CN109319100A - A kind of ship-board aircraft buffer-type method for arresting and stop formation - Google Patents
A kind of ship-board aircraft buffer-type method for arresting and stop formation Download PDFInfo
- Publication number
- CN109319100A CN109319100A CN201811306847.7A CN201811306847A CN109319100A CN 109319100 A CN109319100 A CN 109319100A CN 201811306847 A CN201811306847 A CN 201811306847A CN 109319100 A CN109319100 A CN 109319100A
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- CN
- China
- Prior art keywords
- buffer
- bar
- ship
- stop formation
- block
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/68—Arrester hooks
Abstract
A kind of ship-board aircraft buffer-type method for arresting and stop formation, the stop formation, which contains, blocks bar, buffer blocks bar under, the upper end that bar is blocked on described is connect with airframe, on block the lower end of bar and buffer ontology upper end is connected as one, the buffer ontology is a rigid cavity, the buffer medium and a damper piston of air-fuel mixture are equipped in rigid chamber body, damper piston is equipped with buffer medium through hole, the piston rod of upper end and buffering piston that bar is blocked under described is hinged, the lower end that bar is blocked under described is equipped with and the matched hook of check cable;When aircraft landing, the check cable of bar lower end hooked on warship body deck is blocked under, the shock loading of check cable blocks bar under passing through and passes to buffer, and buffer is made to absorb shock loading, realizes that ship-board aircraft buffer-type blocks.
Description
Technical field
The application designs airplane structural design technology, specifically a kind of ship-board aircraft buffer-type method for arresting and blocks knot
Structure.
Background technique
During ship-board aircraft warship, the process success or not of blocking is directly related to the safety of aircraft, and arrester hook is
Wherein the most key component.Existing arrester hook is mainly made of upper hook rod, lower hook rod and gib head three parts, and the three parts are logical
Cross connection component connection.Upper hook rod is connected to airframe, and lower hook rod is connected to upper hook rod, and gib head is connected to lower hook rod, becomes
One complete arrester hook.For aircraft in warship, gib head hangs on warship vizard plate fixed check cable, then by lower hook rod and
Upper hook rod forms one powerful resistance to aircraft, to make to be down to zero in the aircraft taxi speed short time and shut down.Due to mesh
Upper hook rod, upper hook rod and the gib head of preceding arrester hook are all integral pieces, pass through between part and hingedly connect together, so that entirely blocking
Hook is hindered almost without retractility, and rigidity is especially big, in moment the active force on arrester hook can be transmitted to airframe, to rising to the bait
The Structural strength calls of bar and fuselage join domain are especially high, so that structural fatigue performance is bad at this, can even lead when serious
Cause structural failure, and then cause aircraft warship failure.It is to reduce arrester hook to the impact force of aircraft, mostly concerned patent is,
A kind of buffering off-load arrester hook hook arm 201310611967.9.
Summary of the invention
Present invention is designed to provide a kind of ship-board aircraft buffer-type method for arresting and stop formation.Pass through improvement
The structure type of arrester hook increases first-level buffer structure, by the active force pair on arrester hook between arrester hook and airframe
The influence of airframe mechanism minimizes.
A kind of ship-board aircraft buffer-type method for arresting containing the stop formation connecting with aircraft body and is located at warship body deck
On check cable, which is characterized in that the stop formation contain block bar, buffer and under block bar, it is described on block
The upper end of resistance bar is connect with airframe, and the lower end and buffer ontology upper end for above blocking bar are connected as one, described slow
Rushing device ontology is a rigid cavity, and the buffer medium and a damper piston of air-fuel mixture, buffering are equipped in rigid chamber body
Piston is equipped with buffer medium through hole, and the piston rod of upper end and buffering piston that bar is blocked under described is hinged, described
Under block bar lower end be equipped with and the matched hook of check cable;When aircraft landing, the hook that bar lower end is blocked under hooks warship
Check cable on body deck, the shock loading of check cable block bar under passing through and pass to buffer, so that buffer is absorbed impact and carry
Lotus realizes that ship-board aircraft buffer-type blocks.
Buffer ontology upper end is equipped with sealing cover, and sealing cover is equipped with buffer medium inlet, which is situated between
Matter inlet is the structure of an included sealing.
The beneficial effects of the present application are as follows: 1) by blocked by bar and under block buffer between bar so that blocking
Movement have pooling feature, ship-board aircraft can be allowed softer in warship, at the same reduce to airframe with above block
The impact of the join domain structure of bar, so that its longer life expectancy.2) by adjust buffer damping, can to different aircrafts into
Row targeted design.3) present invention is air-fuel mixture medium in the buffer medium of buffer, and advantage has: buffer is high-efficient,
More impact energys can be absorbed;Operation and Maintenance is simple, each aircraft after warship blocks, operated without personnel, buffering piston
The effect that can use oil-air pressure difference returns to initial position, it is automatic for next time warship block and be ready.
Attached drawing is described in further detail the application with reference to embodiments.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of ship-board aircraft buffer-type stop formation.
Fig. 2 is the schematic diagram of the section structure of ship-board aircraft buffer-type stop formation.
Explanation is numbered in figure: being blocked on 1 and is blocked bar, 6 hooks, 7 companies under bar, 2 buffers, 3 piston rods, 4 connection components, 5
Spindle, 8 buffer medium inlets, 9 sealing covers, 10 damper pistons, 11 through holes, 12 rigid cavitys, 13 seal assemblies
Specific embodiment
Referring to the ship-board aircraft buffer-type method for arresting that attached drawing, the application propose, blocked containing what is connect with aircraft body
Structure and the check cable being located on warship body deck, the stop formation contain block bar 1, buffer 2 and under block bar 5,
The upper end that bar 1 is blocked on described is connect with airframe, and the lower end and 2 ontology upper end of buffer for above blocking bar 1 are connected as one
Body structure, 2 ontology of buffer are a rigid cavitys 12, buffer medium in rigid cavity 12 equipped with air-fuel mixture and
One damper piston 10, damper piston 10 are equipped with buffer medium through hole 11, upper end and the buffer of bar 5 are blocked under described
The piston rod 3 of damper piston is hinged by connection component 4, passes through seal assembly between piston rod 3 and the rigid cavity of buffer
13 are tightly connected, and the lower end that bar 5 is blocked under described, which is equipped with, passes through connector 7 under with the matched hook 6 of check cable, hook 6
The lower end for blocking bar 5 is fixed;When aircraft landing, the hook 6 that 5 lower end of bar is blocked under hooks check cable on warship body deck,
The shock loading of check cable blocks bar 5 and passes to buffer 2 under passing through, buffer is made to absorb shock loading, realizes ship-board aircraft
Buffer-type blocks.
Under when blocking bar 5 and being impacted, impact force blocks bar 5 and pushes 10 compression buffer rigidity cavity of damper piston under making
The buffer medium of oil-gas mixture in 12 above damper piston, oil-gas mixture composition absorbs shock loading, effectively reduces
Damage of the shock loading to airframe;After power is blocked in releasing, damper piston 10 is pushed by the high-pressure oil gas mixed liquor of top, band
Bar 5 is blocked under dynamic to automatically reset.In design, by adjusting the size of through hole 11 on damper piston 10, buffer damping is realized
Adjusting, can to different aircrafts carry out targeted design.
In implementation, buffer ontology upper end is equipped with sealing cover 9, and sealing cover is equipped with buffer medium inlet
12, which is the structure of an included sealing.
Claims (4)
1. a kind of ship-board aircraft buffer-type method for arresting containing the stop formation connecting with aircraft body and is located on warship body deck
Check cable, which is characterized in that the stop formation contain block bar, buffer and under block bar, it is described on block
The upper end of bar is connect with airframe, and the lower end and buffer ontology upper end for above blocking bar are connected as one, the buffering
Device ontology is a rigid cavity, and the buffer medium and a damper piston of air-fuel mixture are equipped in rigid chamber body, and buffering is lived
It is equipped with buffer medium through hole beyond the Great Wall, the piston rod of upper end and buffering piston that bar is blocked under described is hinged, under described
The lower end for blocking bar is equipped with and the matched hook of check cable;When aircraft landing, the hook that bar lower end is blocked under hooks warship body
Check cable on deck, the shock loading of check cable block bar under passing through and pass to buffer, and buffer is made to absorb shock loading,
Realize that ship-board aircraft buffer-type blocks.
2. ship-board aircraft buffer-type method for arresting as described in claim 1, which is characterized in that buffer ontology upper end is set
There is sealing cover, sealing cover is equipped with buffer medium inlet, which is the structure of an included sealing.
3. a kind of ship-board aircraft buffer-type stop formation, which is characterized in that the stop formation, which contains, blocks bar, buffer
Block bar under, it is described on block the upper end of bar and connect with airframe, above block the lower end and buffer ontology upper end of bar
It is connected as one, the buffer ontology is a rigid cavity, and the buffering in rigid chamber body equipped with air-fuel mixture is situated between
Matter and a damper piston, damper piston are equipped with buffer medium through hole, and upper end and the buffer that bar is blocked under described are living
The piston rod of plug is hinged, and the lower end that bar is blocked under described is equipped with and the matched hook of check cable.
4. ship-board aircraft buffer-type stop formation as claimed in claim 3, which is characterized in that buffer ontology upper end is set
There is sealing cover, sealing cover is equipped with buffer medium inlet, which is the structure of an included sealing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201811306847.7A CN109319100A (en) | 2018-11-02 | 2018-11-02 | A kind of ship-board aircraft buffer-type method for arresting and stop formation |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201811306847.7A CN109319100A (en) | 2018-11-02 | 2018-11-02 | A kind of ship-board aircraft buffer-type method for arresting and stop formation |
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CN109319100A true CN109319100A (en) | 2019-02-12 |
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CN201811306847.7A Pending CN109319100A (en) | 2018-11-02 | 2018-11-02 | A kind of ship-board aircraft buffer-type method for arresting and stop formation |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113335508A (en) * | 2021-05-28 | 2021-09-03 | 中国航空工业集团公司沈阳飞机设计研究所 | Unmanned aerial vehicle landing retraction jack |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1232598A (en) * | 1967-11-13 | 1971-05-19 | ||
CN103204245A (en) * | 2013-04-11 | 2013-07-17 | 西南交通大学 | Auxiliary landing device for shipboard aircraft of aircraft carrier |
CN103640694A (en) * | 2013-11-28 | 2014-03-19 | 江西洪都航空工业集团有限责任公司 | Hook arm of buffer load-shedding arresting hook |
KR20140115711A (en) * | 2013-03-22 | 2014-10-01 | 김명호 | Aerial Vehicle With Mltipurpose Grip Type Taking Off an Landing Devic |
CN104176246A (en) * | 2014-09-17 | 2014-12-03 | 江西洪都航空工业集团有限责任公司 | Arresting hook retracting and releasing mechanism |
CN104963980A (en) * | 2014-03-19 | 2015-10-07 | 梅西耶道蒂有限公司 | Shock absorber and a method of determining the level of liquid in a shock absorber |
-
2018
- 2018-11-02 CN CN201811306847.7A patent/CN109319100A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1232598A (en) * | 1967-11-13 | 1971-05-19 | ||
KR20140115711A (en) * | 2013-03-22 | 2014-10-01 | 김명호 | Aerial Vehicle With Mltipurpose Grip Type Taking Off an Landing Devic |
CN103204245A (en) * | 2013-04-11 | 2013-07-17 | 西南交通大学 | Auxiliary landing device for shipboard aircraft of aircraft carrier |
CN103640694A (en) * | 2013-11-28 | 2014-03-19 | 江西洪都航空工业集团有限责任公司 | Hook arm of buffer load-shedding arresting hook |
CN104963980A (en) * | 2014-03-19 | 2015-10-07 | 梅西耶道蒂有限公司 | Shock absorber and a method of determining the level of liquid in a shock absorber |
CN104176246A (en) * | 2014-09-17 | 2014-12-03 | 江西洪都航空工业集团有限责任公司 | Arresting hook retracting and releasing mechanism |
Non-Patent Citations (1)
Title |
---|
《飞机设计手册》总编委会: "起飞着陆系统设计", 《飞机设计手册 第14册:起飞着陆系统设计》 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113335508A (en) * | 2021-05-28 | 2021-09-03 | 中国航空工业集团公司沈阳飞机设计研究所 | Unmanned aerial vehicle landing retraction jack |
CN113335508B (en) * | 2021-05-28 | 2023-06-02 | 中国航空工业集团公司沈阳飞机设计研究所 | Landing retraction mechanism of small unmanned aerial vehicle |
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Application publication date: 20190212 |