CN108548075A - A kind of mounting structure of integrated controller on carrier - Google Patents
A kind of mounting structure of integrated controller on carrier Download PDFInfo
- Publication number
- CN108548075A CN108548075A CN201810588465.1A CN201810588465A CN108548075A CN 108548075 A CN108548075 A CN 108548075A CN 201810588465 A CN201810588465 A CN 201810588465A CN 108548075 A CN108548075 A CN 108548075A
- Authority
- CN
- China
- Prior art keywords
- carrier
- positioning disk
- controller
- annular
- integrated controller
- 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.)
- Pending
Links
- 238000009434 installation Methods 0.000 claims abstract description 32
- 239000000203 mixture Substances 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000012937 correction Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 241001074085 Scophthalmus aquosus Species 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000007726 management method Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M13/00—Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles
- F16M13/02—Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles for supporting on, or attaching to, an object, e.g. tree, gate, window-frame, cycle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B1/00—Devices for securing together, or preventing relative movement between, constructional elements or machine parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
- F16B2200/99—Fasteners with means for avoiding incorrect assembly or positioning
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Pinball Game Machines (AREA)
Abstract
The invention discloses a kind of mounting structure of integrated controller on carrier, including:Carrier support tube is connected on carrier;The carrier support tube inner wall is equipped with positioning disk installation position;Annular controller positioning disk is annular plate structure, the intermediate position of the annular controller positioning disk is equipped with integrated controller location hole, multiple integrated controller mounting holes are equipped with around integrated controller location hole, multiple integrated controller mounting holes can install fixed integrated controller through connection component;The periphery wall of annular controller positioning disk is equipped with multiple mounting holes, annular controller positioning disk is connect through connection component with the positioning disk installation position of carrier support tube, and the annular controller positioning disk and integrated controller are fixedly mounted on the positioning disk installation position in carrier support tube.The mounting structure can realize on carrier quickly, securely, integrated controller is reliably installed, and while debugging, conveniently removes.
Description
Technical field
The present invention relates to integrated controller field more particularly to a kind of integrated controller are installed on carrier on carrier
Mounting structure.
Background technology
It delivers body computer and uses analogue technique in early stage.Since later stage the 1960s, microelectric technique and number
Technology rapidly develops, and especially after the advent of microprocessor at the beginning of the seventies, application of the digital computer on carrier is increasingly extensive.
Delivery body computer is a kind of, has that small, light weight, low in energy consumption, reliability is high, real-time and be resistant to dislike
The features such as bad environment, generally as the integrated controller of carrier.It for carrier guidance and control, take off before test
Real-time testing calculating and radio communication management after calculating, take off with aiming etc..It is in missile control system by control work(
The requirement of energy is handled in real time;Handling result is sent to the execution part of control system.Such as when for inertial guidance, delivery
Body computer receives the parameter value from inertia device, and corresponding control instruction is calculated by the requirement of inertial guidance function, leads to
The posture for crossing execution unit control carrier, changes the flight path of carrier, it is made to reach target.For another example it is used for carrier figure
As the multi-computer system in matching guidance system, by the guidance in the correlator and inertial guidance system in position correction system
Computer forms.Correlation computer carries out images match using the map image acquired in radar with the Reference Map being previously stored
Processing, determines the instantaneous position of carrier;Guidance computer utilizes the work of the instantaneous position data correction inertial guidance of carrier
Have error, improves guidance precision.Increasingly strict, carrier meter is required with use environment with the raising of carrier performance indicator
Calculation machine is by with better real-time, reliability, Flouride-resistani acid phesphatase and restructural ability, and towards multi-functional, intelligentized direction
Development.Oneself is through being gradually generalized to space flight, aviation, navigation, oil development, geodesic survey, oceanographic survey, the control of geology brill, robot
The fields such as technology and railway, not only occupy highly important status in the modernization of national defense, in national economy every field
Increasingly show its great function.
But inventor has found securely, to be reliably mounted at how by the delivery body computer as integrated controller at present
On carrier, and when needing debugging, conveniently removes, be problem to be solved.
Invention content
Based on the problems of prior art, the object of the present invention is to provide a kind of integrated controllers on carrier
Integrated controller can easily securely, be reliably installed on carrier by mounting structure, and in debugging, conveniently be removed.
The purpose of the present invention is what is be achieved through the following technical solutions:
Embodiment of the present invention provides a kind of mounting structure of integrated controller on carrier, including:
Carrier support tube, annular controller positioning disk and connection component;Wherein,
The carrier support tube is connected on the carrier;
The carrier support tube is hollow cylinder structure, which is equipped with positioning disk installation position,
The positioning disk installation position is equipped with multiple positioning disks and connects through-hole;
The annular controller positioning disk is annular plate structure, and the intermediate position of the annular controller positioning disk is equipped with comprehensive
Hop controller location hole is equipped with multiple integrated controller mounting holes around the integrated controller location hole, the multiple comprehensive
Hop controller mounting hole can install fixed integrated controller through connection component;
The periphery wall of the annular controller positioning disk is equipped with and the positioning disk installation position in the carrier support tube
On each positioning disk connection through-hole multiple mounting holes correspondingly, each mounting hole of the annular controller positioning disk is through connection
Component connect through-hole with the positioning disk of the positioning disk installation position of the carrier support tube and connects one by one, which is determined
Position disk and integrated controller are fixedly mounted on the positioning disk installation position in the carrier support tube.
As seen from the above technical solution provided by the invention, integrated controller provided in an embodiment of the present invention is delivering
Mounting structure on body, advantage are:
By the way that positioning disk installation position is arranged on carrier support tube inner wall, multiple positioning are set on positioning disk installation position
Disk connects through-hole, and annular controller positioning disk is arranged, and is equipped with and carrier branch on the periphery wall of annular controller positioning disk
Each positioning disk connection through-hole multiple mounting holes correspondingly on the positioning disk installation position in cylinder are supportted, due to can be from carrier branch
The annular controller positioning disk in cylinder external connection fixed cylinder is supportted, facilitates and integrated controller is first fixedly mounted on annular controller
After on positioning disk, then annular controller positioning disk is installed to together with integrated controller in carrier support tube together, realized
On carrier quickly, securely, integrated controller is reliably installed, and conveniently removed when needing debugging.
Description of the drawings
In order to illustrate the technical solution of the embodiments of the present invention more clearly, required use in being described below to embodiment
Attached drawing be briefly described, it should be apparent that, drawings in the following description are only some embodiments of the invention, for this
For the those of ordinary skill in field, without creative efforts, other are can also be obtained according to these attached drawings
Attached drawing.
Fig. 1 is mounting structure schematic diagram of the integrated controller provided in an embodiment of the present invention on carrier;
Fig. 2 is another angle schematic diagram of mounting structure of the integrated controller provided in an embodiment of the present invention on carrier;
Fig. 3 is the structural schematic diagram of the carrier support tube of mounting structure provided in an embodiment of the present invention;
In figure:1- carrier support tubes;11- positioning disks installation position;2- annular controller positioning disks;3- connection components;4-
Integrated controller.
Specific implementation mode
With reference to the particular content of the present invention, technical solution in the embodiment of the present invention is clearly and completely retouched
It states, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.Based on the present invention
Embodiment, every other embodiment obtained by those of ordinary skill in the art without making creative efforts,
Belong to protection scope of the present invention.The content not being described in detail in the embodiment of the present invention belongs to professional and technical personnel in the field
The well known prior art.
As shown in Figure 1 to Figure 3, the embodiment of the present invention provides a kind of mounting structure of integrated controller on carrier, packet
It includes:
Carrier support tube, annular controller positioning disk and connection component;Wherein,
The carrier support tube is connected on the carrier;
The carrier support tube is hollow cylinder structure, which is equipped with positioning disk installation position,
The positioning disk installation position is equipped with multiple positioning disks and connects through-hole;
The annular controller positioning disk is annular plate structure, and the intermediate position of the annular controller positioning disk is equipped with comprehensive
Hop controller location hole, the integrated controller location hole can for integrated controller connecting interface end it is exposed, the Comprehensive Control
Multiple integrated controller mounting holes are equipped with around device location hole, the multiple integrated controller mounting hole can pacify through connection component
The fixed integrated controller of dress;
The periphery wall of the annular controller positioning disk is equipped with and the positioning disk installation position in the carrier support tube
On each positioning disk connection through-hole multiple mounting holes correspondingly, each mounting hole of the annular controller positioning disk is through connection
Component connect through-hole with the positioning disk of the positioning disk installation position of the carrier support tube and connects one by one, which is determined
Position disk and integrated controller are fixedly mounted on the positioning disk installation position in the carrier support tube, i.e., annular controller positioning
Disk and integrated controller thereon are fixedly mounted on through connection component on the positioning disk installation position of carrier support tube.
Above-mentioned mounting structure so that positioning disk installation position matches with annular controller positioning disk, and conveniently from delivery
Annular controller positioning disk is fixed on the positioning disk installation position in the carrier support tube outside body support tube, thus side
Integrated controller is installed on annular controller positioning disk after, by annular controller positioning disk and integrated controller together
Be installed in carrier support tube, since carrier support tube is fixed on carrier, realize by integrated controller securely, can
That leans on is installed on carrier.
In above-mentioned mounting structure, carrier support tube is the hollow cylinder structure of straight tube, and the carrier support tube one end is solid
It is scheduled on the carrier, is connected as one with the carrier.
In above-mentioned mounting structure, the positioning disk installation position is located at one end on the carrier support tube inner wall, the positioning
Disk installation position is connected by the annular groove being located on the carrier support tube inner wall with six positioning disks being arranged along the annular groove
Through-hole is constituted, and six positioning disk connection through-holes are divided into three groups, and every group two are disposed adjacent along annular groove distribution.This two two-phase
The mode of neighbour's arrangement positioning disk connection through-hole, can guarantee the stability of annular controller positioning disk after installation.
In above-mentioned mounting structure, the connection component uses multiple screws, and minus screw, plus screw or interior six can be used
Angle screw etc..
The embodiment of the present invention is specifically described in further detail below.
The present invention provides a kind of mounting structure of integrated controller on carrier, which is supported by carrier
Cylinder, the annular compositions such as controller positioning disk and connection component, wherein carrier support tube joins together with carrier, annular control
Device positioning disk processed realizes that the connection of carrier support tube and integrated controller, carrier support tube and annular controller positioning disk are equal
Be made of the material with some strength and rigidity, such as metal material (such as steel, aluminium, copper material), alloy material or its
There is the material of some strength and rigidity to be made for he.
The advantages of mounting structure of the present invention, is:(1) carrier support tube joins together with carrier, and each section connection can
Lean on, securely, good airproof performance, accurate positioning, be easily installed, be well positioned to meet in-site installation and control, reliability is high, efficiency
Height, versatility are good, for ease of maintenaince and replace;(2) annular controller positioning disk realizes carrier support tube and integrated controller
Connection, it is ensured that each section connection is reliable, secured, good airproof performance, accurate positioning, is easy to adjustment, installation, and satisfaction is installed at the scene
With control, reliability is high, efficient, versatility is good, for ease of maintenaince and replaces;When being also convenient for debugging, easily remove, it can be effective
It improves working efficiency (3) this mounting structure and improves support stiffness and positioning accuracy, also reduce vibration.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto,
Any one skilled in the art is in the technical scope of present disclosure, the change or replacement that can be readily occurred in,
It should be covered by the protection scope of the present invention.Therefore, protection scope of the present invention should be with the protection model of claims
Subject to enclosing.
Claims (4)
1. a kind of mounting structure of integrated controller on carrier, which is characterized in that including:
Carrier support tube, annular controller positioning disk and connection component;Wherein,
The carrier support tube is connected on the carrier;
The carrier support tube is hollow cylinder structure, which is equipped with positioning disk installation position, this is fixed
Position disk installation position is equipped with multiple positioning disks and connects through-hole;
The annular controller positioning disk is annular plate structure, and the intermediate position of the annular controller positioning disk is equipped with comprehensive control
Device location hole processed is equipped with multiple integrated controller mounting holes, the multiple comprehensive control around the integrated controller location hole
Device mounting hole processed can install fixed integrated controller through connection component;
The periphery wall of the annular controller positioning disk be equipped with on the positioning disk installation position in the carrier support tube
Each positioning disk connects through-hole multiple mounting holes correspondingly, and each mounting hole of the annular controller positioning disk is through connection component
Through-hole is connect with the positioning disk of the positioning disk installation position of the carrier support tube to connect one by one, by the annular controller positioning disk
It is fixedly mounted on the positioning disk installation position in the carrier support tube with integrated controller.
2. a kind of mounting structure of the integrated controller according to claim 1 on carrier, which is characterized in that the fortune
Carrier supported cylinder is the hollow cylinder structure of straight tube, which is fixed on the carrier, with the fortune
Carrier is connected as one.
3. a kind of mounting structure of the integrated controller according to claim 1 or 2 on carrier, which is characterized in that institute
It states positioning disk installation position and is located at one end on the carrier support tube inner wall, the positioning disk installation position is by being located at the carrier branch
Annular groove on support cylinder inner wall connects through-hole composition with six positioning disks being arranged along the annular groove, and six positioning disks connect through-hole
It is divided into three groups, every group two are disposed adjacent along annular groove distribution.
4. a kind of mounting structure of the integrated controller according to claim 1 or 2 on carrier, which is characterized in that institute
It states connection component and uses multiple screws.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810588465.1A CN108548075A (en) | 2018-06-08 | 2018-06-08 | A kind of mounting structure of integrated controller on carrier |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810588465.1A CN108548075A (en) | 2018-06-08 | 2018-06-08 | A kind of mounting structure of integrated controller on carrier |
Publications (1)
Publication Number | Publication Date |
---|---|
CN108548075A true CN108548075A (en) | 2018-09-18 |
Family
ID=63493657
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201810588465.1A Pending CN108548075A (en) | 2018-06-08 | 2018-06-08 | A kind of mounting structure of integrated controller on carrier |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN108548075A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114963888A (en) * | 2022-04-19 | 2022-08-30 | 湖北航天飞行器研究所 | Integrated missile controller and installation and use method thereof |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20010022937A1 (en) * | 1999-09-20 | 2001-09-20 | Bucher Charles E. | Tightening device with easy alignment for securing a ceiling fan to a fitting |
US20040205802A1 (en) * | 2002-11-27 | 2004-10-14 | Sunonwealth Electric Machine Industry Co., Ltd. | Holding device for an optical disk drive |
US20130277904A1 (en) * | 2012-04-24 | 2013-10-24 | Cobra Cut Llc | Adjustable Angle Workpiece Positioning Disc |
CN203879773U (en) * | 2014-06-15 | 2014-10-15 | 罗建华 | Horizontal air surrounding blowing remote control electric fan |
CN206253893U (en) * | 2016-11-22 | 2017-06-16 | 无锡职业技术学院 | Cylindrical thin wall class part air clamper |
CN107235447A (en) * | 2017-07-24 | 2017-10-10 | 滁州卷烟材料厂 | A kind of cigarette material lifting delivery system based on comprehensive stress |
CN208503887U (en) * | 2018-06-08 | 2019-02-15 | 深圳市玛伽克蓝箭科技有限公司 | A kind of mounting structure of integrated controller on carrier |
-
2018
- 2018-06-08 CN CN201810588465.1A patent/CN108548075A/en active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20010022937A1 (en) * | 1999-09-20 | 2001-09-20 | Bucher Charles E. | Tightening device with easy alignment for securing a ceiling fan to a fitting |
US20040205802A1 (en) * | 2002-11-27 | 2004-10-14 | Sunonwealth Electric Machine Industry Co., Ltd. | Holding device for an optical disk drive |
US20130277904A1 (en) * | 2012-04-24 | 2013-10-24 | Cobra Cut Llc | Adjustable Angle Workpiece Positioning Disc |
CN203879773U (en) * | 2014-06-15 | 2014-10-15 | 罗建华 | Horizontal air surrounding blowing remote control electric fan |
CN206253893U (en) * | 2016-11-22 | 2017-06-16 | 无锡职业技术学院 | Cylindrical thin wall class part air clamper |
CN107235447A (en) * | 2017-07-24 | 2017-10-10 | 滁州卷烟材料厂 | A kind of cigarette material lifting delivery system based on comprehensive stress |
CN208503887U (en) * | 2018-06-08 | 2019-02-15 | 深圳市玛伽克蓝箭科技有限公司 | A kind of mounting structure of integrated controller on carrier |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114963888A (en) * | 2022-04-19 | 2022-08-30 | 湖北航天飞行器研究所 | Integrated missile controller and installation and use method thereof |
CN114963888B (en) * | 2022-04-19 | 2023-11-03 | 湖北航天飞行器研究所 | Integrated missile controller and installation and use method thereof |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106440948B (en) | A kind of gunnery training system and gunnery training method | |
EP2474812A3 (en) | Flight management system with integrated tactical commands for use with an aircraft and method of operating same | |
CN105067011A (en) | Overall measurement system calibration method based on vision calibration and coordinate transformation | |
CN208503887U (en) | A kind of mounting structure of integrated controller on carrier | |
CN108548075A (en) | A kind of mounting structure of integrated controller on carrier | |
CN208708023U (en) | A kind of mounting structure of controller on carrier | |
CN108759842A (en) | Rotary inertial navigation system outer level damp method based on Kalman filtering | |
CN102607591B (en) | Track data generation method for testing strap-down inertial navigation software | |
CN112859905A (en) | Unmanned aerial vehicle inspection route generation method and device for overhead power line and unmanned aerial vehicle | |
CN109737958A (en) | A kind of acoustics tests the speed the polar region grid inertial navigation error inhibition method of auxiliary | |
CN108917755A (en) | A kind of Imaging Seeker angle of sight error of zero estimation method and device | |
CN114020021B (en) | Design method and system for multi-missile distributed cooperative guidance law | |
CN108733473A (en) | A kind of positioning based on VxWorks aims at the control method of integration apparatus task | |
CN108195552A (en) | A kind of high-speed wind tunnel unmanned plane drop-test mechanism | |
MOYER et al. | An efficient assembly sequencing heuristic for printed circuit board configurations | |
CN208708047U (en) | The circuit board mounting structure in integrated controller on carrier | |
CN207050745U (en) | A kind of high-precision small size single axis gyroscope | |
CN108990325A (en) | A kind of mounting structure of controller on carrier | |
CN110441751B (en) | Dual-radar detection method and device, readable storage medium and terminal equipment | |
EP0042004A1 (en) | Gunnery simulation system. | |
CN208860357U (en) | High-precision inertial navigation set | |
CN108882608A (en) | The circuit board mounting structure in integrated controller on carrier | |
JP5216097B2 (en) | Wing installation | |
CN115488888A (en) | Object positioning method, control method and device of robot system and electronic equipment | |
CN109709821B (en) | Method for measuring delay of on-board communication |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination |