | 天津天地伟业数码科技有限公司 | Automatic laser emergence angle and direction adjusting device |
-
2015
- 2015-06-29 CN CN201510369382.XA patent/CN104990457A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2718501Y (en) * | 2003-12-15 | 2005-08-17 | 中国科学院西安光学精密机械研究所 | 2D precision tracking rotary table |
| CN101320280A (en) * | 2008-06-03 | 2008-12-10 | 中山市科力高自动化设备有限公司 | Two-coordinate torque feedback controller |
| CN101662668A (en) * | 2009-09-17 | 2010-03-03 | 天津市恩普电子设备有限公司 | Infrared light scanning omni-directional spherical pan head |
| CN102556359A (en) * | 2010-12-28 | 2012-07-11 | 中国科学院沈阳自动化研究所 | Airborne air-photo image-stabilizing cloud deck of unmanned aerial vehicle |
| CN102981510A (en) * | 2011-09-02 | 2013-03-20 | 中国航天科工集团第二研究院二０七所 | Small high-precision staring infrared electro-optical stabilization and tracking platform |
| CN102410785A (en) * | 2011-12-13 | 2012-04-11 | 林德福 | Turntable for semi-physical simulation of laser terminally guided projectile |
| CN202953150U (en) * | 2012-12-12 | 2013-05-29 | 山东省科学院海洋仪器仪表研究所 | Onboard laser imaging sight-stabilizing platform |
| CN203250853U (en) * | 2013-02-27 | 2013-10-23 | 宁波森富机电制造有限公司 | Three-axis stabilization mobile tracking mount of shipborne satellite antenna |
| CN203964781U (en) * | 2014-07-11 | 2014-11-26 | 金陵科技学院 | A kind of three axle artificial rotary tables |
| CN104360479A (en) * | 2014-11-27 | 2015-02-18 | 天津天地伟业数码科技有限公司 | Automatic laser emergence angle and direction adjusting device |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106092088A (en) * | 2016-06-16 | 2016-11-09 | 上海航天控制技术研究所 | A kind of three axle Photoelectric Tracking and Aiming mechanisms based on rotating carrier |
| CN106092088B (en) * | 2016-06-16 | 2019-04-05 | 上海航天控制技术研究所 | A kind of three axis Photoelectric Tracking and Aiming mechanisms based on rotating carrier |
| CN106569205A (en) * | 2016-11-01 | 2017-04-19 | 河北汉光重工有限责任公司 | Co-aperture infrared/radar composite seeker |
| CN106482590A (en) * | 2016-11-15 | 2017-03-08 | 河北汉光重工有限责任公司 | A kind of miniaturization, lightweight Seeker Coordinator |
| CN106524833A (en) * | 2016-11-29 | 2017-03-22 | 贵州大学 | Target space angle position simulator and application method |
| CN106927066A (en) * | 2017-03-20 | 2017-07-07 | 上海航天控制技术研究所 | A kind of five axle position markers |
| CN106927066B (en) * | 2017-03-20 | 2019-03-26 | 上海航天控制技术研究所 | A kind of five axis position markers |
| CN108100304A (en) * | 2017-12-20 | 2018-06-01 | 贵州航天电子科技有限公司 | A kind of object space Angle Position simulator |
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Application publication date: 20151021 |
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