CN106469473A - A kind of separate type monitor - Google Patents
A kind of separate type monitor Download PDFInfo
- Publication number
- CN106469473A CN106469473A CN201510513905.3A CN201510513905A CN106469473A CN 106469473 A CN106469473 A CN 106469473A CN 201510513905 A CN201510513905 A CN 201510513905A CN 106469473 A CN106469473 A CN 106469473A
- Authority
- CN
- China
- Prior art keywords
- monitor
- separate type
- type monitor
- module
- body structure
- 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
Abstract
The present invention relates to flight recorder field, a kind of throwing adopted data of flying protected when there is aviation accident is provided to put formula recorder, the data protected by it, cause of accident can be carried out with science, objectively analyze.This invention combines multinomial survival method, and barrier propterty is high, can on all kinds of jet planes life-time service, reliability is high.Described separate type monitor has cavity body structure and airfoil structure；Each functional module of monitor is installed in the cavity of monitor, ensure that the center of gravity of monitor near windward side and is in the overall symmetrical center line of monitor, each functional module includes beacon, energy-storage module, data management module, data storage cell, described separate type monitor also has cover plate, cavity body structure described in cover closure and fixing on an upper, and aerodynamic configuration is integrally formed with upper surface.
Description
Technical field
The present invention relates to a kind of for airborne " formula monitor is put in throwing ", belong to airborne electronic equipment product technical field.
Background technology
With extensive, high frequency applications in each field for the aircraft, the complexity of the flight speed of various military secrets and flight operating mode and
Uncertainty, the frequency more and more higher that aircraft has an accident, the destruction caused and economic loss are increasing.
The considerable damage power being formed in the frequent generation of aviation accident and accident, to the airborne safety for recording aircraft running status
Run monitoring device and propose higher data protection and positioning requirements.It is equipped with that there are certain protective capacities at present on all kinds of aircrafts
Flight parameter recording equipment, for ensure aircraft safety run played an important role.But aviation accident in certain circumstances
These log equipment are to be not enough to the positioning of propulsion accident, search and rescue, analysis cause of accident.And the U.S. and European Countries are current
Have been developed that the aircraft recorder possessing function above, and formulated the level of protection of response and enforced detailed rules and regulations.
In order to adapt to development and the change of flight environment of vehicle, each big main frame institute, factory are it is determined that progressively install, change on type of respectively advocating war
Dress, install additional to have and actively depart from aircraft and implement deceleration and the aircraft black box with certain protective capacities of floatation characteristic can be met,
Run monitoring device to replace existing on-vehicle safety, related work is carried out successively, and related development work is launched successively.
AVIC Shaanxi Qianshan Avionics Co., Ltd. is using the technical advantage in data protection field, and units concerned of institute of main engine plants
Cooperation, development and production are used for aircraft protection positioning recorder " formula recorder is put in throwing ", are provided in flight vehicle accident record
On equipment, it is Plane location and service data offer protection.
Technical specification：The minimum service behaviour specification of ED-112A anti-crash airborne recorder system.
Content of the invention
The present invention provides a kind of throwing adopted data of flying protected when there is aviation accident to put formula recorder, by its institute
The data of protection, can carry out science, objectively analyze to cause of accident.This invention combines multinomial survival method, protective
Can be high, can on all kinds of jet planes life-time service, reliability is high.
Technical scheme is a kind of separate type monitor, and described separate type monitor has a cavity body structure, described cavity body structure by
Above, below, above, bottom surface, two sides are constituted, and are above wherein windward side, and with bottom surface angle be above obtuse angle (about
For 120 °～131 °), after keep vertical with bottom surface, be flight aerodynamic configuration face above, two sides for inner concave so that
Described monitor both sides become airfoil structure；Each functional module of monitor is installed in the cavity of monitor it is ensured that monitor
Center of gravity near windward side and be in the overall symmetrical center line of monitor, each functional module include beacon, energy-storage module,
Data management module, data storage cell, described separate type monitor also has cover plate, the cavity body structure described in cover closure
And on being fixed in the above, and with aerodynamic configuration is integrally formed above.
Described wall body structure enables separate type monitor to swim in be communicated on the water surface.
Separate type monitor passes through molding by composite plus resin base and forms agent structure, passes through built-in metal in agent structure
Part is attached and reinforces throwing and put formula recorder being made up of parts such as outer protective cover, internal damping absorbing energy layer, functional module and cover plates.
By high-strength, high-ductility composite molding, there is the ability that very strong opposing destroys and deforms；Internal damping absorbing energy layer is by spy
Plant macromolecular material composition, foaming is carried out by special process, for protecting internal module not to be subject under high intensity collision situation
Damage；Functional module is placed in macromolecular material, for data storage, accident positioning and report position；Cover plate is also extraordinary composite wood
Material is constituted, and has high intensity, high tenacity feature.Separate type monitor constitutes and sees Fig. 1.
Separate type monitor through simulation calculation and test, stand collision, thump, penetrate, static extruding, high temperature are burnt,
After low temperature baked wheaten cake, fluid immersion, hydrostatic pressure etc. destroy examination, the information that memory module preserves is not damaged, is lost.In addition,
It also has structure gently, can slow down, the features such as floating.
Brief description
Fig. 1 is separate type monitor structural representation；
Fig. 2 is separate type monitor cavity schematic diagram；
Fig. 3 is separate type monitor cavity front view；
Fig. 4 is separate type monitor cavity side view；
Fig. 5 is separate type monitor top view；
1-01 is cover plate；1-02 cover plate trip bolt；1-03 is beacon I；1-04 is beacon II；1-05 is energy-storage module；1-06
For data management module；1-07 is data storage cell；1-08 is cavity body structure.
Specific embodiment
Specifically provide a kind of separate type monitor it is characterised in that：Described separate type monitor by above, below, upper table
Face, lower surface, two sides constitute a cavity body structure, are above wherein windward side, and are above that obtuse angle (is with bottom surface angle
120 °～131 °), after keep vertical with bottom surface, upper surface is flight aerodynamic configuration face, and two sides are for inner concave so that institute
Stating monitor both sides becomes airfoil structure；Each functional module of monitor is installed in the cavity of monitor it is ensured that monitor
Center of gravity near windward side and is in the overall symmetrical center line of monitor, and each functional module includes beacon, energy-storage module, number
According to management module, data storage cell, described separate type monitor also has cover plate, and the cavity body structure described in cover closure is simultaneously
Fix on an upper, and aerodynamic configuration is integrally formed with upper surface.
Cavity structure enables to separate type monitor and swims in communicated on the water surface.
Separate type monitor passes through molding by composite plus resin base and forms agent structure, passes through built-in metal in agent structure
Part is attached and reinforces.
Each module is placed in overcoat in buffering energy-absorbing, and this layer has fire-retardant, heat-insulated and hydrophobic property, whole using macromolecular material
Body formed, very strong protective capability can be produced to module.
Memory module is wrapped with encapsulant, and protection memory module exempts from fluid erosion.
Separate type monitor, compared with same kind of products at abroad, is mainly manifested in the raising of opposing mechanical damage ability.Pass through during design
Selection and to buffering energy-absorbing structure form specific aim optimization it is ensured that its requirement of resistance to mechanical damage capability of reaching, specific as follows：
By high intensity, high-ductility composite under high temperature and high pressure environment integral die shaping, profile has good aerodynamic characteristic and drift
Floating stability characteristic (quality), light filling expanded material in this aerofoil profile feature can also be floated so as to Air slowdown can not only be completed,
Product entirety appearance can meet wave transparent and require.
(2) cover plate high intensity, high-ductility composite overall processing molding, main body is flat type, profile and upper surface outer shape phase
Adaptation, on flat board processing with upper surface cooperation unthreaded hole, fix for carrying out mode connects for screw with upper surface, and dodge frequency lamp position in
On this cover plate.
(3) when upper surface and cover plate are assembled together, cover plate is connected by screw on the built-in fitting of outer cover part, in short transverse entirety
Position the weakest, for avoiding screw to be subject to big load to destroy, causes upper surface to separate with cover plate, pacifies in the two gap
Dress sealing gasket.When monitor such as experiences a shock, extrudes at the external applied load destruction, upper surface is deformed first with cover plate, consumes
Failure energy, effectively reduces the contact failure load that inner chamber module is born.Further, since screw be tightly distributed in highly square
To, the probability not having pure shear shear force to destroy, the probability further reducing screw extraction destruction is it is ensured that upper surface and lid
Plate obtains connection reliability.
The each module of inner chamber is placed on overcoat in buffering energy-absorbing, and this layer has fire-retardant, heat-insulated and hydrophobic property, using macromolecular material
Global formation, can produce very strong protective capability to module.
Using the method for memory module outer wrapping encapsulant, memory module is protected to exempt from fluid erosion.
Claims (5)
1. a kind of separate type monitor it is characterised in that：Described separate type monitor has cavity body structure, and described cavity is tied
Structure by above, below, above, bottom surface, two sides are constituted, and are above wherein windward side, and are above obtuse angle with bottom surface angle
(for 120 °～131 °), after with bottom surface keep vertical, above be flight aerodynamic configuration face, two sides be inner concave, make
Obtaining described monitor both sides becomes airfoil structure；Each functional module of monitor is installed in the cavity of monitor it is ensured that recording
The center of gravity of instrument near windward side and is in the overall symmetrical center line of monitor, each functional module include beacon, energy-storage module,
Data management module, data storage cell, described separate type monitor also has cover plate, the cavity body structure described in cover closure
And be fixed on above, and with aerodynamic configuration is integrally formed above.
2. separate type monitor as claimed in claim 1 is it is characterised in that described cavity body structure enables separate type monitor
Enough swim in and communicated on the water surface.
3. separate type monitor as claimed in claim 1 is it is characterised in that separate type monitor is led to by composite plus resin base
Cross molding and form agent structure, be attached by pre-embedding metal part in agent structure and reinforce.
4. separate type monitor as claimed in claim 1, should it is characterised in that each module is placed in overcoat in buffering energy-absorbing
Layer has fire-retardant, heat-insulated and hydrophobic property, using macromolecular material global formation, can produce very strong protective capability to module.
5. separate type monitor as claimed in claim 1 it is characterised in that memory module is wrapped with encapsulant, deposit by protection
Storage module exempts from fluid erosion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510513905.3A CN106469473A (en) | 2015-08-20 | 2015-08-20 | A kind of separate type monitor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510513905.3A CN106469473A (en) | 2015-08-20 | 2015-08-20 | A kind of separate type monitor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106469473A true CN106469473A (en) | 2017-03-01 |
Family
ID=58229641
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510513905.3A Pending CN106469473A (en) | 2015-08-20 | 2015-08-20 | A kind of separate type monitor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106469473A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106379545A (en) * | 2016-08-30 | 2017-02-08 | 陕西千山航空电子有限责任公司 | Anti-destroy jettisoning recorder with speed reduction function |
| CN109353529A (en) * | 2018-09-11 | 2019-02-19 | 陕西千山航空电子有限责任公司 | Logger mounting rack is put in a kind of throwing |
| CN110706373A (en) * | 2019-09-12 | 2020-01-17 | 陕西千山航空电子有限责任公司 | Positioning and data recording device on water |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201607773U (en) * | 2009-12-30 | 2010-10-13 | 毕耘滔 | Vehicle-mounted road-condition recorder |
| CN202268010U (en) * | 2011-09-16 | 2012-06-06 | 东莞常禾电子有限公司 | Combined driving recording device |
| CN103065372A (en) * | 2012-12-07 | 2013-04-24 | 陕西千山航空电子有限责任公司 | Aviation recorder and automatic positioning method |
| CN104768847A (en) * | 2012-09-19 | 2015-07-08 | 太阳方舟公司 | Hydrogen-regenerating solar-powered aircraft |
| CN104821019A (en) * | 2015-04-17 | 2015-08-05 | 中通客车控股股份有限公司 | Electric vehicle data recorder protecting device and method |
-
2015
- 2015-08-20 CN CN201510513905.3A patent/CN106469473A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201607773U (en) * | 2009-12-30 | 2010-10-13 | 毕耘滔 | Vehicle-mounted road-condition recorder |
| CN202268010U (en) * | 2011-09-16 | 2012-06-06 | 东莞常禾电子有限公司 | Combined driving recording device |
| CN104768847A (en) * | 2012-09-19 | 2015-07-08 | 太阳方舟公司 | Hydrogen-regenerating solar-powered aircraft |
| CN103065372A (en) * | 2012-12-07 | 2013-04-24 | 陕西千山航空电子有限责任公司 | Aviation recorder and automatic positioning method |
| CN104821019A (en) * | 2015-04-17 | 2015-08-05 | 中通客车控股股份有限公司 | Electric vehicle data recorder protecting device and method |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106379545A (en) * | 2016-08-30 | 2017-02-08 | 陕西千山航空电子有限责任公司 | Anti-destroy jettisoning recorder with speed reduction function |
| CN109353529A (en) * | 2018-09-11 | 2019-02-19 | 陕西千山航空电子有限责任公司 | Logger mounting rack is put in a kind of throwing |
| CN110706373A (en) * | 2019-09-12 | 2020-01-17 | 陕西千山航空电子有限责任公司 | Positioning and data recording device on water |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US20140277923A1 (en) | Deployable flight recorder | |
| CN106469473A (en) | A kind of separate type monitor | |
| CN102030102B (en) | Horizontal tail front edge for bird strike-resisting airplane | |
| CN108482683A (en) | A kind of system and method using the anti-deicing of sliding discharge plasma | |
| Zeppetelli et al. | In-flight icing risk management through computational fluid dynamics-icing analysis | |
| CN205608828U (en) | Flight data record protection memory excels in | |
| CN105261082B (en) | The amphibious positioning emergency device of black box intelligence land-sea | |
| CN106379545A (en) | Anti-destroy jettisoning recorder with speed reduction function | |
| CN201971150U (en) | Aircraft tailplane with front edge reinforced element | |
| CN111697176A (en) | Anti-collision device of battery pack and electric aircraft | |
| CN203895600U (en) | Airborne radome equipped with self-balance air pressure function | |
| CN203982464U (en) | The amphibious positioning emergency device in sea, black box intelligence land | |
| CN106965873B (en) | Omnidirectional movement inspection platform with double-layer vehicle body | |
| CN203904918U (en) | Two-stage anti-collision buffer ring | |
| CN212047934U (en) | Safe intelligent aircraft wheel chock | |
| CN214493342U (en) | Unmanned aerial vehicle vaulting pole structure | |
| CN202063257U (en) | Light multipurpose aircraft | |
| CN203904919U (en) | Inside energy dissipation pad of anti-collision fender | |
| CN205563740U (en) | Machine carries to launch and floats urgent positioner of formula | |
| CN218077963U (en) | Compound layer type new energy environment test box | |
| RU2131828C1 (en) | Container mainly intended for landable aero-space objects | |
| CN220493364U (en) | Pressure relief side plate of sealed case and sealed case | |
| CN208096136U (en) | Aviation helmet | |
| CN216102810U (en) | Crash-resistant emergency positioning device with floating function | |
| CN217730797U (en) | Energy-absorbing structural unit for resisting falling and collision of airplane |
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 | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170301 |
|
| RJ01 | Rejection of invention patent application after publication |