CN110065643A - Can promote ensure aircraft carrier safety the device of warship - Google Patents

Abstract

" can promote ensure aircraft carrier safety the device of warship " includes tail hooks, check cable, pressure sensor, high speed high definition camera device, self-con-tained unit, Self controlling valve and door, nor gate (D) etc..Pressure sensor setting is on tail hook.In carrier-borne drive end unit, simultaneously closely alignment tail hooks the setting of high speed high definition camera device in front.Carrier-borne aircraft reduction of speed warship when, pressure sensor and high speed high definition camera device overall process detection tail hook and the hook operation of check cable.Then by pressure sensor, high speed high definition camera device, the operation with the devices such as door, nor gate (D), self-con-tained unit, Self controlling valve, ensure that tail hook can successfully catch on a wherein check cable, then carrier-borne aircraft safety warship.Conversely, when confirming that tail hook fails to catch on any check cable, it is ensured that carrier-borne function is refueled in time to be accelerated to go around, safe from warship.The present invention has many important advantages.In particular, being convenient to be configured installation on the carrier-borne aircraft of other active services.

Description

Can promote ensure aircraft carrier safety the device of warship

Technical field: the present invention relates to a kind of " can promote guarantee aircraft carrier safely the device of warship "

Background technique: it is current, ensure aircraft carrier safety the device of warship, be with carrier-borne aircraft body tail portion is arranged in Tail hooks to catch on the check cable being arranged at type aircraft carrier deck tail portion.The device can force the carrier-borne aircraft to land and rest on the first of aircraft carrier On plate.There are following deficiencies for defencive function of the device to carrier landing:

It can be unlikely to accelerate successfully to go around because of stall, then cause after hooking check cable failure to ensure The accident that the carrier-borne aircraft falls into the sea, carrier-borne aircraft, which is taken, keeps high flying speed to carry out the method for warship.This kind warship method exist Many defects.For example, carrier-borne aircraft must be directed at the aircraft carrier to be landed with flying speed moment, itself just have very big Difficulty and security risk.Then, but can because quickly warship, increase carrier-borne aircraft hook check cable difficulty, then reduce Success hooks the probability of check cable.In addition, the carrier-borne aircraft is in a very short period of time by complete after the carrier-borne aircraft successfully hooks check cable Prompt drop speed be it is static, the health of the pilot of carrier-borne aircraft can be caused to damage.In addition, the high speed of carrier-borne aircraft warship, increase warship Carrier aircraft high speed warship when with type aircraft carrier deck impact force, then increase the damage etc. to carrier-borne aircraft.

In this way, how efficiently against above-mentioned defect, promote the safety for ensureing aircraft carrier warship just become It is necessary.

Summary of the invention: it is an object of the invention to provide it is a kind of " can promote guarantee aircraft carrier safely the dress of warship Set ", it is that a kind of hooked using the tail being additionally arranged to carrier-borne aircraft is detected automatically with check cable hook overall process, and can be directed to should Hook result success or not, it is automatic carry out immediately, effectively cope with, then, it is ensured that carrier-borne function slows down, safety the dress of warship It sets.

Can promote ensure aircraft carrier safety the device of warship, mainly include: carrier-borne aircraft, tail hook (tail hook setting In the tail portion of carrier-borne aircraft body.Its function is to catch on the check cable being arranged at type aircraft carrier deck tail portion, then drops the carrier-borne aircraft It falls on the deck for resting on aircraft carrier.), pockets (pockets setting tail hook on.Its function is, for accommodating The check cable caught on by tail, to ensure that tail hook can hook firm check cable.), (check cable is arranged in aircraft carrier first for first check cable At plate tail portion.Its function is mutually caught on tail hook, rests on carrier-borne aircraft landing on the deck of aircraft carrier.), second (check cable is arranged at type aircraft carrier deck tail portion for check cable.Certain intervals are kept with first check cable.Its function is, when Tail hook fails after catching on first check cable, this check cable continues mutually to catch on tail hook, then stops carrier-borne aircraft landing It stays on the deck of aircraft carrier.), Article 3 check cable (check cable be arranged at type aircraft carrier deck tail portion.It is protected with Article 2 check cable Hold certain intervals.Its function is, after tail hook fails to catch on Article 2 check cable, this check cable, which continues to hook with tail, mutually to be hooked Firmly, carrier-borne aircraft landing is rested on the deck of aircraft carrier.), pressure sensor (pressure sensor setting accommodate it is recessed Middle part at the slot bottom of slot.Its function is blocked when the pockets on tail hook successfully catch on three check cables one therein Suo Hou, the check cable being hooked on will apply a pressure with the pressure sensor contacts in pockets and to the pressure sensor Power.Then, the pressure sensor is high electric by after the check cable pressure applied being hooked on, generating at once and exporting one Ordinary mail number " 1 ".Then by high level signal " 1 " input logic and door.Conversely, the pressure sensor generates at once and exports one Low level signal " 0 ".Then by low level signal " 0 " input logic and door.It is tauted in order to avoid the pressure sensor Huge extruding force caused by check cable is damaged, and is provided with elastic limit device on the pressure sensor.), high speed high-definition camera (the high speed high definition camera device is arranged at the tail portion of carrier-borne aircraft body device and front is closely directed at tail and hooks.Its function is, It can accurately detect the hook that first check cable, Article 2 check cable, Article 3 check cable are hooked with tail respectively respectively in order Extension process, until whether having linked up with success.When the tail of high speed high definition camera device confirmation carrier-borne aircraft catches on three check cables Wherein when a check cable, export high level signal " 1 ".Then by high level signal " 1 " input logic and door.Conversely, then It exports low level signal " 0 ".Then by low level signal " 0 " input logic and door.In order to ensure carrier-borne aircraft night warship Safety, the high speed high definition camera device are provided with night vision function.), hand push button (hand push button setting self-con-tained unit with On circuit between Self controlling valve, which is set as normally opened button.Its function is that Self controlling valve occurs wrong in order to prevent Error starting.When carrier-borne aircraft is preparing to warship, the pilot of the carrier-borne aircraft presses the hand push button, then, connect self-con-tained unit with Circuit between Self controlling valve.), (output end of nor gate D is arranged in the self-con-tained unit to self-con-tained unit.Its function is to receive to come From the output signal of nor gate D.When nor gate D is to the self-con-tained unit input low level signal " 0 ", the self-con-tained unit is to automatic control Valve continues to issue out code.Then, Self controlling valve continues to remain turned-off.When nor gate D inputs high electricity to the self-con-tained unit When ordinary mail number " 1 ", which issues open command to Self controlling valve.Then, Self controlling valve is opened at once.), oil transportation general pipeline (oil transportation general pipeline is arranged between the fuel storage device of the carrier-borne aircraft and the oil transportation branch pipe of two settings parallel with one another.Its function Can convey fuel oil for two oil transportation branch pipes.), (this oil transportation branch pipe is arranged in oil transportation general pipeline and automatic control for oil transportation branch pipe Between valve.Its function is that after Self controlling valve is opened, the fuel oil for flowing through oil transportation general pipeline is conveyed to aircraft engine.), it is another (this oil transportation branch pipe is arranged between oil transportation general pipeline and manual valve one oil transportation branch pipe.Its function is, when manual valve is opened Afterwards, the fuel oil for flowing through oil transportation general pipeline is conveyed to aircraft engine.), Self controlling valve (Self controlling valve setting oil transportation general pipeline with Between one oil transportation branch pipe, which is set as normally closed type and opens and closes two valves.Its function is to receive simultaneously foundation It from the instruction for controlling output, opens or continue and remains turned-off, then connect or be still truncated from the oil transportation branch pipe to aircraft engine The access of machine conveying fuel oil.), manual valve (manual valve be arranged between oil transportation general pipeline and another oil transportation branch pipe, by warship Carrier aircraft pilot's manual manipulation.Its function is adjusted by the amount of fuel of oil transportation branch pipe input aircraft engine, and warship is then changed The flying speed of carrier aircraft.When carrier-borne aircraft is preparing to warship, pilot suitably shrinks the manual valve, then reduces the carrier-borne aircraft Warship flying speed.), aircraft engine, (input terminal of nor gate is arranged in door for this with door.Its its function is to work as pressure Sensor exports high level signal " 1 " with door to this.Meanwhile when high speed high definition camera device also goes out high level signal with door to this It, should be with door to nor gate input high level signal " 1 " after " 1 ".When pressure sensor exports low level signal " 0 " with door to this. It, should be with door to nor gate input low level meanwhile after high speed high definition camera device also exports low level signal " 0 " with door to this Signal " 0 ".) A, (input terminal of nor gate is arranged in door for this with door.Its function is, when pressure sensor is exported to this with door High level signal " 1 ".It, should be with door to nor gate meanwhile after high speed high definition camera device goes out high level signal " 1 " with door to this Input high level signal " 1 ".When pressure sensor is to this and door output low level signal " 0 ", meanwhile, when high speed high-definition camera fills It sets after also exporting low level signal " 0 " with door to this, it should be with door to nor gate input low level signal " 0 ".) B, (should be with door The input terminal of nor gate is arranged in door.Its function is, when pressure sensor exports high level signal " 1 " with door to this.Meanwhile when After high speed high definition camera device goes out high level signal " 1 " with door to this.It should be with door to nor gate input high level signal " 1 ".When Pressure sensor exports low level signal " 0 " with door to this.Meanwhile when high speed high definition camera device also exports low electricity with door to this It, should be with door to nor gate input low level signal " 0 " after ordinary mail number " 0 ".) C, nor gate (nor gate setting with door with from It controls between device.Its function is received from the level signal exported with door, and the output signal is then inputted self-con-tained unit.) D。

When with door A, with door B, with door C in, only one with door to the nor gate input high level signal " 1 ", and other When two and door are to the nor gate input low level signal " 0 ", which exports low level signal " 0 ", then inputs automatic control Device.Then, which continues to output out code to Self controlling valve.Then, Self controlling valve continues to remain turned-off.After And an oil transportation branch pipe continues to close.Then, the fuel oil of oil transportation general pipeline is flowed through, oil transportation branch pipe input aircraft hair cannot be flowed through Motivation.Then, it is preparing to the carrier-borne aircraft of warship, is just still flowed through by the carrier-borne aircraft pilot manipulation manual valve with regulation another Fuel flow in oil transportation branch pipe.Then, the carrier-borne aircraft continue to keep original reduction of speed warship state and safe warship.

When exporting low level signal " 0 " simultaneously and at the same time after inputting nor gate D with door A, with door B, with door C, this is non- Door D output high level signal " 1 ", then inputs self-con-tained unit.Then, self-con-tained unit exports open command to Self controlling valve.After And Self controlling valve is opened at once.Then, an oil transportation branch pipe is open-minded.Then, the fuel oil for flowing through oil transportation general pipeline flows through the oil transportation Branch pipe inputs aircraft engine.Then, carrier-borne aircraft accelerates to meet an urgent need at once and go around, and then successfully goes around from warship.

In order to further ensure carrier-borne aircraft, the successful emergency of especially relatively large carrier-borne aircraft is gone around, can be carrier-borne at this Rocket booster is provided on machine.The rocket booster is designed to then protect with the same program of Self controlling valve, synchronous averaging Hindering carrier-borne aircraft oiling accelerates emergency to go around, safe from warship.

Slow down warship it is an advantage of the invention that carrier-borne aircraft can receive throttle.This:

1. reducing the difficulty of carrier landing.

2. improving carrier-borne tail hooks the probability for successfully catching on check cable.

3. improving the degree of safety of carrier landing.

4. be more conducive to carrier-borne aircraft night safe warship.

5. reducing the pressure at heart of carrier-borne aircraft pilot and the immoderation of body.

6. shorten single carrier-borne aircraft the warship time, then, improve shipboard aircraft group warship, from warship efficiency.

7. reduce carrier-borne aircraft high speed warship when and type aircraft carrier deck impact force, then reduce the damage to carrier-borne aircraft.

8. reducing carrier-borne aircraft to the pulling force of check cable, various safe things caused by due to check cable is pulled off then are reduced Therefore improve the safe operating life of check cable.

9. reliable performance, easily fabricated, it is easily assembled, it is low in cost.

10. can easily be configured installation on the carrier-borne aircraft of other active services.

Detailed description of the invention: Fig. 1 is the general morphology schematic diagram of function and principle of the invention.

Fig. 2 is the function of robot control system(RCS) and device of the invention and the form schematic diagram of principle.

Specific real mode: the present invention includes: carrier-borne aircraft 1, tail hook 2, pockets 3, first check cables 4, Article 2 Check cable 5, Article 3 check cable 6, pressure sensor 7, high speed high definition camera device 8, hand push button 9, self-con-tained unit 10, oil transportation General pipeline 11, oil transportation branch pipe 12, oil transportation branch pipe 13, Self controlling valve 14, manual valve 15, aircraft engine 16, with door A and door B, and Door C, nor gate D.

When carrier-borne aircraft 1 is ready for landing warship, the pilot of the carrier-borne aircraft 1 first presses hand push button 9, connects automatic control Circuit between device 10 and Self controlling valve 14.Then, which suitably shrinks manual valve 15, to reduce carrier-borne aircraft 1 Flying speed and adjust carrier-borne aircraft 1 warship posture.Then, the tail of carrier-borne aircraft 1 hooks 2 and stretchs out, and carries out hook check cable Prepare.

When the tail of carrier-borne aircraft 1, which hooks 2, catches on first check cable 4, the signal " 1 " that pressure sensor 7 exports then is inputted With door A.When high speed high definition camera device 8 also confirmed that the tail hook 2 of carrier-borne aircraft 1 has caught on first check cable 4 simultaneously, high speed is high The signal " 1 " that clear photographic device 8 exports also inputs and door A.At this moment, it is " 1 " with the signal of door A output and inputs nor gate D.After And the signal of nor gate D output is " 0 ".And input self-con-tained unit 10.Then, self-con-tained unit 10 continues defeated to Self controlling valve 14 Out code out.Then, Self controlling valve 14 continues to remain turned-off.Then, oil transportation branch pipe 12 is not still open-minded.

When the tail of carrier-borne aircraft 1 catches on Article 2 check cable 5, pressure sensor 7 export signal " 1 " and input with Door.When high speed high definition camera device 8 also confirmed that the tail hook 2 of carrier-borne aircraft 1 has caught on Article 2 check cable 5 simultaneously, high speed high definition The signal " 1 " that photographic device 8 exports also inputs and door B.At this moment, it is " 1 " with the signal of door B output and inputs nor gate D.After And the signal of nor gate D output is " 0 " and inputs self-con-tained unit 10.Then, self-con-tained unit 10 is continued to output to Self controlling valve 14 Out code.Then, Self controlling valve 14 continues to remain turned-off.Then, oil transportation branch pipe 12 is not still open-minded.

When carrier-borne aircraft 1 tail hook 2 catch on Article 3 check cable 6 when, pressure sensor 7 export signal " 1 " and input with Door C；When high speed high definition camera device 8 also confirmed that the tail hook 2 of carrier-borne aircraft 1 has caught on Article 3 check cable 6 simultaneously, high speed high definition The signal " 1 " that photographic device 8 exports also inputs and door C.At this moment, it is " 1 " with the signal of door C output and inputs nor gate D.After And the signal of nor gate D output is " 0 " and inputs self-con-tained unit 10.Then, self-con-tained unit 10 is continued to output to Self controlling valve 14 Out code.Then, Self controlling valve 14 continues to remain turned-off.Then, oil transportation branch pipe 12 is not still open-minded.

This is because the logic function of nor gate D itself determines: that is, when with door A, with door B, with door C in, only one A and door to nor gate D input high level signal " 1 ", and other two with Men Junxiang nor gate D input low level signal When " 0 ", nor gate D exports low level signal " 0 ", then inputs self-con-tained unit 10.Then, self-con-tained unit 10 is to Self controlling valve 14 continue to output out code.Then, Self controlling valve 14 continues to remain turned-off.Then, oil transportation branch pipe 12 is not still open-minded.Then, The fuel oil of oil transportation general pipeline 11 is flowed through, oil transportation branch pipe 12 cannot be flowed through and input aircraft engine 16.In this way, carrier-borne aircraft 1 is just still It is constant to remain original warship situation of slowing down, up to 1 safety of carrier-borne aircraft warship.

Conversely, the signal that pressure sensor 7 exports becomes when the tail of carrier-borne aircraft 1 hook 2 fails to catch on first check cable 4 For " 0 " and input and door A.Meanwhile high speed high definition camera device 8 also confirms carrier-borne aircraft) tail hook 2 and fail to catch on first and block Output signal when rope 4 becomes also as " 0 " and input and door A.At this moment, the output signal with door A becomes " 0 " and inputs nor gate D. Then, the signal of nor gate D output continues as " 0 " and inputs self-con-tained unit 10.

Then, when the tail of carrier-borne aircraft 1, which hooks 2, to be continued to fail to catch on Article 2 check cable 5 again, what pressure sensor 7 exported Signal becomes " 0 " and inputs and door B.Meanwhile high speed high definition camera device 8 also confirms that the tail of carrier-borne aircraft 1 hooks 2 and fails to catch on second Output signal becomes " 0 " and inputs and door B when check cable 5.At this moment, the output signal with door B becomes " 0 " and inputs nor gate D.Then, the signal of nor gate D output continues as " 0 " and inputs self-con-tained unit 10.

Then, when the tail of carrier-borne aircraft 1, which hooks 2, to be continued to fail to catch on Article 3 check cable 6, the letter of the output of pressure sensor 7 Number become " 0 " and inputs and door C.Meanwhile high speed high definition camera device 8 also confirms that the tail of carrier-borne aircraft 1 hooks 2 and fails to catch on Article 3 When check cable 6, output signal becomes " 0 " and inputs and door C.At this moment, the output signal with door C becomes " 0 " and inputs nor gate D.Then, the signal of nor gate D output continues as " 0 " and inputs self-con-tained unit 10.

At this moment, fail to catch on first check cable 4 since the tail of carrier-borne aircraft 1 hooks 2, then, the tail of carrier-borne aircraft 1 hooks 2 again not Article 2 check cable 5 can be caught on；Then, the tail of carrier-borne aircraft 1, which hooks 2 and fails to catch on Article 3 again, blocks 6.As a result, due to carrier-borne aircraft 1 Tail hooks and 2 ultimately fails to catch on: first check cable 4, Article 2 check cable 5, Article 3 block any bar in 6, at this point, with door A, Low level signal " 0 " is just exported simultaneously with door B, with door C and at the same time input nor gate D.Since the logic function of nor gate D is determined It is fixed: only when and at the same time after inputting nor gate D, nor gate D is just exported output signal " 0 " simultaneously by door A and door B and door C High level signal " 1 " simultaneously inputs self-con-tained unit 10.Then, self-con-tained unit 10 exports open command to Self controlling valve 14；Then, certainly Control valve 14 is opened at once；Then, oil transportation branch pipe 12 is open-minded；Then, the fuel oil for flowing through oil transportation general pipeline 11 flows through oil transportation branch pipe 12 input aircraft engines 16；Then, carrier-borne aircraft 1 just accelerates to meet an urgent need at once and go around, and then safe overshoot is from warship.

Claims (1)

1. can promote ensure aircraft carrier safety the device of warship, feature include: carrier-borne aircraft (1), tail hook (2), accommodate Groove (3), first check cable (4), Article 2 check cable (5), Article 3 check cable (6), pressure sensor (7), high speed are high Clear photographic device (8), hand push button (9), self-con-tained unit (10), oil transportation general pipeline (11), oil transportation branch pipe (12), oil transportation branch pipe (13), Self controlling valve (14), manual valve (15), aircraft engine (16) and door (A) and door (B) and door (C), nor gate (D)；Tail hooks (2) and is arranged in the tail portion of carrier-borne aircraft (1) body；Pockets (3) setting hooks on (2) in tail；First check cable (4) it is arranged at type aircraft carrier deck tail portion；Article 2 check cable (5) is arranged at type aircraft carrier deck tail portion, with first check cable (4) Keep certain intervals；Article 3 check cable (6) is arranged at type aircraft carrier deck tail portion, between keeping certain with Article 2 check cable (5) Every；The middle part that pressure sensor (7) is arranged at the slot bottom of pockets (3)；High speed high definition camera device (8) is arranged carrier-borne At the tail portion of machine (1) body and front closely alignment tail hook (2), in order to ensure carrier-borne aircraft (1) night warship safety, high speed High definition camera device (8) is provided with night vision function；Hand push button (9) is arranged between self-con-tained unit (10) and Self controlling valve (14) Circuit on, malfunction occurs for Self controlling valve (14) in order to prevent, and hand push button (9) is set as button open in usual；Automatic control dress (10) setting is set in the output end of nor gate (D)；The fuel storage device and two in the carrier-borne aircraft (1) is arranged in oil transportation general pipeline (11) Between the oil transportation branch pipe (12) and oil transportation branch pipe (13) of item setting parallel with one another；Oil transportation branch pipe (12) is arranged in oil transportation general pipeline (11) Between Self controlling valve (14)；Oil transportation branch pipe (13) is arranged between oil transportation general pipeline (11) and manual valve (15)；Self controlling valve (14) it is arranged between oil transportation general pipeline (11) and oil transportation branch pipe (12), Self controlling valve (14) is set as normally closed type and opens and closes two Position valve；Manual valve (15) is arranged between oil transportation general pipeline (11) and oil transportation branch pipe (13)；It is arranged with door (A) in nor gate (D) input terminal；The input terminal in nor gate (D) is set with door (B)；The input terminal in nor gate (D) is set with door (C)；Or The input terminal in self-con-tained unit (10) is arranged in NOT gate (D)；In order to further ensure carrier-borne aircraft (1), especially relatively large is carrier-borne The successful emergency of machine (1) is gone around, and can be provided with rocket booster on carrier-borne aircraft (1), which is designed to Then further ensure that the oiling of carrier-borne aircraft (1) accelerates emergency to go around with the same program of Self controlling valve (14), synchronous averaging；This hair It is bright to be configured installation on the carrier-borne aircraft (1) of other active services with can be convenient.