Background technology
For the waters surface such as solution boats and ships, naval vessels, submarine and/or the device such as submarine navigation, operation are when running into the situation such as contingency or disaster and can only waiting for that external force is rescued without self-saving ability again, for avoiding precarious position to worsen further, Chinese patent literature CN2931289Y provides a kind of self-help apparatus.Its groundwork and structure, be be respectively equipped with at the outer wall position of the described aircraft left and right sides for put can outward extending charge-discharge air bag structure store storehouse, store in storehouse the charge-discharge air bag structure being provided with and can being controlled folding and unfolding by operating-controlling mechanism, charge-discharge air bag structure is communicated with corresponding gas filled device.Under normal circumstances, this store storehouse by with by operating-controlling mechanism control open and close gas-tight silo lid close.Meet accident or dangerous situation time, need to judge according to corresponding manipulation instrument and meter and after confirming the state degree of dangerous situation, more artificially to start this self-help apparatus.Because some dangerous situation is the deterioration that namely appears and develops in wink, now can operating personal self keep stable and normal operation all very difficult, more be difficult to complete rapidly a series of operating sequence of saving oneself, still can cause being difficult to the loss toward retrieving, therefore further Improvement and perfection is still needed, to improve the success ratio saving oneself or wait for that he rescues to greatest extent, the personnel that may cause and property damage are down to minimum.
Summary of the invention
Given this, the invention provides aircraft self-help apparatus in a kind of water of improvement.
Aircraft self-help apparatus in the water that the present invention improves is the further Improvement and perfection on the corresponding self-help apparatus basis of above-mentioned bibliographical information.Its basic structure be equally be respectively equipped with at the outer wall position of the described aircraft left and right sides can be controlled to open and close by centralized control unit store storehouse, store in storehouse the charge-discharge air bag structure being respectively arranged with the inflation unit that controls with acceptor center control unit and being connected.In described aircraft and be provided with keep data transmission to connect with centralized control unit at least one horizon sensor (or claiming obliquity sensor) and/or at least one cabin in water level detector.Described sensor can send centralized control unit at any time by the detection signal speed such as whether to intake in the current horizontality of the navigation equipment such as warship, ship, cabin, by centralized control unit, the navigation equipment status signal received is carried out the process such as corresponding comparison, computing and analysis to the corresponding controlling valu preset.Once there is exceeding water level in the over-tilting of preset control value and/or cabin to cross high abnomal condition, automatically corresponding actuating unit can be started rapidly, open store storehouse, to charge-discharge air bag inflation and charge-discharge air bag is discharged to the navigation equipment such as warship, ship both sides, navigation equipment is made to keep stablizing floating condition, avoid dangerous situation to further develop and worsen, thus improve the success ratio saving oneself and/or wait for that he rescues, reduce and avoid the loss of human life/property to greatest extent.
The above-mentioned detection signal transmitted sensor and preset control value carry out the process of corresponding comparison, computing and analysis, except can adopting the multiple existing ripe data processing module that arranges in described centralized control unit, also can adopt the PLC(programmable logic controller (PLC) with central processing unit (CPU) of manipulation function that can integrate simultaneously comprise and open and store storehouse, have to centralized control units itself such as charge-discharge air bag inflation and release charge-discharge air bags) or the computing machine etc. of appropriate form.
The setting of the sensor described in said structure, preferred diverse location in described navigation equipment arranges multiple respectively according to actual needs, to improve the accuracy to there is abnomal condition detection.On the other hand, the sensor of dissimilar/performance, also can be separately positioned on the diverse location of navigation equipment, improves the sensitivity and accuracy that detect with maximum freshness.Such as, in described cabin, water level detector is preferably arranged on the cabin inner bottom part of navigation equipment; Described horizon sensor is preferably arranged on the position being not less than device vertical dimension 1/2, as deck, operator's station or higher position.
On said structure basis, at least one touching/pressure sensor also keeping data transmission to connect with described centralized control unit can also be provided with, detecting by different way and the collision that extraneous obstacle occurs more rapidly, delicately at the outer wall position of the described aircraft left and right sides.
Can find out, aircraft self-help apparatus in the water of the above-mentioned improvement of the present invention, by the respective sensor arranged, can according to received over-tilting, the abnomal condition signal such as water inlet in cabin, particularly in the very first time that dangerous situation occurs, just can automatically start corresponding actuating unit rapidly, open and store storehouse and inflate to charge-discharge air bag, prevent further developing and worsening of dangerous situation, avoid because operating personal self heavy handled reason is sluggish or delay the quality time of saving oneself and operating, substantially increase navigation equipment execution save oneself and/or wait for the success ratio that he rescues, reduce and avoid the loss of human life/property when dangerous situation occurs to greatest extent.
Below by way of the detailed description of the invention by accompanying drawing illustrated embodiment, foregoing of the present invention is described in further detail again.But this should be interpreted as that the scope of the above-mentioned theme of the present invention is only limitted to following example.Without departing from the idea case in the present invention described above, the various replacement made according to ordinary skill knowledge and customary means or change, all should comprise within the scope of the invention.
Detailed description of the invention
Fig. 1 and Fig. 2 is for the self-help apparatus of aircraft in the water of the present invention shown in the boats and ships of surface navigation.At the position of the outer wall 5 of the hull left and right sides, be respectively arranged with in a symmetrical and store storehouse 6, the gas-tight silo lid 10 in its Hatch Opening portion, side is connected on the sidewall of boats and ships through hinge 9, and the keying of gas-tight silo lid 10 can be controlled by some groups of hydraulic gears 4.Both sides store in storehouse 6 be respectively arranged be activated after can the charge-discharge air bag structure 7 that arranges of outward extending many group independent parallel, each group of charge-discharge air bag structure 7 is communicated with equipment 2 through the inflation mechanism that pipeline and air compressor etc. are conventional respectively, and can be received through flexible beam control structure controls such as suitable rope belts 8 it-put by winch 1.Under normal circumstances, each group charge-discharge air bag structure 7 is compressed airtight storing up in storing in storehouse 6.The Open-close sealing storehouse lid hydraulic gear 4 of 10 and the startup of winch 1 and inflation mechanism 2 etc., control by centralized control unit 3 is unified respectively.At the different parts of grade all around of aircraft cabin inner bottom part, be respectively arranged with water level detector 12 in some cabins all keeping data transmission to connect with centralized control unit 3; Be provided with several horizon sensors 11 keeping data transmission to connect with centralized control unit 3 being not less than in the different parts place such as device vertical dimension 1/2 or deck/operator's station.At the different parts of aircraft both sides outer wall 5, be also provided with touching/pressure sensor 13 that several also keep data transmission to connect with described centralized control unit 3.
Shown in Fig. 1 is the configuration state propagating described self-help apparatus under normal circumstances.Shown in Fig. 2 is then be in when saving oneself state, and the gas-tight silo lid 10 storing the Hatch Opening portion, side in storehouse 6 is opened, and each charge-discharge air bag structure 7 is charged pressurized air and the expansion that stretches out discharges, and ensures that ship in distress keeps stablizing floating state of saving oneself at the water surface.