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CN112196932A - Throttle valve for buffer - Google Patents

Throttle valve for buffer
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Publication number
CN112196932A
CN112196932ACN202011028759.2ACN202011028759ACN112196932ACN 112196932 ACN112196932 ACN 112196932ACN 202011028759 ACN202011028759 ACN 202011028759ACN 112196932 ACN112196932 ACN 112196932A
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China
Prior art keywords
valve
valve seat
side wall
circle
annular
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Application number
CN202011028759.2A
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Chinese (zh)
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CN112196932B (en
Inventor
汪兰明
杜进
焦阳
张松
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China Helicopter Research and Development Institute
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China Helicopter Research and Development Institute
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Priority to CN202011028759.2ApriorityCriticalpatent/CN112196932B/en
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Abstract

The invention belongs to the technical field of structural design of helicopters, and discloses a throttle valve for a buffer, which comprises: valve pin, valve seat, valve barrel, big spring, valve cover, little spring, outer retaining ring and interior retaining ring. The valve seat is of an H-shaped tubular structure, a group of oil holes are distributed in an annular mode at the position, close to the side wall, of the middle partition plate, a small hole is formed in the center of the middle partition plate, and a circle of annular holes are formed in the side wall of the upper cavity of the valve seat; a group of valve pins are arranged in the holes at the upper part of the valve seat; the valve sleeve is provided with an annular groove on the middle side wall of the inner circle, 1 group of oil holes are arranged in the middle of the groove, the inner circle of the valve sleeve is assembled on the excircle of the middle upper part of the valve seat, the large spring is assembled on the excircle of the lower part of the valve seat, the upper part of the large spring is attached to the lower end face of the valve sleeve, the outer retaining ring is assembled on the lower part of the valve seat, the upper end face of the outer retaining ring is in contact with the lower end face of the large spring, the large spring is compressed, the valve cover is inversely assembled in the lower cavity of the. The throttle valve is suitable for buffers with different landing speed requirements.

Description

Throttle valve for buffer
Technical Field
The invention belongs to the technical field of structural design of helicopters, and particularly relates to a throttle valve for a buffer.
Background
A throttling valve for a buffer is used for an undercarriage buffer, and the requirement that the buffer is suitable for different landing speeds can be met by adjusting the size of a damping hole according to the oil pressure in the buffer.
The defects of the background art are as follows:
the existing throttle valve for the buffer usually adopts a fixed oil hole or an oil needle structure, is usually suitable for the design of the buffer with constant landing speed, has larger landing speed span (more than 0.5 m/s-12.8 m/s) for helicopters, particularly crash-resistant undercarriages, adopts the multi-stage buffers in series to meet the requirements of normal landing and crash resistance, and has more complex structure and higher weight cost.
Disclosure of Invention
The purpose of the invention is as follows: a throttle valve for a buffer is provided which is adaptable to different landing speed requirements.
The technical scheme of the invention is as follows:
a throttle valve for a damper, comprising: the valve comprises a valve pin, a valve seat, a valve sleeve, a large spring, a valve cover, a small spring, an outer retainer ring and an inner retainer ring;
the valve seat is of an H-shaped tubular structure and is divided into an upper cavity and a lower cavity by a central partition plate; a circle of annular first oil holes are axially formed in the periphery of the central partition plate close to the side wall;
the upper end of the valve seat is connected with the upper end of a buffer piston rod;
the outer side wall of the upper end of the valve seat is provided with a ring-shaped boss; the annular boss is provided with a group of first through holes along the axial direction;
the valve pins are of T-shaped cylindrical structures, and a group of valve pins are arranged in the first through hole from top to bottom;
the valve sleeve is of a tubular structure and is sleeved on the outer side wall of the upper cavity of the valve seat;
the outer retainer ring is of a tubular structure and is sleeved at the bottom of the valve seat;
the large spring is sleeved on the outer side wall of the valve seat and between the valve sleeve and the outer retainer ring;
the valve cover is of a U-shaped annular structure and is inversely assembled in the lower cavity of the valve seat;
the small retainer ring is of a tubular structure and is arranged at the bottom end inside the lower cavity of the valve seat,
the small spring is arranged between the small retainer ring and the bottom of the valve cover.
Furthermore, a circle of second oil holes are formed in the side wall of the upper cavity of the valve seat along the radial direction.
Furthermore, a circle of annular groove is formed in the inner side wall of the valve sleeve; and a circle of third oil holes matched with the second oil holes are radially arranged in the annular groove. The valve sleeve is mainly used for increasing the area of the damping hole and reducing the damping force after the valve sleeve moves downwards under the action of oil pressure through the valve pin and the compression spring moves downwards.
Further, a second through hole is formed in the center of the central partition plate of the valve seat, and the area of the second through hole is not more than 30% of the total area of the circle of the first oil holes. The buffer has the main effects that the buffer is used as a rebound fixed oil hole, provides larger damping for the rebound of the buffer, and prevents the buffer from having the phenomenon of higher rebound speed.
Furthermore, a third through hole is formed in the center of the bottom of the valve cover, and the diameter of the third through hole is smaller than the difference value between the diameter of a circle formed by the circle centers of the circle of the annular first oil holes and the diameter of the first oil holes.
Further, the diameter of the third through hole is larger than that of the second through hole. When guaranteeing that third oilhole and second oilhole coincide, fluid can pass through the second oilhole completely.
Further, an annular flange edge is arranged on the outer side wall of the upper end of the valve sleeve; the upper end face of the annular flange is in contact with the lower end face of the annular boss of the valve seat, and the upper end face of the annular flange is also in contact with the bottom end face of the valve pin.
Furthermore, the side wall of the lower end of the valve seat is provided with a pin along the radial direction for fixing the outer retainer ring and the inner retainer ring.
The invention has the beneficial effects that:
the invention has simple and compact structure, can meet the damping requirements of the buffer at different landing speeds, can improve the buffering performance of the buffer and reduce the structural complexity of the buffer.
Drawings
FIG. 1 is a schematic view of a throttle valve for a damper;
FIG. 2 is a schematic diagram of a positive stroke, low speed operation of the throttle valve;
FIG. 3 is a schematic diagram of the positive stroke high speed operation of the throttle valve;
FIG. 4 is a schematic diagram of reverse throttle operation;
description of numbering: 1 valve pin, 2 valve seats, 3 valve sleeves, 4 large springs, 5 valve covers, 6 small springs, 7 outer check rings and 8 inner check rings.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Fig. 1 is a schematic structural composition diagram of the invention, and the throttle valve comprises avalve pin 1, avalve seat 2, avalve sleeve 3, alarge spring 4, avalve cover 5, asmall spring 6, anouter retainer 7, aninner retainer 8 and the like. Thevalve seat 2 is in an H-shaped tubular structure, a group of oil holes are distributed in an annular mode at the position, close to the side wall, of the middle partition plate, a small hole is formed in the center of the middle partition plate, and a circle of annular holes are formed in the side wall of the upper cavity of the valve seat; thevalve seat 2 is connected with the upper end of a piston rod of the buffer to divide the buffer into two oil cavities; the tail of thevalve pin 1 is of a T-shaped cylindrical structure, and a group ofvalve pins 1 are arranged in holes in the upper part of thevalve seat 2; thevalve bush 3 is of a T-shaped tubular structure, the side wall of the middle of an inner circle is provided with an annular groove, the middle of the groove is provided with 1 group of oil holes, the inner circle of thevalve bush 3 is assembled on the excircle of the middle upper part of thevalve seat 2, and the upper part of thevalve bush 3 is respectively contacted with the upper and lower end surfaces of the valve seat and the end surface of thevalve pin 1;big spring 4 assembles on the lower part excircle ofdisk seat 2, and the terminal surface laminating under 3 upper portions of big spring and thevalve barrel 3, outer retainer ring assembly in the lower part of disk seat, the terminal surface contact under up end and thebig spring 3, compressesbig spring 4, andvalve cover 5 is "U" type annular structure, and the hole is dug at the center, and the assembly is invertedly atdisk seat 2 lower part intracavity, andlittle spring 6 assembles inside in the valve gap, and the lower extreme passes throughlittle retainer ring 6 to be fixed in the cavity of 2 lower parts of disk seat.
FIG. 2 is the normal stroke small speed working principle of the present invention, the oil pressure in the oil chamber can only overcome the acting force of thesmall spring 6 to open thevalve cover 5, at this time, the oil hole in the center of thevalve seat 2 is completely opened, and the oil enters the oil return chamber through the damping hole to generate the damping force; FIG. 3 is a positive stroke high speed working principle of the present invention, the oil pressure in the oil chamber can overcome the acting force of thesmall spring 6 to open thevalve cover 5, meanwhile, the oil pressure acts on thevalve sleeve 3 through thevalve pin 1, the oil hole in the middle of the side wall of thevalve sleeve 3 and the damping hole in the side wall of thevalve seat 2 are combined with each other by overcoming the acting force of thelarge spring 4, and the oil in the oil chamber enters the oil return chamber through the central damping hole and the side wall damping of thevalve seat 2 to generate; FIG. 4 shows the reverse stroke working principle of the present invention, the upper part of thevalve sleeve 3 is attached to the end surface of thevalve seat 2 under the pressure of the oil return chamber and the acting force of thelarge spring 4, the oil hole on the side wall of thevalve seat 2 is closed, the upper part of thevalve cover 5 is attached to the middle end surface of thevalve seat 2 under the pressure of the oil return chamber and the acting force of thelarge spring 4, the oil hole at the center of thevalve seat 2 close to the side wall, the center oil hole of thevalve cover 5 coincides with the center small oil hole of thevalve seat 2, and at this time.
The foregoing is merely a detailed description of the embodiments of the present invention, and some of the conventional techniques are not detailed. The scope of the present invention is not limited thereto, and any changes or substitutions that can be easily made by those skilled in the art within the technical scope of the present invention will be covered by the scope of the present invention. The protection scope of the present invention shall be subject to the protection scope of the claims.

Claims (8)

CN202011028759.2A2020-09-252020-09-25Throttle valve for bufferActiveCN112196932B (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
CN202011028759.2ACN112196932B (en)2020-09-252020-09-25Throttle valve for buffer

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
CN202011028759.2ACN112196932B (en)2020-09-252020-09-25Throttle valve for buffer

Publications (2)

Publication NumberPublication Date
CN112196932Atrue CN112196932A (en)2021-01-08
CN112196932B CN112196932B (en)2022-04-22

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CN202011028759.2AActiveCN112196932B (en)2020-09-252020-09-25Throttle valve for buffer

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Citations (16)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
GB1563273A (en)*1976-02-041980-03-26Messier Hispano SaShock absorber
DE4406918A1 (en)*1993-03-181994-09-22Fichtel & Sachs Ag Damping valve device
US5409088A (en)*1991-04-121995-04-25Yamaha Hatsudoki Kabushiki KaishaShock absorber
JP2000225823A (en)*1999-02-042000-08-15Kayaba Ind Co Ltd Payload-sensitive hydraulic shock absorber
CN1601138A (en)*2003-09-272005-03-30吕崇耀Method for changing hydraulic overflow in large flux into buffered throttle
CN101016926A (en)*2007-02-062007-08-15南京航空航天大学Undercarriage bumper having inner flow regulating valve
FR2902850A1 (en)*2006-06-212007-12-28Soben Soc Par Actions SimplifiHydraulic end-stop device for adjustable shock absorber of e.g. helicopter, has outer tube integrated with actuator arranged outside body, and including openings mapped with openings of inner tube so that fluid rapidly flows via openings
CN102138024A (en)*2008-09-012011-07-27Zf腓特烈港股份公司 adjustable damping valve
CN102562915A (en)*2010-12-302012-07-11杨洁Self-adaptive damping adjustment diverter valve of self-adaptive variable damper shock absorber
JP2012140981A (en)*2010-12-282012-07-26Hitachi Automotive Systems LtdDamping force adjusting-type shock absorber
KR101398755B1 (en)*2013-05-162014-05-27주식회사 만도Variable hydraulic stopping damper
CN203670326U (en)*2013-12-182014-06-25常德中联重科液压有限公司Overflow valve of oily function is mended in area
CN105626764A (en)*2014-10-272016-06-01蒋磊Method for buffering undercarriage by mixing rubber and spring
CN105782324A (en)*2016-04-282016-07-20广州汽车集团股份有限公司Solenoid valve assembly externally arranged on absorber and absorber
CN107143604A (en)*2017-06-292017-09-08黄永宁Damper from main inlet control valve and its staged method of discharge
CN110701234A (en)*2019-10-222020-01-17中国北方车辆研究所Shock acceleration sensitive valve for shock absorber

Patent Citations (16)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
GB1563273A (en)*1976-02-041980-03-26Messier Hispano SaShock absorber
US5409088A (en)*1991-04-121995-04-25Yamaha Hatsudoki Kabushiki KaishaShock absorber
DE4406918A1 (en)*1993-03-181994-09-22Fichtel & Sachs Ag Damping valve device
JP2000225823A (en)*1999-02-042000-08-15Kayaba Ind Co Ltd Payload-sensitive hydraulic shock absorber
CN1601138A (en)*2003-09-272005-03-30吕崇耀Method for changing hydraulic overflow in large flux into buffered throttle
FR2902850A1 (en)*2006-06-212007-12-28Soben Soc Par Actions SimplifiHydraulic end-stop device for adjustable shock absorber of e.g. helicopter, has outer tube integrated with actuator arranged outside body, and including openings mapped with openings of inner tube so that fluid rapidly flows via openings
CN101016926A (en)*2007-02-062007-08-15南京航空航天大学Undercarriage bumper having inner flow regulating valve
CN102138024A (en)*2008-09-012011-07-27Zf腓特烈港股份公司 adjustable damping valve
JP2012140981A (en)*2010-12-282012-07-26Hitachi Automotive Systems LtdDamping force adjusting-type shock absorber
CN102562915A (en)*2010-12-302012-07-11杨洁Self-adaptive damping adjustment diverter valve of self-adaptive variable damper shock absorber
KR101398755B1 (en)*2013-05-162014-05-27주식회사 만도Variable hydraulic stopping damper
CN203670326U (en)*2013-12-182014-06-25常德中联重科液压有限公司Overflow valve of oily function is mended in area
CN105626764A (en)*2014-10-272016-06-01蒋磊Method for buffering undercarriage by mixing rubber and spring
CN105782324A (en)*2016-04-282016-07-20广州汽车集团股份有限公司Solenoid valve assembly externally arranged on absorber and absorber
CN107143604A (en)*2017-06-292017-09-08黄永宁Damper from main inlet control valve and its staged method of discharge
CN110701234A (en)*2019-10-222020-01-17中国北方车辆研究所Shock acceleration sensitive valve for shock absorber

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
刘向尧等: "国内中小型无人机起落缓冲装置的研究现状与展望", 《贵州农机化》*

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