CN107985622A - A kind of aircraft arresting cable supporting structure - Google Patents

A kind of aircraft arresting cable supporting structure Download PDF

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Publication number
CN107985622A
CN107985622A CN201711220887.5A CN201711220887A CN107985622A CN 107985622 A CN107985622 A CN 107985622A CN 201711220887 A CN201711220887 A CN 201711220887A CN 107985622 A CN107985622 A CN 107985622A
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CN
China
Prior art keywords
supporting structure
hook
check cable
cable
aircraft
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201711220887.5A
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Chinese (zh)
Other versions
CN107985622B (en
Inventor
孔凡超
张家仙
李茂�
王成刚
孙凤伟
宋舟航
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Beijing Institute of Aerospace Testing Technology
Original Assignee
Beijing Institute of Aerospace Testing Technology
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Filing date
Publication date
Application filed by Beijing Institute of Aerospace Testing Technology filed Critical Beijing Institute of Aerospace Testing Technology
Priority to CN201711220887.5A priority Critical patent/CN107985622B/en
Publication of CN107985622A publication Critical patent/CN107985622A/en
Application granted granted Critical
Publication of CN107985622B publication Critical patent/CN107985622B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND 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
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/02—Arresting gear; Liquid barriers

Abstract

The present invention provides a kind of check cable (2) supporting structure, and for (4) unmanned plane when runway landing is slided and run, (5) airplane wheel or (6) arrester hook have the probability for hitting check cable (2) supporting structure.When airplane wheel (5) or arrester hook (6) strike (2) supporting structure, lateral component is produced to (2) supporting structure, (2) supporting structure can be translated toward side, avoid influencing (6) arrester hook (3) hook check cable.The present invention is by the specific shape face of support structure designs, ensureing that supporting structure can avoid when being collided, improving the success rate of aircraft arrestment.

Description

A kind of aircraft arresting cable supporting structure
Technical field
The present invention relates to aircraft arresting cable to block field, and effect is that the supporting structure for reducing check cable hooks aircraft arrestment The influence of hook success rate.
Background technology
Field is blocked in aircraft arresting cable, the check cable length of aircraft arresting system is long, in order to ensure aircraft arrestment Check cable on the smooth hook of hook, check cable must have supporting structure.Under certain probability, airplane wheel or arrester hook can strike branch Support structure, influences the success rate of aircraft arrestment.
Traditional aircraft arresting cable is supported using steel wire, and steel wire support can destroy runway；Or using wheel support, wheel Shape lack special design, and the success blocked is influenced after arrester hook collision.
The content of the invention
1 technical problems to be solved
The check cable length of aircraft arresting system is long, in order to ensure check cable on the smooth hook of aircraft arrestment hook, blocks Suo Bixu has supporting structure, and existing probability airplane wheel or arrester hook directly impinge supporting structure, can influence aircraft arrestment Success；The present invention is by the specific shape face of support structure designs, ensureing that supporting structure can avoid when being collided, improving and fly The success rate that machine blocks.
2 technical solutions
Certain fixed-wing unmanned plane arresting system, employs diameter 10mm steel wire ropes and is used as (3) check cable, (2) supporting structure It is pre-installed on (3) check cable, (4) check cable two is (1) damper.
(2) (8) centre bore is set among supporting structure, (3) check cable is gone through from (8) centre bore, (2) supporting structure and (3) there are 0.5mm~1mm gaps between check cable, (2) supporting structure side is (7) scalene cone, the included angle A between two sides For 10 °~20 °.
(4) for unmanned plane when runway landing is slided and run, there is shock check cable (2) branch in (5) airplane wheel or (6) arrester hook The probability of support structure.When airplane wheel (5) or arrester hook (6) strike (2) supporting structure, side is produced to (2) supporting structure To component, (2) supporting structure can toward side translate, avoid influence (6) arrester hook (3) hook check cable.
Brief description of the drawings
Attached drawing 1 is a kind of scheme of installation of aircraft arresting cable supporting structure of the present invention
Attached drawing 2 is a kind of appearance schematic diagram of aircraft arresting cable supporting structure of the present invention
Wherein：
(1)-damper
(2)-aircraft arresting cable supporting structure
(3)-steel wire rope
(4)-aircraft
(5)-airplane wheel
(6)-arrester hook
(7)-scalene cone
(8)-centre bore
Angle between A- two sides
Embodiment
Certain fixed-wing unmanned plane arresting system, employs diameter 10mm steel wire ropes and is used as (3) check cable, (2) supporting structure It is pre-installed on (3) check cable, (4) check cable two is (1) damper.
(2) there are 0.5mm gaps between supporting structure and (3) check cable, (2) supporting structure side is (7) scalene cone, is cut Angle is 15 ° on face.
(4) for unmanned plane when runway landing is slided and run, there is shock check cable (2) branch in (5) airplane wheel or (6) arrester hook The probability of support structure.When airplane wheel (5) or arrester hook (6) strike (2) supporting structure, side is produced to (2) supporting structure To component, (2) supporting structure can toward side translate, avoid influence (6) arrester hook (3) hook check cable.

Claims (1)

  1. A kind of 1. aircraft arresting cable supporting structure, it is characterised in that：Supporting structure sets centre bore, centre bore hole wall and check cable Between have 0.5mm~1mm gaps, the side of supporting structure is scalene cone, the angle between the scalene cone of both sides 10 °~20 ° it Between.
CN201711220887.5A 2017-11-29 2017-11-29 Aircraft arresting cable bearing structure Active CN107985622B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711220887.5A CN107985622B (en) 2017-11-29 2017-11-29 Aircraft arresting cable bearing structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711220887.5A CN107985622B (en) 2017-11-29 2017-11-29 Aircraft arresting cable bearing structure

Publications (2)

Publication Number Publication Date
CN107985622A true CN107985622A (en) 2018-05-04
CN107985622B CN107985622B (en) 2024-02-27

Family

ID=62033895

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711220887.5A Active CN107985622B (en) 2017-11-29 2017-11-29 Aircraft arresting cable bearing structure

Country Status (1)

Country Link
CN (1) CN107985622B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110329529A (en) * 2019-07-22 2019-10-15 北京航天试验技术研究所 Tensioning apparatus and check cable for unmanned plane check cable are tensioned support component
CN112278313A (en) * 2020-11-05 2021-01-29 湖南浩天翼航空技术有限公司 Landing arresting rope mechanism of sliding unmanned aerial vehicle
CN112678196A (en) * 2021-01-19 2021-04-20 西安爱生技术集团公司 Cross-shaped supporting structure of unmanned aerial vehicle arresting cable, arresting system and method
CN112678197A (en) * 2021-01-19 2021-04-20 西安爱生技术集团公司 Herringbone supporting structure of unmanned aerial vehicle arresting cable, arresting system and method

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2526541A (en) * 1949-01-22 1950-10-17 Goodrich Co B F Inflatable cable-support apparatus for aircraft landing means
US3010683A (en) * 1959-10-12 1961-11-28 All American Eng Co Integral cable supports
US3086735A (en) * 1961-10-19 1963-04-23 John J Radovitz Chain arresting gear
US3158341A (en) * 1962-07-19 1964-11-24 All American Eng Co Support system for aircraft arresting cables
GB1223374A (en) * 1969-04-14 1971-02-24 All American Eng Co Aircraft arresting system
GB1389660A (en) * 1971-02-03 1975-04-03 Sherborne Rubber Co Arrester gear for aircraft
KR100398619B1 (en) * 2003-03-28 2003-09-19 Donghae Machinery & Aviat Co L System for supporting emergency landing of airplane
KR20050041997A (en) * 2004-12-28 2005-05-04 이기문 Runway overrun barrier
US6981673B1 (en) * 2004-11-05 2006-01-03 The United States Of America As Represented By The Secretary Of The Navy Wear resisting sleeve system for aircraft landing arresting cables
CN200967949Y (en) * 2006-10-19 2007-10-31 中国水电顾问集团华东勘测设计研究院 Large span waterborne safety protection facilities
CN104908968A (en) * 2015-06-23 2015-09-16 李竟儒 Device capable of preventing airplane from rushing out of runway in taking-off and landing process

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2526541A (en) * 1949-01-22 1950-10-17 Goodrich Co B F Inflatable cable-support apparatus for aircraft landing means
US3010683A (en) * 1959-10-12 1961-11-28 All American Eng Co Integral cable supports
US3086735A (en) * 1961-10-19 1963-04-23 John J Radovitz Chain arresting gear
US3158341A (en) * 1962-07-19 1964-11-24 All American Eng Co Support system for aircraft arresting cables
GB1223374A (en) * 1969-04-14 1971-02-24 All American Eng Co Aircraft arresting system
GB1389660A (en) * 1971-02-03 1975-04-03 Sherborne Rubber Co Arrester gear for aircraft
KR100398619B1 (en) * 2003-03-28 2003-09-19 Donghae Machinery & Aviat Co L System for supporting emergency landing of airplane
US6981673B1 (en) * 2004-11-05 2006-01-03 The United States Of America As Represented By The Secretary Of The Navy Wear resisting sleeve system for aircraft landing arresting cables
KR20050041997A (en) * 2004-12-28 2005-05-04 이기문 Runway overrun barrier
CN200967949Y (en) * 2006-10-19 2007-10-31 中国水电顾问集团华东勘测设计研究院 Large span waterborne safety protection facilities
CN104908968A (en) * 2015-06-23 2015-09-16 李竟儒 Device capable of preventing airplane from rushing out of runway in taking-off and landing process

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
薛骋豪;王田苗;张以成;梁建宏;: "小型固定翼无人机定点降落轨迹跟踪与控制", 机器人技术与应用, no. 03 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110329529A (en) * 2019-07-22 2019-10-15 北京航天试验技术研究所 Tensioning apparatus and check cable for unmanned plane check cable are tensioned support component
CN112278313A (en) * 2020-11-05 2021-01-29 湖南浩天翼航空技术有限公司 Landing arresting rope mechanism of sliding unmanned aerial vehicle
CN112678196A (en) * 2021-01-19 2021-04-20 西安爱生技术集团公司 Cross-shaped supporting structure of unmanned aerial vehicle arresting cable, arresting system and method
CN112678197A (en) * 2021-01-19 2021-04-20 西安爱生技术集团公司 Herringbone supporting structure of unmanned aerial vehicle arresting cable, arresting system and method

Also Published As

Publication number Publication date
CN107985622B (en) 2024-02-27

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