CN201489587U - Emergency state information instrument of aircraft - Google Patents
Emergency state information instrument of aircraft Download PDFInfo
- Publication number
- CN201489587U CN201489587U CN2009201734651U CN200920173465U CN201489587U CN 201489587 U CN201489587 U CN 201489587U CN 2009201734651 U CN2009201734651 U CN 2009201734651U CN 200920173465 U CN200920173465 U CN 200920173465U CN 201489587 U CN201489587 U CN 201489587U
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- aircraft
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- diaphragm capsule
- instrument
- pedestal
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Abstract
The utility model relates to an emergency state information instrument of an aircraft. The emergency state information instrument of the aircraft comprises a retracted folding sealing diaphragm capsule; the diaphragm capsule is aerated with high-pressure low-density gas and is provided with a valve for aeration and a pressure indication meter correspondingly; the upper part of the diaphragm capsule is provided with a cover plate serving as a shell of the aircraft, the lower part of the diaphragm capsule is provided with a base, and an ejection releasing mechanism which is formed by a pull rod and a pressure spring sleeved with the pull rod is arranged between an upper cover plate and a lower base of the diaphragm capsule; the base is connected with the exterior through a steel wire rope which is arranged at the bottom of the base, and the inside of the base is provided with a draw gear which is connected with the diaphragm capsule; and the inside of the diaphragm capsule is provided with an instrument container and a parachute containing chamber, and the external surface of the diaphragm capsule is provided with a light emitting signal mechanism. The emergency state information instrument of the aircraft has the advantages that: the retracted folding sealing diaphragm capsule which is pre-aerated with the high-pressure low-density gas is adopted; and once the emergency of the aircraft takes place, the diaphragm capsule is released to float in the air under the action of the ejection releasing mechanism so as to rescue, assist and provide the data reference after the diaphragm capsule is recovered.
Description
[technical field]
The utility model relates to a kind of search and rescue utility appliance, refers in particular to a kind ofly can carry out detection record and provide rescuing aircraft emergency circumstance information instrument easily to external environment condition at that time when emergency takes place for it at aircraft.
[background technology]
Voyage data recorder, popular name " black box " is a kind of instrument that data storing in the equipment navigation process is got off, its range of application is now quite wide, not only include aircrafts such as aircraft, dirigible, hot air balloon, also bring into use in the last few years on the vehicles of navigation device such as boats and ships, submarine even land operation etc.After the said equipment is provided with black box, follow-up when need understanding sailing condition, all can by reproducing device with aircraft at that time the record data in the operational process access and reset, analyze, thereby draw valuable data.Yet existing aircraft black box, the navigation situation data of its storage is mainly at device interior, talk with the record of real-time recording, navigation process device state etc. such as the driver, but can't carry out detection record to aircraft external circumstances or environment, in case this just makes that aircraft breaks down or accident, the relevant personnel can't obtain the outside at that time more reference datas of incident.In addition, the autonomous calling for help of existing black box is limited in one's ability, and after aircraft had an accident in special geographical environment, the rescue worker often was difficult in time look for its whereabouts.
[summary of the invention]
The purpose of this utility model is to have overcome above-mentioned defective, and providing a kind of can carry out detection record and provide aircraft to rescue the aircraft emergency circumstance information instrument of subsidiary function aircraft external environment condition parameter.
The purpose of this utility model is achieved in that a kind of aircraft emergency circumstance information instrument, its improvements are: it comprises the airtight bellows of a telescopic folding, be filled with in the bellows high pressure low density gas and thereon correspondence be provided with inflation with valve and pressure indicator, bellows top then is provided with the cover plate as the aircraft housing parts, the bottom is provided with pedestal, is provided with by pull bar between bellows upper cover plate, bottom base and goes up the jettison release mechanism that the stage clip of socket constitutes; Described pedestal links to each other with the outside by the wire rope that its bottom is provided with, and the haulage gear that connects bellows is installed in pedestal; Be provided with the ccontaining storehouse of instrument storehouse and parachute in the described bellows; Described bellows outside surface is provided with luminous signal mechanism.
Haulage gear includes the connection wirerope in the described pedestal, and wirerope one end and pedestal are fixed, and the middle part is folded with in pedestal, and the other end connects bellows;
The two ends of described base bottom wire rope is connected in base bottom and forms a steel wire ring, is socketed with on the steel wire ring to connect to be buckled in outside linking to each other;
Be provided with video recording sound pick-up outfit and GPS worldwide navigation equipment in the described instrument storehouse;
Described luminous signal mechanism comprises light emitting source and the high reflective material that sticks.
Than common search and rescue utility appliance, the beneficial effects of the utility model have been to adopt the telescopic folding bellows that is filled with high pressure low density gas in advance, the instrument that can detect external environment condition is set in the bellows, and be provided with controlled jettison release mechanism between pedestal about the bellows and loam cake, in case the aircraft generation emergency circumstance, jettison release mechanism discharges, bellows expand and on float to top, corresponding installation site distance, detecting instrument is quick and precisely shot with video-corder aircraft emergency circumstance body information in real time in it, and luminous signal mechanism sends out a signal for help simultaneously and the aircraft azimuth information, so that implement the rescue scheme, reclaim simultaneously under the emergency circumstance various data parameters for your guidance.
[description of drawings]
Below in conjunction with accompanying drawing in detail concrete structure of the present utility model is described in detail
Fig. 1 is a structural representation of the present utility model
[embodiment]
Below in conjunction with accompanying drawing the utility model specific embodiment is described in detail.
As shown in Figure 1, the utility model relates to a kind of aircraft emergency circumstance information instrument, it comprises the airtight bellows of a telescopic folding, be filled with in the bellows high pressure low density gas and thereon correspondence be provided with inflation with valve and pressure indicator, bellows top then is provided with the cover plate as the aircraft housing parts, the bottom is provided with pedestal, is provided with by pull bar between bellows upper cover plate, bottom base and goes up the jettison release mechanism that the stage clip of socket constitutes; Described pedestal links to each other with the outside by the wire rope that its bottom is provided with, and the haulage gear that connects bellows is installed in pedestal; Be provided with the ccontaining storehouse of instrument storehouse and parachute in the described bellows; Described bellows outside surface is provided with luminous signal mechanism.
It comprises the bellows 2 of telescopic folding, and bellows 2 is arranged on the pedestal 1, and its top then is provided with cover plate 4, and this cover plate 4 directly is arranged at outside the aircraft, with the part of an integral body of its shell formation.Bellows 2 whole employing totally-enclosed designs, be provided with the ccontaining storehouse 201 of instrument storehouse 202 and parachute in it, wherein be equipped with video recording sound pick-up outfit 204, GPS worldwide navigation equipment 203 and calling for help equipment in the instrument storehouse 202, airtight inner chamber 205 its complementary spaces of bellows 2 are filled with high pressure low density gas in advance, corresponding, be provided with inflation valve 5 and pressure indicator 6 in bellows 2 tops; In the described pedestal 1 haulage gear is installed then, haulage gear comprises the connection wire rope, wire rope one end and pedestal 1 are fixing, the middle part around superimposed in pedestal 1, the other end then connects bellows 2, the wire rope 102 that is provided with in pedestal 1 bottom links to each other with the outside, and the two ends of wire rope 102 is connected in and forms a wire line thimble on the pedestal 1, is socketed with junction button 101 on the wire line thimble and links to each other in the outside.And in the cover plate 4 of bellows 2,1 of pedestal is provided with by pull bar and goes up the jettison release mechanism 3 that the stage clip of socket constitutes, this jettison release mechanism 3 can manually or automatically discharge under the control, at ordinary times during the instrument off working state, bellows 2 integral body are in collapsed folded under the effect of pull bar, stage clip guarantees to eliminate bellows cover plate 4 and 1 slit of pedestal simultaneously, thereby the volume of lowering apparatus takies to greatest extent, in case and jettison release mechanism 3 is released, stage clip is upheld, cover plate 4 is ejected, bellows 2 effect of chamber 205 mesohigh gases is within it then expanded rapidly down, under the bellows 2 low density gas effect within it after the expansion floatability aloft or the water surface, thereby the rescue indication is provided.For further strengthening result of use of the present utility model, in described bellows 2 outside surfaces luminous signal mechanism is set, this luminous signal mechanism both can adopt the light emitting source of active illuminating band flicker to realize, also can be by adopting reflective or energy storage optically focused sticks, coating material provides whole rescue indicating effect.It is pointed out that above-mentioned wire rope 102 can replace with carbon fiber or similar material.
In sum, the utility model is by adopting the telescopic folding bellows 2 that is filled with high pressure low density gas in advance, be provided with the instrument that can detect external environment condition in the bellows 2, its bottom base 1 is provided with haulage gear, 4 of pedestal 1 and loam cakes are provided with controlled jettison release mechanism 3, on the bellows 2 luminous signal mechanism is set in addition, in case the aircraft generation emergency circumstance, jettison release mechanism work, bellows 2 expand and on float to top, corresponding installation site distance, detecting instrument is quick and precisely shot with video-corder aircraft emergency circumstance body information in real time in it, send out a signal for help simultaneously and the aircraft azimuth information, so that the related personnel seeks and implement the rescue scheme, reclaim simultaneously under the emergency circumstance various data parameters for your guidance.
It is to be noted; the utility model is not limited to above-mentioned embodiment; any simple modification, equivalent variations and modification that any those skilled in the art do the foregoing description in based on technical solutions of the utility model all belong in the protection domain of the present utility model.
Claims (5)
1. aircraft emergency circumstance information instrument, it is characterized in that: it comprises the airtight bellows of a telescopic folding, be filled with in the bellows high pressure low density gas and thereon correspondence be provided with inflation with valve and pressure indicator, bellows top then is provided with the cover plate as the aircraft housing parts, the bottom is provided with pedestal, is provided with by pull bar between bellows upper cover plate, bottom base and goes up the jettison release mechanism that the stage clip of socket constitutes; Described pedestal links to each other with the outside by the wire rope that its bottom is provided with, and the haulage gear that connects bellows is installed in pedestal; Be provided with the ccontaining storehouse of instrument storehouse and parachute in the described bellows; Described bellows outside surface is provided with luminous signal mechanism.
2. aircraft emergency circumstance information instrument as claimed in claim 1, it is characterized in that: haulage gear includes the connection wire rope in the described pedestal, and wire rope one end and pedestal are fixed, and the middle part is folded with in pedestal, and the other end connects bellows.
3. aircraft emergency circumstance information instrument as claimed in claim 1, it is characterized in that: the two ends of described base bottom wire rope is connected in base bottom and forms a wire line thimble, is socketed with on the wire line thimble to connect to be buckled in outside linking to each other.
4. aircraft emergency circumstance information instrument as claimed in claim 1 is characterized in that: be provided with video recording sound pick-up outfit, GPS worldwide navigation equipment and calling for help equipment in the described instrument storehouse.
5. aircraft emergency circumstance information instrument as claimed in claim 1 is characterized in that: described luminous signal mechanism comprises light emitting source and reflective or energy storage optically focused sticks, coating material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201734651U CN201489587U (en) | 2009-09-03 | 2009-09-03 | Emergency state information instrument of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201734651U CN201489587U (en) | 2009-09-03 | 2009-09-03 | Emergency state information instrument of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201489587U true CN201489587U (en) | 2010-05-26 |
Family
ID=42428457
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009201734651U Expired - Fee Related CN201489587U (en) | 2009-09-03 | 2009-09-03 | Emergency state information instrument of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201489587U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102320373A (en) * | 2011-05-21 | 2012-01-18 | 苏州新阳升电气有限公司 | Automatic cable cutting device for upward floating type data recorder |
| CN102360220A (en) * | 2011-05-31 | 2012-02-22 | 江汉大学 | Device and method for searching aviation recorder on seabed |
| CN103971423A (en) * | 2014-04-11 | 2014-08-06 | 李然 | Spherical aircraft black box |
| CN107108032A (en) * | 2014-10-17 | 2017-08-29 | 斯凯克公司 | For the method and apparatus from flight equipment launching objects |
| CN107813954A (en) * | 2017-10-11 | 2018-03-20 | 东莞市联洲知识产权运营管理有限公司 | A kind of folding rack in unmanned plane robot |
| CN109816814A (en) * | 2018-12-20 | 2019-05-28 | 中国船舶重工集团公司第七一0研究所 | A kind of black box device based on UUV platform |
| WO2020062205A1 (en) * | 2018-09-30 | 2020-04-02 | 苏州新阳升科技股份有限公司 | Cable cutting device for floating data recorder |
-
2009
- 2009-09-03 CN CN2009201734651U patent/CN201489587U/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102320373A (en) * | 2011-05-21 | 2012-01-18 | 苏州新阳升电气有限公司 | Automatic cable cutting device for upward floating type data recorder |
| CN102360220A (en) * | 2011-05-31 | 2012-02-22 | 江汉大学 | Device and method for searching aviation recorder on seabed |
| CN102360220B (en) * | 2011-05-31 | 2013-06-12 | 江汉大学 | Device and method for searching aviation recorder on seabed |
| CN103971423A (en) * | 2014-04-11 | 2014-08-06 | 李然 | Spherical aircraft black box |
| CN107108032A (en) * | 2014-10-17 | 2017-08-29 | 斯凯克公司 | For the method and apparatus from flight equipment launching objects |
| CN107108032B (en) * | 2014-10-17 | 2021-02-19 | 斯凯克公司 | Method and device for launching an object from a flying device |
| CN107813954A (en) * | 2017-10-11 | 2018-03-20 | 东莞市联洲知识产权运营管理有限公司 | A kind of folding rack in unmanned plane robot |
| WO2020062205A1 (en) * | 2018-09-30 | 2020-04-02 | 苏州新阳升科技股份有限公司 | Cable cutting device for floating data recorder |
| CN109816814A (en) * | 2018-12-20 | 2019-05-28 | 中国船舶重工集团公司第七一0研究所 | A kind of black box device based on UUV platform |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100526 Termination date: 20170903 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |