CN107856874B - Grabbing net type carrier-based aircraft arresting device - Google Patents

Grabbing net type carrier-based aircraft arresting device Download PDF

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Publication number
CN107856874B
CN107856874B CN201711064832.XA CN201711064832A CN107856874B CN 107856874 B CN107856874 B CN 107856874B CN 201711064832 A CN201711064832 A CN 201711064832A CN 107856874 B CN107856874 B CN 107856874B
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China
Prior art keywords
arresting
aircraft
net
carrier
sliding trolley
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Expired - Fee Related
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CN201711064832.XA
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Chinese (zh)
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CN107856874A (en
Inventor
杨飏
陈壮
秦静远
黄瑞欣
喻巧
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Dalian University of Technology
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Dalian University of Technology
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/02Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)

Abstract

The invention discloses a catching net type carrier-based aircraft arresting device, which comprises: the aircraft comprises two parallel slideways arranged on an aircraft carrier deck, a damper and an ejector arranged at the tail end of a carrier-based aircraft; each slideway is provided with a sliding trolley which is matched with the slideway to slide, a barrier net is vertically fixed above each sliding trolley, and the extending direction of the barrier net is the same as that of the slideway; the barrier net is hinged at the upper end of the sliding trolley, and the sliding trolley is connected with the damper through a cable; the ejector is capable of ejecting the arresting cable to the left side and the right side, the ejection head part of the arresting cable is provided with a grapple which is matched with meshes of the arresting net to be firmly grabbed; when the shipboard aircraft lands, the arresting cables are horizontally ejected from the tail of the shipboard aircraft to the arresting nets on the two sides at the same time, when the arresting nets are buckled by the grapple catches of the arresting cables, the shipboard aircraft which lands slides on the deck, and the arresting cables drive the arresting nets to consume energy through the dampers, so that the effect of reducing the speed and arresting is achieved for the shipboard aircraft.

Description

Grabbing net type carrier-based aircraft arresting device
Technical Field
The invention relates to a shipboard aircraft landing auxiliary device, in particular to a grabbing net type shipboard aircraft arresting device.
Background
In the existing technology, the arresting of the shipboard aircraft is mostly realized by adopting an arresting cable technology and through the hooking of a tail hook of the shipboard aircraft and the arresting cable. However, successful engagement of the tail hook with the arrester cord is associated with a number of factors, including: the hooking between the tail hook and the arresting cable is prone to errors due to landing opportunity, the speed per hour of the carrier-based aircraft, psychological factors of pilots, weather factors, visibility factors and the like, and therefore the successful hooking of the carrier-based aircraft cannot be guaranteed. If the tail hook of the carrier-based aircraft cannot successfully hook the arresting cable, arresting fails, if the tail hook is light, the pilot flies again to prepare for secondary arresting, and if the tail hook is heavy, the carrier-based aircraft crashes to crash or fails to fly again, and then the aircraft is damaged and people die.
The similar invention is mainly focused on the energy consumption aspect of the arresting cable after the carrier-based aircraft lands. The method includes but is not limited to energy dissipation by means of hydraulic pressure, turbine power, electromagnetic effect and the like, and the energy dissipation is carried out to enable the energy dissipation to drive the piston to move so as to carry out energy consumption and speed reduction, so that the speed reduction effect on the carrier-based aircraft sliding at a high speed is realized. However, if the tail hook is not hung with the arrester wire fixed with the ground after the carrier-based aircraft lands, the speed reducing device has no meaning.
Disclosure of Invention
Aiming at the technical problems, the invention provides a net-grabbing type carrier-based aircraft arresting device capable of carrying out secondary grabbing.
In order to achieve the purpose, the method is realized by the following technical scheme:
a net-grabbing type carrier-based aircraft arresting device, comprising: the aircraft carrier comprises two parallel slideways arranged on an aircraft carrier deck, a damper arranged below the slideways and an ejector arranged at the tail end of a carrier-based aircraft;
each slide way is provided with a sliding trolley which slides with the slide way, a barrier net is vertically fixed above each sliding trolley, and the extending direction of the barrier net is the same as that of the slide way;
ensuring that the vertical state interval of the arresting net meets the width required by the landing of the shipboard aircraft, wherein the length of the arresting net is determined according to the actual sliding energy consumption requirement of the berthing of the shipboard aircraft;
the arresting net is hinged at the upper end of the sliding trolley, a driving device for driving the arresting net to be vertical to the upper end surface of the sliding trolley from a flat laying state is arranged on the sliding trolley, and the sliding trolley is connected with the damper through a cable;
the ejector is capable of ejecting the barricade to the left side and the right side, the ejection head of the barricade is provided with a grapple, and the grapple is matched with meshes of the barricade net to be firmly grabbed.
By adopting the technical scheme, when the carrier-based aircraft is not landed, the arresting net is in a lodging state, when the carrier-based aircraft approaches the aircraft carrier, the arresting net is firstly changed into an upright state (under the drive of the sliding trolley driving device) from the lodging state, meanwhile, the carrier-based aircraft is prepared for ejecting the tail arresting cable, the monitoring radar on the carrier-based aircraft can measure the position suitable for ejecting the arresting cable, after the carrier-based aircraft is landed on the aircraft carrier, when the carrier-based aircraft slides over the arresting net, the feedback sensor returns an instruction, the ejector at the tail of the carrier-based aircraft ejects the arresting cable, and after the arresting cable is grabbed by the grabbing hook of the arresting cable, the two pieces of the arresting cable start to cooperate with the arresting work, if the arresting cable is not grabbed, the second-time hook throwing is started immediately, and the combination of the tail hook claw and the net surface can be ensured due. The arrester wire grapple grabs the arrester net and then drives the sliding trolley to slide on the slideway, and the sliding trolley is connected with the damper under the deck through the cable so as to be decelerated and landed by the carrier-based aircraft. And after the speed reduction and the falling of the carrier-based aircraft are finished, the arresting net can be withdrawn along the slideway and redeployed.
In conclusion, when the carrier-based aircraft lands on a ship, the grapple is ejected to the two horizontal sides and hooked with the arresting nets on the two sides of the runway to achieve the effect of deceleration and arresting. Different from the traditional arresting system which needs high precision, the slide way type arresting net has larger receiving area, can be combined with a tail hook claw ejected by a machine body more easily, can be ejected again at any time because the arresting net can synchronously slide along a slide way along with an airplane, obviously reduces failure and secondary re-flying rate, and ensures that a carrier-based airplane can safely and accurately land an aircraft carrier deck.
The foregoing description is only an overview of the technical solutions of the present invention, and in order to make the technical means of the present invention more clearly understood, the present invention may be implemented in accordance with the content of the description, and in order to make the above and other objects, features, and advantages of the present invention more clearly understood, the following preferred embodiments are described in detail with reference to the accompanying drawings.
Drawings
The invention is shown in 6 figures, wherein:
FIG. 1 is a schematic diagram of a shipboard aircraft of the present invention before landing;
FIG. 2 is a schematic diagram of the carrier-based aircraft of the present invention in preparation for landing;
FIG. 3 is a schematic diagram of the landing of the carrier-based aircraft of the present invention;
FIG. 4 is an isometric view of the carrier landing of the present invention;
FIG. 5 is a schematic view of a grapple of the present invention;
fig. 6 is an enlarged view of a portion of the barrier net of the present invention.
Detailed Description
As shown in fig. 1, 2, 3, 4, 5 and 6, the net-type carrier-based aircraft arresting device includes: the aircraft carrier comprises two parallel slideways 3 arranged on an aircraft carrier deck 1, a damper 7 arranged below the slideways 3 and an ejector 6 arranged at the tail end of a carrier-based aircraft 2;
each slide way 3 is provided with a sliding trolley which slides with the slide way, a barrier net 4 is vertically fixed above each sliding trolley, and the extending direction of the barrier net 4 is the same as that of the slide way 3;
ensuring that the vertical state interval of the arresting nets 4 meets the required width for landing of the shipboard aircraft 2, wherein the arresting nets 4 are determined according to the actual requirement of the shipboard aircraft 2;
the arresting net 5 is hinged at the upper end of the sliding trolley, a driving device for driving the arresting net 5 to be vertical to the upper end surface of the sliding trolley from a flat laying state is arranged on the sliding trolley, and the sliding trolley is connected with the damper 7;
the ejector 6 can eject the arresting cable 5 to the left side and the right side, and the ejection head of the arresting cable 5 is provided with a grapple which is matched with meshes of the arresting net 4 for being firmly grabbed.
By adopting the technical scheme, when the carrier-based aircraft 2 is not landed, the arresting net 4 is in a lodging state, when the carrier-based aircraft 2 approaches to an aircraft carrier, firstly, the arresting net 4 is changed into an upright state (under the drive of a sliding trolley driving device) from the lodging state, meanwhile, the carrier-based aircraft 2 is prepared for ejection of the tail arresting cable 5, a monitoring radar on the carrier-based aircraft 2 can measure the position suitable for ejecting the arresting cable 5, after the carrier-based aircraft 2 is landed, when the carrier-based aircraft 2 slides over the arresting net 4, a feedback sensor returns an instruction (a ground sensing feedback device which is arranged on a deck and corresponds to the arresting net), as long as the carrier-based aircraft passes through the ground where the arresting net is located, and the ground sensing feedback device feeds back a signal, the arresting cable can be ejected, the ejector 6 at the tail of the carrier-based aircraft ejects the arresting cable 5, after the arresting net 4 is caught by a catching hook of the arresting cable 5, the arresting net 4 and the arresting net and the ejector 6, immediately starting to throw the hook for the second time, and ensuring the combination of the tail hook claw and the net surface because of the huge net surface. The grab hook 5 grabs the arresting net 4 and then drives the sliding trolley to slide on the slideway 3, and the sliding trolley is connected with the damper 7 under the deck through a cable for the speed reduction landing of the carrier-based aircraft. When the speed reduction and the descent of the carrier-based aircraft are completed, the arresting net 4 can be withdrawn along the slideway and redeployed.
Although the present invention has been described with reference to a preferred embodiment, it should be understood that various changes, substitutions and alterations can be made herein without departing from the spirit and scope of the invention as defined by the appended claims.

Claims (1)

1. The utility model provides a net formula carrier-borne aircraft arresting device which characterized in that includes:
the aircraft carrier comprises two parallel slideways (3) arranged on an aircraft carrier deck (1), a damper (7) arranged below the slideways (3) and an ejector (6) arranged at the tail end of a carrier-based aircraft (2);
each slideway (3) is provided with a sliding trolley which is matched with the slideway to slide, a barrier net (4) is vertically fixed above each sliding trolley, and the extending direction of each barrier net (4) is the same as that of the slideway (3);
the arresting net (4) is hinged at the upper end of the sliding trolley, a driving device for driving the arresting net (4) from a flat laying state to a state perpendicular to the upper end surface of the sliding trolley is arranged on the sliding trolley, and the sliding trolley is connected with the damper (7);
the ejector (6) can eject the barricade (5) to the left side and the right side, a grapple is arranged at the ejection head part of the barricade (5), and the grapple is matched with meshes of the barricade net (4) to be firmly grabbed.
CN201711064832.XA 2017-11-02 2017-11-02 Grabbing net type carrier-based aircraft arresting device Expired - Fee Related CN107856874B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711064832.XA CN107856874B (en) 2017-11-02 2017-11-02 Grabbing net type carrier-based aircraft arresting device

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Application Number Priority Date Filing Date Title
CN201711064832.XA CN107856874B (en) 2017-11-02 2017-11-02 Grabbing net type carrier-based aircraft arresting device

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CN107856874A CN107856874A (en) 2018-03-30
CN107856874B true CN107856874B (en) 2021-01-15

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110589005B (en) * 2018-06-12 2022-12-06 王振牛 Rescue method for injured fighter aircraft abnormal deflection aircraft carrier
CN109625305B (en) * 2018-12-04 2024-02-13 青岛启航弹射科技有限公司 Unmanned aerial vehicle recovery unit
CN110703799B (en) * 2019-10-28 2021-09-24 大连理工大学 Multi-carrier-based aircraft cooperative deck surface sliding track planning method based on centralized optimal control

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB578440A (en) * 1943-04-15 1946-06-28 Phillips & Powis Aircraft Ltd Improvements in aircraft arrester gear and in methods of landing aircraft on ships and other confined spaces
US5653308A (en) * 1995-08-07 1997-08-05 White; Lawrence G. Safety net support array
CN205203416U (en) * 2015-11-13 2016-05-04 中国人民解放军国防科学技术大学 Formula unmanned aerial vehicle recovery system is retired to carrier -borne track that receive and releases
CN105799946A (en) * 2016-04-27 2016-07-27 武汉大学 Airplane safe forced landing assisting system and safe forced landing method
CN205952314U (en) * 2016-08-11 2017-02-15 深圳光启空间技术有限公司 Unmanned aerial vehicle launching appliance
CN106892129A (en) * 2017-03-22 2017-06-27 哈尔滨工业大学 A kind of small-sized fixed-wing unmanned plane recovery system
CN107031861A (en) * 2017-06-07 2017-08-11 滨州学院 Unmanned plane retracting device

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB578440A (en) * 1943-04-15 1946-06-28 Phillips & Powis Aircraft Ltd Improvements in aircraft arrester gear and in methods of landing aircraft on ships and other confined spaces
US5653308A (en) * 1995-08-07 1997-08-05 White; Lawrence G. Safety net support array
CN205203416U (en) * 2015-11-13 2016-05-04 中国人民解放军国防科学技术大学 Formula unmanned aerial vehicle recovery system is retired to carrier -borne track that receive and releases
CN105799946A (en) * 2016-04-27 2016-07-27 武汉大学 Airplane safe forced landing assisting system and safe forced landing method
CN205952314U (en) * 2016-08-11 2017-02-15 深圳光启空间技术有限公司 Unmanned aerial vehicle launching appliance
CN106892129A (en) * 2017-03-22 2017-06-27 哈尔滨工业大学 A kind of small-sized fixed-wing unmanned plane recovery system
CN107031861A (en) * 2017-06-07 2017-08-11 滨州学院 Unmanned plane retracting device

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Inventor after: Yang Yang

Inventor after: Chen Zhuang

Inventor after: Qin Jingyuan

Inventor after: Huang Ruixin

Inventor after: Yu Qiao

Inventor before: Yang Yang

Inventor before: Qin Jingyuan

Inventor before: Huang Ruixin

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Inventor before: Yu Qiao

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Granted publication date: 20210115