CN106194496A - A kind of governor valve - Google Patents
A kind of governor valve Download PDFInfo
- Publication number
- CN106194496A CN106194496A CN201610632587.7A CN201610632587A CN106194496A CN 106194496 A CN106194496 A CN 106194496A CN 201610632587 A CN201610632587 A CN 201610632587A CN 106194496 A CN106194496 A CN 106194496A
- Authority
- CN
- China
- Prior art keywords
- valve
- base plate
- ear mount
- ear
- open slot
- 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.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/11—Varying effective area of jet pipe or nozzle by means of pivoted eyelids
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Valve Housings (AREA)
Abstract
The invention discloses a kind of governor valve, belong to aero-engine spray bar technology field.The present invention includes: base plate and valve, open slot it is provided with on base plate, base plate one end is provided with connection ear mount, open slot is provided with two fixed ear bases near the one end connecting ear mount, valve includes installing ear mount and valve base plate, installs ear mount and is arranged on one end of valve base plate, installs ear mount and is flexibly connected with fixed ear base, the valve base plate other end is unsettled, and base plate is installed fixing by connecting ear mount;Present configuration is simple, be easily maintained, by governor valve position, pneumatic location, the jet pipe excessive expansion issues under the big Mach number of supersonic speed during transonic speed flight can be effectively improved, improve nozzle thrust characteristic, when nozzle gas flow instability, the vibration of valve also can be alleviated.
Description
Technical field
The invention belongs to aero-engine spray bar technology field, be specifically related to a kind of governor valve.
Background technology
At present, most electromotors are under the off design point big Mach number of particularly supersonic speed during transonic speed flight, and jet pipe goes out
There is the problem excessively expanded in mouth, causes motor power loss bigger.And on jet pipe governor valve, increase pneumatic valve, can
To improve the jet pipe excessive expansion issues under the big Mach number of supersonic speed during transonic speed flight, improve nozzle thrust characteristic, work as spray
During pipe air-flow instability, it is also possible to alleviate the vibration of governor valve, to meet the use demand of fighter plane.
Summary of the invention
The purpose of the present invention: in order to solve the problems referred to above, the present invention proposes a kind of governor valve, have employed pneumatic location
The position of governor valve, alleviates the vibration of governor valve, and improves jet pipe excessive expansion problem.
The technical scheme is that a kind of governor valve, including: base plate and valve, base plate is provided with open slot, the end
Plate one end is provided with connection ear mount, and open slot is provided with two fixed ear bases near the one end connecting ear mount, and valve includes installing
Ear mount and valve base plate, install ear mount and be arranged on one end of valve base plate, installs ear mount and is flexibly connected with fixed ear base, at the bottom of valve
The plate other end is unsettled, and base plate is installed fixing by connecting ear mount.
Preferably, the contour shape of described valve base plate is identical with the opening shape of described open slot and valve base plate can
Open slot is made to seal.
Preferably, described installation ear mount is bolted with described fixed ear base.
Preferably, described installation ear mount is connected by ball pin with described fixed ear base.
Preferably, described valve base plate arranges circulating type reinforcement, and the cross that is internally connected with of circulating type reinforcement adds
Strong muscle, and described circulating type reinforcement, described criss-crossing reinforcing ribs and valve base plate link into an integrated entity.
The technology beneficial effect of the present invention: simple in construction, be easily maintained, by governor valve position, pneumatic location, can have
Effect improves the jet pipe excessive expansion issues under the big Mach number of supersonic speed during transonic speed flight, improves nozzle thrust characteristic, works as spray
During pipe air-flow instability, also can alleviate the vibration of valve.
Accompanying drawing explanation
Fig. 1 is the structural representation of a preferred embodiment of a kind of governor valve of the present invention;
Fig. 2 is the base arrangement schematic diagram of embodiment illustrated in fig. 1;
Fig. 3 is the valve structure schematic diagram of embodiment illustrated in fig. 1;
Fig. 4 is that valve closes schematic diagram;
Fig. 5 is that valve opens schematic diagram;
Wherein, 1-base plate, 2-valve, 3-open slot, 4-fixed ear base, 5-connects ear mount, and 6-installs ear mount, at the bottom of 7-valve
Plate, 8-circulating type reinforcement, 9-criss-crossing reinforcing ribs.
Detailed description of the invention
Clearer for the purpose making the present invention implement, technical scheme and advantage, below in conjunction with in the embodiment of the present invention
Accompanying drawing, the technical scheme in the embodiment of the present invention is further described in more detail.In the accompanying drawings, the most identical or class
As label represent same or similar element or there is the element of same or like function.Described embodiment is the present invention
A part of embodiment rather than whole embodiments.The embodiment described below with reference to accompanying drawing is exemplary, it is intended to use
In explaining the present invention, and it is not considered as limiting the invention.Based on the embodiment in the present invention, ordinary skill people
The every other embodiment that member is obtained under not making creative work premise, broadly falls into the scope of protection of the invention.Under
Face combines accompanying drawing and is described in detail embodiments of the invention.
In describing the invention, it is to be understood that term " " center ", " longitudinally ", " laterally ", "front", "rear",
The orientation of the instruction such as "left", "right", " vertically ", " level ", " top ", " end " " interior ", " outward " or position relationship are for based on accompanying drawing institute
The orientation shown or position relationship, be for only for ease of and describe the present invention and simplify description rather than instruction or the dress of hint indication
Put or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that protect the present invention
The restriction of scope.
Below in conjunction with the accompanying drawings embodiments of the invention are described in detail, refer to Fig. 1 to Fig. 5;
A kind of governor valve, including: base plate 1 and valve 2, base plate 1 is provided with open slot 3, the shape of open slot 3 is permissible
Being that triangle, rectangle, trapezoidal, circular, oval and swallow-tail form, and quantity are 1 to 10, aperture position can select as required
Select.
Base plate 1 one end is provided with connection ear mount 5, and base plate 1 fixedly mounts with miscellaneous part by connecting ear mount 5.
Open slot 3 is provided with two symmetrical fixed ear bases 4 near the one end connecting ear mount 5, and valve 2 is by installing ear mount 6
Form with valve base plate 7, ear mount 6 is installed and is arranged on one end of valve base plate 7, ear mount 6 cooperation is installed and is arranged on two fixing ears
Between seat 4, it is achieved ear mount 6 is installed and fixed ear base 4 is flexibly connected;Ear mount 6 is installed and fixed ear base 4 selects by bolt even
Connect, it is possible to connected by ball pin;Valve 2 can be made to rotate around the installing hole axis of fixed mounting 4, opening of governor valve 7
Degree size.
The other end of valve base plate 7 is unsettled, and the contour shape of valve base plate 7 is identical with the opening shape of described open slot 3
And valve base plate 7 contour dimension is more than the opening size of open slot 3, both cooperate, and make valve base plate 7 fit completely base plate
When 1, open slot 3 can be sealed.
Valve base plate 7 edge retainer ring geometric pattern reinforcement 8, arranges criss-crossing reinforcing ribs 9 in circulating type reinforcement 8, and
Described circulating type reinforcement 8 and described criss-crossing reinforcing ribs 9 are integrally welded, are jointly fixed on valve base plate 7, strengthen valve
The structural strength of base plate 7.
When core flow pressure is higher than outer flowing pressure, valve base plate 7 is close to base plate 1 under inside and outside differential pressure effect, and valve 2 closes
Close.
When core flow pressure is less than outer flowing pressure, valve base plate 7 is inwardly opened under inside and outside differential pressure effect, flowing gas
Enter core flow, improve the excessive expansion of core flow.The opening degree of valve 2 moves along with the change of inside and outside differential pressure, widens
Range of accommodation.
One governor valve simple in construction of the present invention, it is easily maintained, by governor valve position, pneumatic location, can effectively change
It is apt to the jet pipe excessive expansion issues under the big Mach number of supersonic speed during transonic speed flight, improves nozzle thrust characteristic, when jet pipe gas
When stream is unstable, also can alleviate the vibration of valve.
Last it is noted that above example is only in order to illustrate technical scheme, it is not intended to limit.To the greatest extent
The present invention has been described in detail by pipe with reference to previous embodiment, it will be understood by those within the art that: it is still
Technical scheme described in foregoing embodiments can be modified, or wherein portion of techniques feature is carried out equivalent replace
Change;And these amendments or replacement, do not make the essence of appropriate technical solution depart from the essence of various embodiments of the present invention technical scheme
God and scope.
Claims (5)
1. a governor valve, it is characterised in that including: base plate (1) and valve (2), base plate (1) is provided with open slot (3),
Base plate (1) one end is provided with connection ear mount (5), and open slot (3) is provided with two fixed ear bases near the one end connecting ear mount (5)
(4), valve (2) includes installing ear mount (6) and valve base plate (7), installs ear mount (6) and is arranged on one end of valve base plate (7), peace
Dress ear mount (6) is flexibly connected with fixed ear base (4), and valve base plate (7) other end is unsettled, and base plate (1) is pacified by connecting ear mount (5)
Dress is fixing.
A kind of governor valve the most according to claim 1, it is characterised in that: the contour shape of described valve base plate (7) with
The opening shape of described open slot (3) is identical and valve base plate (7) can make open slot (3) seal.
A kind of governor valve the most according to claim 1, it is characterised in that: described installation ear mount (6) and described fixing ear
Seat (4) is bolted.
A kind of governor valve the most according to claim 1, it is characterised in that: described installation ear mount (6) and described fixing ear
Seat (4) is connected by ball pin.
A kind of governor valve the most according to claim 1, it is characterised in that: described valve base plate (7) arranges circulating type and adds
Strong muscle (8), circulating type reinforcement (8) be internally connected with criss-crossing reinforcing ribs (9), and described circulating type reinforcement (8), described
Criss-crossing reinforcing ribs (9) and valve base plate (7) link into an integrated entity.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610632587.7A CN106194496A (en) | 2016-08-04 | 2016-08-04 | A kind of governor valve |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610632587.7A CN106194496A (en) | 2016-08-04 | 2016-08-04 | A kind of governor valve |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106194496A true CN106194496A (en) | 2016-12-07 |
Family
ID=57497656
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610632587.7A Pending CN106194496A (en) | 2016-08-04 | 2016-08-04 | A kind of governor valve |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106194496A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107882654A (en) * | 2017-11-10 | 2018-04-06 | 中国航发沈阳发动机研究所 | The dual vector jet pipe of expansion segment pressure self-balancing and there is its aero-engine |
CN107882653A (en) * | 2017-11-10 | 2018-04-06 | 中国航发沈阳发动机研究所 | Expansion segment pressure self-balancing axisymmetric vectoring exhaust nozzle and there is its aero-engine |
CN108104975A (en) * | 2017-12-14 | 2018-06-01 | 中国航发沈阳发动机研究所 | A kind of axisymmetric nozzle air-flow adjusting mechanism and with its axisymmetric nozzle |
CN109339955A (en) * | 2018-12-16 | 2019-02-15 | 中国航发沈阳发动机研究所 | A kind of support construction of air bleed valve regulating mechanism |
CN114263533A (en) * | 2021-12-20 | 2022-04-01 | 中国人民解放军国防科技大学 | Shock wave/boundary layer interference control device based on secondary flow circulation array and self-adaptive control method |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5666802A (en) * | 1993-02-08 | 1997-09-16 | Lair; Jean-Pierre | Turbine engine equipped with thrust reverser |
CN201028064Y (en) * | 2006-12-29 | 2008-02-27 | 陕西燎原航空机械制造公司 | Limited air check valve |
CN103867337A (en) * | 2012-12-11 | 2014-06-18 | 中航商用航空发动机有限责任公司 | Variable cycle engine with high bypass ratio |
CN103967617A (en) * | 2013-01-24 | 2014-08-06 | 李吉光 | Turboprop engine |
CN105715385A (en) * | 2014-12-05 | 2016-06-29 | 雄和崴有限公司 | Adjustment and control method and device for negative pressure air intake of air inlet system |
-
2016
- 2016-08-04 CN CN201610632587.7A patent/CN106194496A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5666802A (en) * | 1993-02-08 | 1997-09-16 | Lair; Jean-Pierre | Turbine engine equipped with thrust reverser |
CN201028064Y (en) * | 2006-12-29 | 2008-02-27 | 陕西燎原航空机械制造公司 | Limited air check valve |
CN103867337A (en) * | 2012-12-11 | 2014-06-18 | 中航商用航空发动机有限责任公司 | Variable cycle engine with high bypass ratio |
CN103967617A (en) * | 2013-01-24 | 2014-08-06 | 李吉光 | Turboprop engine |
CN105715385A (en) * | 2014-12-05 | 2016-06-29 | 雄和崴有限公司 | Adjustment and control method and device for negative pressure air intake of air inlet system |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107882654A (en) * | 2017-11-10 | 2018-04-06 | 中国航发沈阳发动机研究所 | The dual vector jet pipe of expansion segment pressure self-balancing and there is its aero-engine |
CN107882653A (en) * | 2017-11-10 | 2018-04-06 | 中国航发沈阳发动机研究所 | Expansion segment pressure self-balancing axisymmetric vectoring exhaust nozzle and there is its aero-engine |
CN108104975A (en) * | 2017-12-14 | 2018-06-01 | 中国航发沈阳发动机研究所 | A kind of axisymmetric nozzle air-flow adjusting mechanism and with its axisymmetric nozzle |
CN109339955A (en) * | 2018-12-16 | 2019-02-15 | 中国航发沈阳发动机研究所 | A kind of support construction of air bleed valve regulating mechanism |
CN109339955B (en) * | 2018-12-16 | 2021-09-03 | 中国航发沈阳发动机研究所 | Supporting structure of deflation valve adjusting mechanism |
CN114263533A (en) * | 2021-12-20 | 2022-04-01 | 中国人民解放军国防科技大学 | Shock wave/boundary layer interference control device based on secondary flow circulation array and self-adaptive control method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106194496A (en) | A kind of governor valve | |
JP5087545B2 (en) | Aircraft turbojet engine, aircraft equipped with such a turbojet engine, and method of attaching such a turbojet engine to an aircraft | |
CN103867235B (en) | A kind of tubular type subtracts whirlpool device bleed air system | |
US9327780B1 (en) | Aerodynamic bumper center deflector for a truck or tractor vehicle | |
US10012087B2 (en) | Gas turbine including a contoured end wall section of a rotor blade | |
CN105443247A (en) | Pre-cooler inlet ducts that utilize active flow-control and systems and methods including the sam | |
EP2829732B1 (en) | Centrifugal fan and method for manufacturing same | |
JP2017165400A (en) | Method and system for mounting aircraft engine | |
JP2008545572A (en) | Aircraft engine unit | |
CN103381883A (en) | Overpressure door for aircraft | |
CN103748011B (en) | Including turbogenerator with for being connected to the assembly of the system of airframe | |
EP3244020B1 (en) | Gas turbine engine having a vane assembly | |
CN205381408U (en) | Ejector device | |
CN207795413U (en) | The bleed component and gas turbine of gas turbine | |
CN109723571B (en) | Throat offset type pneumatic thrust vectoring nozzle with trapezoidal section and aircraft equipped with same | |
CN108045555B (en) | Spoiler arranged on front edge of deep open type embedded article cabin | |
CN215860343U (en) | Hollow outlet guide vane assembly, aircraft engine and aircraft | |
CN109367797B (en) | Pull-in type layout aircraft air inlet channel with engine power output later | |
CN113606668B (en) | Air duct structure, air supply system and air conditioner | |
CN116305584A (en) | Control surface installation optimization method and structure | |
CN211739300U (en) | Valve plate mounting part and air conditioner | |
CN115749969A (en) | Rotor blade with self-air-entraining front edge and self-adaptive air-jet blade top | |
CN107882653A (en) | Expansion segment pressure self-balancing axisymmetric vectoring exhaust nozzle and there is its aero-engine | |
CN208252789U (en) | One kind is to folder butterfly valve | |
CN103775136A (en) | Vane |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161207 |