CN106081140A - Unmanned plane automatic pilot installing rack penetrated by a kind of big gun - Google Patents
Unmanned plane automatic pilot installing rack penetrated by a kind of big gun Download PDFInfo
- Publication number
- CN106081140A CN106081140A CN201610550873.9A CN201610550873A CN106081140A CN 106081140 A CN106081140 A CN 106081140A CN 201610550873 A CN201610550873 A CN 201610550873A CN 106081140 A CN106081140 A CN 106081140A
- Authority
- CN
- China
- Prior art keywords
- automatic pilot
- overload
- gps antenna
- rigid frame
- unmanned plane
- 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.)
- Granted
Links
- 230000015572 biosynthetic process Effects 0.000 claims abstract description 4
- 238000004026 adhesive bonding Methods 0.000 claims description 4
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
- 230000006835 compression Effects 0.000 claims description 3
- 238000007906 compression Methods 0.000 claims description 3
- 210000000038 chest Anatomy 0.000 abstract description 6
- 238000009434 installation Methods 0.000 abstract description 5
- 238000003860 storage Methods 0.000 abstract description 3
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 238000010276 construction Methods 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 7
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 208000033999 Device damage Diseases 0.000 description 1
- 108091092878 Microsatellite Proteins 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Support Of Aerials (AREA)
Abstract
The invention discloses a kind of big gun and penetrate unmanned plane automatic pilot installing rack, including overload-resistant rigid frame and automatic pilot shield shell, the outwardly formation in the edge mounting flange of overload-resistant rigid frame left end, automatic pilot shield shell is arranged in the left half of overload-resistant rigid frame, automatic pilot shield shell is connected with mounting flange by bumper post, the right half of overload-resistant rigid frame is provided with gps antenna support, gps antenna support is connected with overload-resistant rigid frame by spring, and gps antenna support is provided with gps antenna.Beneficial effects of the present invention: improve anti-overload ability, alleviates construction weight, reduces installation difficulty, it is achieved that modularity；Reduce the impact to automatic pilot, it is to avoid the damage of device, meet the overload requirement of transmitting；Achieve the gps antenna of Pop-up, the problem quickly ejected after solving in gps antenna thorax storage in fuselage and going out thorax, improve the locating speed of navigation system, precision.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, it particularly relates to unmanned plane automatic pilot installing rack penetrated by a kind of big gun.
Background technology
Microminiature autopilot system is the core control part of SUAV.Its internal mainly by navigation system and
Flight control system two parts form.The Inertial Measurement Unit that is made up of micromechanical gyro again inside navigation system, magnetic compass, GPS etc.
Navigational material forms, and these senser elements are the most sensitive to temperature, vibrations, electromagnetic interference etc., and therefore, traditional unmanned plane is automatic
The damping problem of pilot mounting structure Inertial Measurement Unit to be considered, the electromagnetic shielding of whole navigation flight control system are asked
Topic, and the installation gain problem of gps antenna.
Unmanned plane penetrated by big gun is a kind of special Small and micro-satellite, due to the particularity of emission process, this unmanned plane
Automatic pilot to experience bigger overload in emission process, and due to bigger overload, its fuselage is typically by high intensity
Carbon fiber or metal manufacture, and launch before gps antenna must be accommodated in fuselage, it is impossible to good reception gps signal.Cause
This, the mounting structure of existing automatic pilot does not all account for these demands, and prior art can not meet requirement.
For the problem in correlation technique, effective solution is the most not yet proposed.
Summary of the invention
It is an object of the invention to provide a kind of big gun and penetrate unmanned plane automatic pilot installing rack, to overcome currently available technology to deposit
Above-mentioned deficiency.
For realizing above-mentioned technical purpose, the technical scheme is that and be achieved in that:
A kind of big gun penetrates unmanned plane automatic pilot installing rack, including overload-resistant rigid frame and automatic pilot shield shell, institute
State overload-resistant rigid frame and be divided into left half and right half, and the height of left half is more than the height of right half, described overload-resistant
The outwardly formation in edge and the big gun of rigid frame left end penetrate the mounting flange that unmanned plane body is fastenedly connected, and described Method for Installation
Blue installed surface is perpendicular to launch axis, described automatic pilot shield shell by machinery position constraint described overload-resistant just
Property framework left half in, and this automatic pilot shield shell arranges along launching axis direction, this automatic pilot shielding case
Body is connected with mounting flange also by some bumper posts, and the right half of described overload-resistant rigid frame is provided with gps antenna support.
Further, this gps antenna support is connected with described overload-resistant rigid frame by least four spring, should
Gps antenna support is provided with gps antenna.
Further, in described each spring, it is equipped with guider screw, and one end of guider screw is propped up with described gps antenna
Frame is connected.
Further, described overload-resistant rigid frame left half upper surface is away from described overload-resistant rigid frame right half upper end
The distance value in face is more than the one-tenth-value thickness 1/10 of described gps antenna support, described spring height value under compression and described GPS
The one-tenth-value thickness 1/10 sum of antenna.
Selectable, described gps antenna can be bonded on described gps antenna support by the way of gluing is bonding.
Preferably, described bumper post is rubber buffer post.
Preferably, described overload-resistant rigid frame is of an L-shaped structure.
Preferably, described overload-resistant rigid frame and described mounting flange all use high-strength aluminum alloy material.
Beneficial effects of the present invention: use and launch axial mounting flange, improve anti-overload ability, alleviate structure weight
Amount, reduces installation difficulty, it is achieved that modularity；Use bumper post, reduce the impact to automatic pilot, it is to avoid device
Damage, meet the overload requirement of transmitting；By arranging spring between gps antenna support and overload-resistant rigid frame, from
And achieve the gps antenna of Pop-up, and the problem quickly ejected after solving in gps antenna thorax storage in fuselage and going out thorax, carry
The high locating speed of navigation system, precision.
Accompanying drawing explanation
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, below will be to institute in embodiment
The accompanying drawing used is needed to be briefly described, it should be apparent that, the accompanying drawing in describing below is only some enforcements of the present invention
Example, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to obtains according to these accompanying drawings
Obtain other accompanying drawing.
The structural representation of unmanned plane automatic pilot installing rack penetrated by the big gun that Fig. 1 is described according to embodiments of the present invention.
In figure:
1, overload-resistant rigid frame；2, automatic pilot shield shell；3, mounting flange；4, bumper post；5, gps antenna support；
6, spring；7, gps antenna.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Describe, it is clear that described embodiment is only a part of embodiment of the present invention rather than whole embodiments wholely.Based on
Embodiment in the present invention, all other embodiments that those of ordinary skill in the art are obtained, broadly fall into present invention protection
Scope.
As it is shown in figure 1, penetrate unmanned plane automatic pilot installing rack according to a kind of big gun described in embodiments of the invention, including
Overload-resistant rigid frame 1 and automatic pilot shield shell 2, described overload-resistant rigid frame 1 is divided into left half and right half, and
The height of left half is more than the height of right half, and the outwardly formation in edge of described overload-resistant rigid frame 1 left end is penetrated with big gun
The mounting flange 3 that unmanned plane body is fastenedly connected, and the installed surface of described mounting flange 3 be perpendicular to launch axis, described automatically
Pilot shield shell 2 by machinery position constraint in the left half of described overload-resistant rigid frame 1, and this automatic pilot
Shield shell 2 is arranged along launching axis direction, and this automatic pilot shield shell 2 is also by some bumper posts 4 and mounting flange 3
Connecting, the right half of described overload-resistant rigid frame 1 is provided with gps antenna support 5, and wherein this gps antenna support 5 is by four
Spring 6 is connected with described overload-resistant rigid frame 1, and this gps antenna support 5 is provided with gps antenna 7.
It is equipped with guider screw in described each spring 6, and one end of guider screw is connected with described gps antenna support 5
Connect.
Described overload-resistant rigid frame 1 left half upper surface away from described overload-resistant rigid frame 1 right half upper surface away from
Distance values is more than the one-tenth-value thickness 1/10 of described gps antenna support 5, described spring 6 height value under compression and described gps antenna
The one-tenth-value thickness 1/10 sum of 7.
Described gps antenna 7 is bonded on described gps antenna support 5 by the way of gluing is bonding.
Understand the technique scheme of the present invention for convenience, below by way of above-mentioned to the present invention in specifically used mode
Technical scheme is described in detail.
When specifically used, described mounting flange 3 and described overload-resistant rigid frame 1 are overall numerical control machine-shaping, adopt
With high-strength aluminum alloy material, described mounting flange 3 and big gun are penetrated unmanned plane body and are bolted, and installed surface is perpendicular to send out
Penetrating axis, described automatic pilot shield shell 2, is being launched by machinery position constraint in described overload-resistant rigid frame 1
Axis direction, described automatic pilot shield shell 2 is connected with described mounting flange 3 by described bumper post 4, thus reaches fall
The effect of low launching over loading, described gps antenna 7 is bonded to above described gps antenna support 5 by gluing, and described gps antenna props up
Frame 5 by guider screw with and described spring 6 be connected with described overload-resistant rigid frame 1, in described spring 6 compressive state, institute
Stating gps antenna 7 can be received in unmanned aerial vehicle body, upspring state at described spring 6, described gps antenna 7 can stretch out unmanned plane machine
The height that body is outer eight millimeters.
In sum, by means of the technique scheme of the present invention, launch axial mounting flange 3 by using, improve
Anti-overload ability, alleviates construction weight, reduces installation difficulty, it is achieved that modularity；Using bumper post 4, it is right to reduce
The impact of automatic pilot, it is to avoid the damage of device, meets the overload requirement of transmitting；By at gps antenna support 5 with anti-
Between overload rigid frame 1, spring 6 is set, it is achieved thereby that the gps antenna 7 of Pop-up, solves fuselage in gps antenna 7 thorax
Interior storage and the problem quickly ejected after going out thorax, improve the locating speed of navigation system, precision.
The foregoing is only presently preferred embodiments of the present invention, not in order to limit the present invention, all essences in the present invention
Within god and principle, any modification, equivalent substitution and improvement etc. made, should be included within the scope of the present invention.
Claims (8)
1. unmanned plane automatic pilot installing rack penetrated by a big gun, it is characterised in that described installing rack includes overload-resistant rigid frame
With automatic pilot shield shell, described overload-resistant rigid frame is divided into left half and right half, and the height of left half is more than
The height of right half, the outwardly formation in edge of described overload-resistant rigid frame left end is penetrated unmanned plane body with big gun and is fastenedly connected
Mounting flange, and the installed surface of described mounting flange be perpendicular to launch axis, described automatic pilot shield shell passes through machine
Tool position constraint is in the left half of described overload-resistant rigid frame, and this automatic pilot shield shell is along launching axis direction
Arranging, this automatic pilot shield shell is connected with described mounting flange also by some bumper posts, described overload-resistant rigid frame
The right half of frame is provided with gps antenna support.
Unmanned plane automatic pilot installing rack penetrated by a kind of big gun the most according to claim 1, it is characterised in that this gps antenna
Support is connected with described overload-resistant rigid frame by least four spring, and this gps antenna support is provided with gps antenna.
Unmanned plane automatic pilot installing rack penetrated by a kind of big gun the most according to claim 2, it is characterised in that described each bullet
It is equipped with guider screw in spring, and one end of guider screw is connected with described gps antenna support.
Unmanned plane automatic pilot installing rack penetrated by a kind of big gun the most according to claim 3, it is characterised in that described overload-resistant
The rigid frame left half upper surface distance value away from described overload-resistant rigid frame right half upper surface props up more than described gps antenna
The one-tenth-value thickness 1/10 of frame, described spring height value under compression and the one-tenth-value thickness 1/10 sum of described gps antenna.
Unmanned plane automatic pilot installing rack penetrated by a kind of big gun the most according to claim 2, it is characterised in that described GPS days
Line is bonded on described gps antenna support by the way of gluing is bonding.
Unmanned plane automatic pilot installing rack penetrated by a kind of big gun the most according to claim 1, it is characterised in that described bumper post
For rubber buffer post.
Unmanned plane automatic pilot installing rack penetrated by a kind of big gun the most according to claim 1, it is characterised in that described overload-resistant
Rigid frame is of an L-shaped structure.
Unmanned plane automatic pilot installing rack penetrated by a kind of big gun the most according to claim 1, it is characterised in that described overload-resistant
Rigid frame and described mounting flange all use high-strength aluminum alloy material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610550873.9A CN106081140B (en) | 2016-07-13 | 2016-07-13 | A kind of big gun penetrates UAV autopilot mounting rack |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610550873.9A CN106081140B (en) | 2016-07-13 | 2016-07-13 | A kind of big gun penetrates UAV autopilot mounting rack |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106081140A true CN106081140A (en) | 2016-11-09 |
| CN106081140B CN106081140B (en) | 2019-01-22 |
Family
ID=57220602
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610550873.9A Active CN106081140B (en) | 2016-07-13 | 2016-07-13 | A kind of big gun penetrates UAV autopilot mounting rack |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106081140B (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5088658A (en) * | 1991-03-20 | 1992-02-18 | Raytheon Company | Fin command mixing method |
| JP2007085627A (en) * | 2005-09-21 | 2007-04-05 | Mitsubishi Electric Corp | Guided missile |
| CN202295292U (en) * | 2011-09-09 | 2012-07-04 | 中国航天科工集团第三研究院第八三五七研究所 | Novel vibration reduction device suitable for automatic driving instrument of unmanned plane |
| DE102014008788A1 (en) * | 2014-06-10 | 2015-12-17 | Hans-Joachim Lange | Method and device for increasing flight safety |
| CN204945804U (en) * | 2015-08-31 | 2016-01-06 | 致导科技（北京）有限公司 | A kind of unmanned plane robot pilot |
| CN105628019A (en) * | 2015-12-25 | 2016-06-01 | 河北工业大学 | Modular micro AUV communication-navigation module |
| CN205819580U (en) * | 2016-07-13 | 2016-12-21 | 西藏长源动力科技有限公司 | Unmanned plane automatic pilot installing rack penetrated by a kind of big gun |
-
2016
- 2016-07-13 CN CN201610550873.9A patent/CN106081140B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5088658A (en) * | 1991-03-20 | 1992-02-18 | Raytheon Company | Fin command mixing method |
| JP2007085627A (en) * | 2005-09-21 | 2007-04-05 | Mitsubishi Electric Corp | Guided missile |
| CN202295292U (en) * | 2011-09-09 | 2012-07-04 | 中国航天科工集团第三研究院第八三五七研究所 | Novel vibration reduction device suitable for automatic driving instrument of unmanned plane |
| DE102014008788A1 (en) * | 2014-06-10 | 2015-12-17 | Hans-Joachim Lange | Method and device for increasing flight safety |
| CN204945804U (en) * | 2015-08-31 | 2016-01-06 | 致导科技（北京）有限公司 | A kind of unmanned plane robot pilot |
| CN105628019A (en) * | 2015-12-25 | 2016-06-01 | 河北工业大学 | Modular micro AUV communication-navigation module |
| CN205819580U (en) * | 2016-07-13 | 2016-12-21 | 西藏长源动力科技有限公司 | Unmanned plane automatic pilot installing rack penetrated by a kind of big gun |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106081140B (en) | 2019-01-22 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11100810B2 (en) | Drone encroachment avoidance monitor | |
| CN206409570U (en) | Shock absorber and aircraft | |
| US10392125B2 (en) | System and method for onboard wake and clear air turbulence avoidance | |
| CN106125765B (en) | A kind of vehicle-mounted landing simulation system of boat-carrying unmanned helicopter | |
| CN110160523B (en) | Initial alignment azimuth angle compensation method based on azimuth binding and vehicle-mounted weapon system | |
| US20210302142A1 (en) | Laser guided bomb with proximity sensor | |
| KR20140113922A (en) | Test apparatus for avionic sensors and method of testing avionic sensors | |
| CN102530255A (en) | Accurate parachute landing device for traction type unmanned plane and method | |
| CN205819580U (en) | Unmanned plane automatic pilot installing rack penetrated by a kind of big gun | |
| CN106081140A (en) | Unmanned plane automatic pilot installing rack penetrated by a kind of big gun | |
| US10926887B2 (en) | Systems for and methods of providing indicators useful for piloting an aircraft | |
| CN108398956B (en) | Unmanned aerial vehicle balance system for shipborne platform and control method thereof | |
| CN112492514B (en) | Flight data and image transmission device capable of expanding controllable range of unmanned aerial vehicle | |
| CN106292707A (en) | Can be by the method and device of set point automatic Landing unmanned plane | |
| CN116954247A (en) | Composite guidance aircraft guidance control method and system considering falling angle constraint during flight | |
| CN109190191A (en) | A kind of ship load stabilized platform structure design method based on performance | |
| CN205686620U (en) | A kind of Multi-layer suspension type damping device of system for flight control computer | |
| CN212313865U (en) | Automatic landing device that stabilizes of unmanned aerial vehicle | |
| CN205872511U (en) | Pneumatic launching cradle of unmanned aerial vehicle | |
| CN214824196U (en) | Unmanned aerial vehicle laser radar nacelle | |
| CN210149569U (en) | Wing protective structure for unmanned aerial vehicle | |
| RU2013110582A (en) | METHOD FOR PRECISE LANDING OF UNMANNED AIRCRAFT | |
| CN217951081U (en) | Airborne mobile measurement system shock-absorbing structure | |
| Lesonen et al. | Landing methods of unmanned aerial vehicle | |
| CN110375746B (en) | Multimode combined receiving system for airborne radio navigation |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220623 Address after: No. 248, business building 2, building 1, jianxiyuan Zhongli, Haidian District, Beijing 100143 Patentee after: ORIGIN DYNAMIC (BEIJING) TECHNOLOGY CO.,LTD. Address before: 850032 No. 1, building 10, Shitong sunshine new town, No. 158, Jinzhu West Road, Lhasa, Tibet Autonomous Region Patentee before: TIBET CHANGYUAN POWER TECHNOLOGY Co.,Ltd. |