CN1962363A - Method for omnidirectionally preventing flying bird from collision of turbine jet plane - Google Patents
Method for omnidirectionally preventing flying bird from collision of turbine jet plane Download PDFInfo
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- CN1962363A CN1962363A CN200610154701.6A CN200610154701A CN1962363A CN 1962363 A CN1962363 A CN 1962363A CN 200610154701 A CN200610154701 A CN 200610154701A CN 1962363 A CN1962363 A CN 1962363A
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- metal guard
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Abstract
The invention relates to a method for avoiding bird to impact turbine injection plane, wherein it fixes anti-impact metal frame at the front air inlet of plane; the metal frame has not lower parameters than the plane; its appearance is taper; when landing and starting, the blades of turbine engine rotate in high speed, the metal frame can confirm enough airflow and avoid bird into engine. The invention has taper shape to reduce the air resistance.
Description
Affiliated technical field
The present invention relates to a kind of turbo type jet airplane, particularly can prevent the method for aerial bird strike, suction aircraft turbojet engine turbo type jet airplane.
Background technology
The automotive gas turbine formula propelling unit that jet plane adopts, take off and in-flight the impeller high speed revolution of angle of rake turbine engine produce powerful negative pressure, admission port at the turbine engine front end forms high-revolving charge flow, head-on sudden birds had strong suction, impulse turbine driving engine during in case birds suck, cause the mechanical accidents such as blade infringement, engine off of turbine engine, cause when serious that turbine engine crashes, and causes the airplane crash of air crash.The admission port that can affirm the turbine engine front end is key and weak locating in the bird strike.
From the birth of jet plane so far the accident that causes of the turbine engine of bird strike aircraft never stopped, increasing along with jet power aircraft and flight is because the aircraft accident of bird strike aircraft accident and disaster also increases thereupon.Though be military jet airplane, civil aviaton's jet airplane with aerial bird strike, suck in the aircraft turbojet engine, all can cause the sudden mechanical breakdown of aircraft, the serious air crash that directly causes takes place; From recent newspaper, Internet report, the world all has everywhere to happen occasionally because the birds of bird strike aircraft suck the accident of aircraft turbojet engine; Solve the bird strike aircraft, the generation of stopping airplane crash has caused the concern of the world today.
The existence of birds is all arranged in human lives's space, the activity space sea level elevation of birds on high from several meters all be its action radius to the full kms of number, at peri-urban numerous sparrows, dove group are arranged; Various eagles in mountain forest; Coastal the seabirds such as sea-gull that circle in the air are arranged, even in the aerial threat that far flies all may cause aircraft navigation that has migratory birds such as various wild geese, swan to gather in groups band together everywhere of last km.From the plateau to the Plain, the birds that grow on trees from the continent to the ocean are engraved in when having the space of flying with their and are threatening aloft jet plane.Particularly the airport all is in trees, lawn and the pasture and water fish pond of greening vegetation around the airport of open area of outskirts of a town combination, it all is the place that various birds are looked for food and perch, a large amount of sparrows, the rock dove of peri-urban existence, has extremely strong adaptive capacity, birds flight in groups has sudden, the a slice of gathering in groups band together during flight still can be taken precautions against the management aspect in the airport.For beyond the airport, be in the open area of outskirts of a town combination, in the peri-urban growth numerous sparrows, dove group are arranged, have extremely strong adaptive capacity, a slice of gathering in groups band together during flight; Trees, lawn and the pasture and water fish pond of greening vegetation all are the places that various birds are looked for food and perch around the airport.For numerous flying birds in the mountain forest and large-scale eagle; What have everywhere aloft in addition that various migratory birds gather in groups band together far flies (wild goose, swan etc.).More some large-scale transient migrates in groups and flies in the convective zone on cloud layer, and radar can not find that aviator's sight line does not catch up with the speed of aircraft, is hard to guard against in fact;
At present, the known method that prevents the bird strike aircraft is all limited to and is taken off, when landing the finite space around the airport is taken precautions against, the high-wall trammel net is set around each airport runways, on the airport and be provided with the aerial flying bird that special personnel, equipment troop cooperate the strong sound wave device to tackle around the airport and become to catching up with, find that flying bird adopts the method for mode warn birds such as coal gas big gun, firecrackers.For example, international airport, Xiaoshan, Hangzhou is just set up sole duty at the initial stage of setting up and is driven bird team, drive the bird team member and adopt modes such as trammel net, coal gas big gun, firecrackers to drive bird throughout the year, employ millions of circles simultaneously and drive bird and a whole set of acoustic control machine equipment from external introduction car and drive flying bird around the airfield runway.Reach the purpose that becomes to catching up with the bird of taking off, when landing the bird of the airflight around the airport is discharged the flight of strong sound scaring, shoot dead by force in case of necessity and become to catching up with.All airports, various countries are preventing that the bird strike aircraft from all adopting similar approach for this reason, have employed the consumption of great amount of manpower and material resources, financial resources separately.Along with aircraft and flight constantly increase, from the plateau to the Plain, the wide birds activity space from the continent to the ocean, and all spaces have no idea at all to prevent that flying bird and aircraft impact from causing that the air crash of sudden turbo-machine mechanical breakdown takes place beyond on the airport.Just because of present technical method adopts the airport to defend bird strike aircraft method on every side all is extremely passive, and the strick precaution scope is little.So this orthodox method for many years worldwide all can not fully, effectively solve because the birds of bird strike aircraft suck the fact that the accident of aircraft turbojet engine takes place.From recent newspaper, Internet report, all have everywhere because the accident of the birds of bird strike aircraft suction aircraft turbojet engine happens occasionally in the world; Consequently human and birds are ended in defeat for both sidesboth suffer losses; Solve the accident of bird strike aircraft, the generation of stopping airplane crash has become world today's property difficult problem.
Summary of the invention
In order to overcome the existing deficiency of the method for bird strike aircraft birds suction aircraft turbojet engine, the passive situation that take precautions against change aspect, airport of preventing, fundamentally eliminate the generation of bird strike aircraft accident; The invention provides a kind of actv., prevent that effectively birds from sucking the method for aircraft turbojet engine comprehensively.This method has not only been guaranteed omnibearingly in the taking off of aircraft, landing and the whole flight way to prevent that effectively bird strike aircraft birds from sucking the aircraft turbojet engine, and has fundamentally been ensured the comprehensive safe flight of aircraft.
The technical solution adopted for the present invention to solve the technical problems is: the metal guard that fixedly mounts a protecting against shock in the front end air inflow point of the angle of rake turbojet engine of each jet airplane automotive gas turbine formula, the metal guard is tapered or trapezoidal according to the profile mechanism processing of the front end air inflow point of the angle of rake turbojet engine of aircraft gas turbines formula, taper or trapezoidal 30 ~ 90 degree that are; When taking off and the impeller high speed revolution of angle of rake turbine engine in-flight, the metal guard can guarantee that sufficient air communication crosses and can stop birds to suck the aircraft turbojet engine at the turbine engine front end; The metal guard is the taper of rocket head or sub warhead, can overcome many deficiencies of planar metal guard; Can reduce air resistance on taper or the trapezium structure, prevent bird strike, the breathing area greater than the turbo-machine admission port is arranged, prevent that with timeliness birds from sucking the purpose that the aircraft turbojet engine reaches in the influx that does not reduce air.
The invention has the beneficial effects as follows,
1, can in the airport, ensure the safety of taking off, landing of aircraft.
2, the omnibearing birds suction aircraft turbojet engine that effectively prevents in whole flight whole process guarantees aircraft safety flight.
3, have simple in structure, processing, easy for installation, anti-bird is comprehensive whenever and wherever possible, and is with low cost, effect is direct.Slight metal guard just can be avoided aspect, airport personnel, input that equipment is huge.
The specific embodiment
Because the type of jet airplane is numerous, it is different that combustion gas wheel propelling unit is in the position of each aircraft, various propelling unit front end air entry shapes are different, and concrete enforcement need be in the position of aircraft according to the combustion gas wheel propelling unit of jet airplane, the profile mechanism of propelling unit front end air entry shape decision metal guard processes tapered or trapezoidal; Import has separate space to adopt the cone-shaped metal guard to install and fix for the propelling unit front end air, can keep steady air current; For propelling unit front end air import compactness about fuselage or below aircraft, can adopt trapezoidal metal guard to be installed in fuselage and propelling unit front end air inflow point is fixed.The metal guard must adopt every technical index of material to be not less than the requirement of the surface metal of aircraft own.The breathing area that the cone-shaped metal guard has more than 2 times can not reduce ventilation area; The metal guard is conical or trapezoidal half-conical streamline contour according to aircraft configuration mechanism, run into the protecting against shock effect that the head-on sudden birds overwhelming majority slips over metal guard conical suface, injury probability to brunt metal guard awl point as same bullet hits is very little, though can injure flying bird, can save the safety of the intact and aero-engine of metal guard from damage; Thereby can avoid the injury of the frontal impact turbine wheel of birds fully, reach people, aircraft and birds and live together peacefully, realize peaceful coexistence human and natural biology.
Claims (3)
1, a kind of comprehensive method that prevents the turbojet of bird strike is characterized in that the metal guard at a front end air inflow point fixed installation protecting against shock of the angle of rake turbojet engine of each jet airplane automotive gas turbine formula,
2, metal guard according to claim 1 is characterized in that: the profile mechanism processing according to aircraft front end air inflow point is tapered or trapezoidal,
3, the profile mechanism of metal guard according to claim 2 processing is tapered or trapezoidal, it is characterized in that: tapered or trapezoidal 30~90 degree that are of profile mechanism processing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN200610154701.6A CN1962363A (en) | 2006-11-21 | 2006-11-21 | Method for omnidirectionally preventing flying bird from collision of turbine jet plane |
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CN200610154701.6A CN1962363A (en) | 2006-11-21 | 2006-11-21 | Method for omnidirectionally preventing flying bird from collision of turbine jet plane |
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CN1962363A true CN1962363A (en) | 2007-05-16 |
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CN200610154701.6A Pending CN1962363A (en) | 2006-11-21 | 2006-11-21 | Method for omnidirectionally preventing flying bird from collision of turbine jet plane |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2011091591A1 (en) * | 2010-01-29 | 2011-08-04 | Zhang Haihu | Anti-impaction net of aero plane engine |
CN102320377A (en) * | 2011-06-28 | 2012-01-18 | 金平 | Anti-collision aircraft engine |
CN103803091A (en) * | 2014-02-25 | 2014-05-21 | 顾天罡 | Active type bird strike prevention method and device for aircraft |
CN103979111A (en) * | 2014-04-24 | 2014-08-13 | 马同金 | Airplane bird breaking mesh cutter |
CN110889172A (en) * | 2019-12-04 | 2020-03-17 | 中国直升机设计研究所 | Method for prefabricating impact damage of helicopter rotor system |
-
2006
- 2006-11-21 CN CN200610154701.6A patent/CN1962363A/en active Pending
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2011091591A1 (en) * | 2010-01-29 | 2011-08-04 | Zhang Haihu | Anti-impaction net of aero plane engine |
CN102320377A (en) * | 2011-06-28 | 2012-01-18 | 金平 | Anti-collision aircraft engine |
CN103803091A (en) * | 2014-02-25 | 2014-05-21 | 顾天罡 | Active type bird strike prevention method and device for aircraft |
CN103803091B (en) * | 2014-02-25 | 2015-10-28 | 顾天罡 | Aircraft hits method and device with active anti-bird |
CN103979111A (en) * | 2014-04-24 | 2014-08-13 | 马同金 | Airplane bird breaking mesh cutter |
CN103979111B (en) * | 2014-04-24 | 2016-10-26 | 马同金 | Aircraft broken trammel net cover cutter |
CN110889172A (en) * | 2019-12-04 | 2020-03-17 | 中国直升机设计研究所 | Method for prefabricating impact damage of helicopter rotor system |
CN110889172B (en) * | 2019-12-04 | 2023-03-28 | 中国直升机设计研究所 | Method for prefabricating impact damage of helicopter rotor system |
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Open date: 20070516 |