CN104963787B - Binary spraying pipe with reverse thrusting function - Google Patents
Binary spraying pipe with reverse thrusting function Download PDFInfo
- Publication number
- CN104963787B CN104963787B CN201510401053.9A CN201510401053A CN104963787B CN 104963787 B CN104963787 B CN 104963787B CN 201510401053 A CN201510401053 A CN 201510401053A CN 104963787 B CN104963787 B CN 104963787B
- Authority
- CN
- China
- Prior art keywords
- convergence plate
- convergence
- pushing away
- circle
- dimensional nozzle
- 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.)
- Active
Links
Landscapes
- Actuator (AREA)
- Nozzles (AREA)
Abstract
The invention relates to the field of aero-engine designing, in particular to a binary spraying pipe with the reverse thrusting function. The problems that an existing reverse thrusting device is complex in structure, and air flow is prone to leakage are solved. The binary spraying pipe with the reverse thrusting function is mainly composed of a circle-to-square cylinder body, a reduction plate, a grid, movable outer covers, connecting rod mechanisms, actuating cylinders and side wall plates. The front end of the circle-to-square cylinder body is connected with an engine. In the normal air exhausting state, an in-spraying-pipe flow passage is composed of the reduction plate and the side wall plates; the actuating cylinders drive the middle section of the reduction plate through the connecting rod mechanisms to rotate to achieve the reverse thrusting function. On the premise that the reverse thrusting function is achieved, the binary spraying pipe guarantees the structural form and the functions of a conventional binary spraying pipe, the overall size is small, the structure is simple, reliability is high, convenience is brought to integration of a machine body, and the defects of a conventional spraying pipe reverse thrusting device are overcome.
Description
Technical field
The present invention relates to Aeroengine Design field, and in particular to a kind of with the anti-two-dimensional nozzle for pushing away function.
Background technology
The raising of air speed and the increase of wing loads, necessarily make to take off increases with distance of landing run, in order to
Shorten aircraft ground run distance and make necessary maneuvering flight action, it is necessary to be counter to push away deceleration device.Traditional grab bucket shape baffling
Plate THR REV, comparison is heavy, and the propulsive thrust load born is big；Deflecting fence THR REV, mechanical coordination part is more, complex structure,
Air-flow is easily revealed causes engine performance to reduce.So the shortcoming in order to make up traditional THR REV, needs a kind of not shadow of design
The conventional version and performance of jet pipe are rung, and with the anti-two-dimensional nozzle for pushing away function.
The content of the invention
It is an object of the invention to provide it is a kind of with the anti-two-dimensional nozzle for pushing away function, solve existing THR REV complex structure
And the problem that air-flow is easily revealed.
The technical scheme is that：There is provided it is a kind of with the anti-two-dimensional nozzle for pushing away function, include circle turn square tube body 1,
Grid 3, movable outer housing 5, converging portion, linkage 8, pressurized strut 9 and rotation dish 10, it is characterised in that：
The circle turns the one end of square tube body 1 and is provided in round, and is fastenedly connected with electromotor, the other end be set to it is square, in
Between seamlessly transit.
The converging portion is symmetricly set on described two side walls comprising two sidewall panelings 7 for vertically and symmetrically arranging and two
Convergence plate between plate 7, the sidewall paneling 7 is with the plate shape that restrains into the inner chamber of converging portion.
The convergence plate includes convergence plate leading portion 2, convergence plate stage casing 6 and convergence plate back segment 4, the convergence plate leading portion 2
One end away from electromotor that one end turns square tube body 1 with the circle is connected, and the other end passes through arc surface with the convergence plate stage casing 6
Overlap joint, the convergence plate stage casing 6 is overlapped with the convergence plate back segment 4 by arc surface again.
The convergence plate stage casing 6 is connected on the sidewall paneling 7 by the rotation dish 10, and the rotation dish 10 is by turning
Axle is connected on the sidewall paneling 7.
The space that the grid 3 is arranged on the convergence plate leading portion 2, the convergence plate back segment 4 and the sidewall paneling 7 are surrounded
It is interior.
The linkage 8, is connected with one end of the pressurized strut 9, the linkage 8 also with two rotation dish
10 roller end connection.
The other end of the pressurized strut 9 turns square tube body 1 and is connected with the circle.
The movable outer housing 5 is symmetricly set on the outside of convergence plate, and two ends are fixedly connected on the rotating shaft of the rotation dish 10
On.
Alternatively, the movable outer housing 5, convergence plate stage casing 6 and the synchronous axial system of rotation dish 10.
Alternatively, the pressurized strut 9 is provided with 2, the symmetrical both sides for being distributed in sidewall paneling 7.
Alternatively, there is a strip chute along jet pipe is axial arranged on the sidewall paneling 7, and chute central plane crosses spray
The axis of pipe, strip chute could be arranged to rectangle chute, it is also possible to which two ends connect the above and below of chute with arc surface.
Alternatively, the strip chute on described two sidewall panelings 7 is symmetrical arranged.
Alternatively, the grid 3 is set to the tetragon grid dress that transverse slat is intersected to form with riser.
Beneficial effects of the present invention：There is provided a kind of with the anti-two-dimensional nozzle for pushing away function, the two-dimensional nozzle is with anti-
On the premise of pushing away function, it is ensured that the version and function of conventional two-dimensional nozzle, contour dimension is little, simple structure, reliability high,
It is easy to fuselage integration, compensate for the defect of conventional THR REV.
Description of the drawings
Fig. 1 is the present invention with the anti-two-dimensional nozzle axonometric chart for pushing away function；
Fig. 2 be the present invention with the anti-two-dimensional nozzle for pushing away function is counter push away working condition when side view；
Fig. 3 be the present invention with the anti-two-dimensional nozzle for pushing away function is counter push away working condition when sectional view；
Fig. 4 be the present invention with it is counter push away the two-dimensional nozzle normal operating conditions of function when side view；
Fig. 5 be the present invention with it is counter push away the two-dimensional nozzle normal operating conditions of function when sectional view；
Fig. 6 is the axonometric chart of grid 3 of the present invention with the anti-two-dimensional nozzle for pushing away function.
Wherein：1-circle turn square tube body, 2-convergence plate leading portion, 3-grid, 4-convergence plate back segment, 5-movable outer housing,
6-convergence plate stage casing, 7-sidewall paneling, 8-linkage, 9-pressurized strut, 10-rotation dish
Specific embodiment
Here exemplary embodiment will be illustrated in detail, its example is illustrated in the accompanying drawings.Explained below is related to
During accompanying drawing, unless otherwise indicated, the same numbers in different accompanying drawings represent identical key element.
As shown in drawings, the present invention provides a kind of with the anti-two-dimensional nozzle for pushing away function, includes circle and turns square tube body 1, lattice
Grid 3, movable outer housing 5, converging portion, linkage 8, pressurized strut 9 and rotation dish 10.
The circle turns the one end of square tube body 1 and is provided in round, and is fastenedly connected with electromotor, the other end be set to it is square, in
Between seamlessly transit, circle turn square tube body 1 be whole two-dimensional nozzle supporting member.
The converging portion is symmetricly set on described two side walls comprising two sidewall panelings 7 for vertically and symmetrically arranging and two
Convergence plate between plate 7, with the convergence plate shape into convergent passage, circle turns square tube body 1 and enters from engine end the sidewall paneling 7
Air-flow can flow out from convergent passage.
The convergence plate includes convergence plate leading portion 2, convergence plate stage casing 6 and convergence plate back segment 4, the convergence plate leading portion 2
One end away from electromotor that one end turns square tube body 1 with the circle is connected, and the other end passes through arc surface with the convergence plate stage casing 6
Overlap joint, the convergence plate stage casing 6 is overlapped with the convergence plate back segment 4 by arc surface again.
The convergence plate stage casing 6 is connected on the sidewall paneling 7 by the rotation dish 10, and the rotation dish 10 is by turning
Axle is connected on the sidewall paneling 7, and rotating shaft is fixed through after sidewall paneling 7 with the movable outer housing 5 being symmetricly set on the outside of convergence plate
Connection, movable outer housing 5, convergence plate stage casing 6 and rotation dish 10 can synchronous axial systems around the shaft.
The space that the grid 3 is arranged on the convergence plate leading portion 2, the convergence plate back segment 4 and the sidewall paneling 7 are surrounded
Interior, when pushing away work as two-dimensional nozzle is counter air ventilation passage.
The linkage 8, is connected with one end of the pressurized strut 9, the linkage 8 also with two rotation dish
10 roller end connection, the linkage 8 of the same side is connected with the roller end of two rotation dish 10 of homonymy, with connecting rod
Axis of rotation is driven in the motor process of mechanism 8, so as to drive movable outer housing 5, convergence plate stage casing 6 and the synchronous axial system of rotation dish 10.
Linkage 8 is driven by pressurized strut 9.Specifically, pressurized strut 9 is axially horizontally disposed along two-dimensional nozzle, one end
Turn square tube body 1 with circle to be fixedly connected, the other end is connected with linkage 8.When two-dimensional nozzle needs execution is counter pushes away order, such as scheme
2nd, shown in Fig. 3, pressurized strut 9 drives convergence plate stage casing 6 to rotate by linkage 8, so that 6 turns upper and lower of convergence plate stage casing
When moving respective precalculated position, mutually overlap joint is allowed to, convergent passage is blocked；Meanwhile, the also synchronous axial system of movable outer housing 5 makes
The anti-inlet, outlet that push away passage is opened simultaneously, gas Jing grids are discharged, so as to realize counter pushing away function.On the contrary, such as Fig. 4, figure
Shown in 5, when jet pipe is in normal exhaust state, movable outer housing 5 is located at the air exit position of grid 3, convergence plate stage casing 6 and receipts
Plate leading portion 2 and the mutually overlap joint of convergence plate back segment 4 are held back, complete convergence plate is formed, air-flow is discharged backward from convergent passage.
The pressurized strut 9 is provided with 2, the symmetrical both sides for being distributed in sidewall paneling 7.
There is a strip chute along jet pipe is axial arranged on the sidewall paneling 7, and chute central plane crosses the axle of jet pipe
Line, strip chute is set to rectangle chute.
Strip chute on described two sidewall panelings 7 is symmetrical arranged.
The grid 3 is set to the tetragon grid dress that transverse slat is intersected to form with riser.
The above, the only specific embodiment of the present invention, but protection scope of the present invention is not limited thereto, any
Those familiar with the art the invention discloses technical scope in, the change or replacement that can be readily occurred in, all should
It is included within the scope of the present invention.Therefore, protection scope of the present invention should be with the scope of the claims
It is accurate.
Claims (6)
1. a kind of with the anti-two-dimensional nozzle for pushing away function, include circle and turn square tube body (1), grid (3), movable outer housing (5), convergence
Section, linkage (8), pressurized strut (9) and rotation dish (10), it is characterised in that：
The circle turns square tube body (1) one end and is provided in round, and is fastenedly connected with electromotor, and the other end is set to square, centre
Seamlessly transit；
The converging portion is symmetricly set on described two sidewall panelings comprising two sidewall panelings for vertically and symmetrically arranging (7) and two
(7) the convergence plate between, the sidewall paneling (7) is with the plate shape that restrains into the inner chamber of converging portion；
The convergence plate includes convergence plate leading portion (2), convergence plate stage casing (6) and convergence plate back segment (4), the convergence plate leading portion
(2) one end away from electromotor that one end turns square tube body (1) with the circle is connected, the other end and it is described convergence plate stage casing (6)
Overlapped by arc surface, it is described to restrain plate stage casing (6) and overlapped by arc surface with convergence plate back segment (4)；
Convergence plate stage casing (6) is connected on the sidewall paneling (7) by the rotation dish (10), and the rotation dish (10) is led to
Cross rotating shaft to be connected on the sidewall paneling (7)；
The grid (3) is arranged on what convergence plate leading portion (2), convergence plate back segment (4) and the sidewall paneling (7) were surrounded
In space；
The linkage (8), is connected with one end of the pressurized strut (9), the linkage (8) also with two rotations
The roller end connection of disk (10)；
The other end of the pressurized strut (9) turns square tube body (1) and is connected with the circle；
The movable outer housing (5) is symmetricly set on the outside of convergence plate, and two ends are fixedly connected on the rotating shaft of the rotation dish (10)
On.
2. according to claim 1 a kind of with the anti-two-dimensional nozzle for pushing away function, it is characterised in that：The movable outer housing
(5), plate stage casing (6) and rotation dish (10) synchronous axial system are restrained.
3. according to claim 1 a kind of with the anti-two-dimensional nozzle for pushing away function, it is characterised in that：The pressurized strut (9)
2 are provided with, the symmetrical both sides for being distributed in sidewall paneling (7).
4. according to claim 1 a kind of with the anti-two-dimensional nozzle for pushing away function, it is characterised in that：The sidewall paneling (7)
On have a strip chute along jet pipe is axial arranged, and chute central plane crosses the axis of jet pipe, and strip chute is set to
Rectangle chute.
5. a kind of with the anti-two-dimensional nozzle for pushing away function according to claim 1 or 4, it is characterised in that：Described two sides
Strip chute on wallboard (7) is symmetrical arranged.
6. according to claim 1 a kind of with the anti-two-dimensional nozzle for pushing away function, it is characterised in that：The grid (3) sets
It is set to the grid dress that transverse slat is intersected to form with riser.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510401053.9A CN104963787B (en) | 2015-07-09 | 2015-07-09 | Binary spraying pipe with reverse thrusting function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510401053.9A CN104963787B (en) | 2015-07-09 | 2015-07-09 | Binary spraying pipe with reverse thrusting function |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104963787A CN104963787A (en) | 2015-10-07 |
| CN104963787B true CN104963787B (en) | 2017-04-19 |
Family
ID=54217842
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510401053.9A Active CN104963787B (en) | 2015-07-09 | 2015-07-09 | Binary spraying pipe with reverse thrusting function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104963787B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106021749B (en) * | 2016-05-25 | 2019-03-05 | 上海交通大学 | The anti-consistency optimization implementation method for pushing away two-dimensional grid |
| CN113107707B (en) * | 2021-04-28 | 2022-03-04 | 中国航发沈阳发动机研究所 | Engine spray pipe structure |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5174502A (en) * | 1991-05-10 | 1992-12-29 | General Electric Company | Support for a translating nozzle vectoring ring |
| FR2796422B1 (en) * | 1999-07-12 | 2001-09-07 | Snecma | AXISYMMETRIC TURBOJET EJECTION NOZZLE, DIVERGENT CONVERGENT WITH JET DEVIATION |
| FR2914700B1 (en) * | 2007-04-04 | 2009-05-22 | Aircelle Sa | THRUST INVERTER FOR REACTION ENGINE |
| CN102877982B (en) * | 2012-07-24 | 2015-04-01 | 中国航空工业集团公司沈阳发动机设计研究所 | Thrust reverser of aero-engine |
| CN103696877A (en) * | 2013-12-05 | 2014-04-02 | 中国航空工业集团公司沈阳发动机设计研究所 | Reverse thrusting device with capacity of adjusting area of spray pipe |
| CN104033282B (en) * | 2014-06-09 | 2016-05-04 | 中国航空工业集团公司沈阳发动机设计研究所 | A kind of binary contracting nozzle with propulsive thrust function |
-
2015
- 2015-07-09 CN CN201510401053.9A patent/CN104963787B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN104963787A (en) | 2015-10-07 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104806378B (en) | A kind of have the anti-binary plug nozzle pushing away function | |
| US3262270A (en) | Thrust reverser | |
| US3262268A (en) | Thrust reverser | |
| US2849861A (en) | Aircraft reaction propulsion units and installations with means to produce reverse thrust | |
| CN104963787B (en) | Binary spraying pipe with reverse thrusting function | |
| US9816462B2 (en) | Integrated thrust reverser device and aircraft engine nacelle equipped therewith | |
| CN101104441A (en) | Gas turbine engine and method of operating same | |
| CN105240158B (en) | It is a kind of that there is the anti-binary plug nozzle for pushing away function | |
| JPH02238159A (en) | Gas turbine jet engine | |
| US4587804A (en) | Device for increasing and deflecting thrust of jet-propulsion engine of V/STOL aircraft | |
| US10450079B2 (en) | Propulsive wing of an aircraft | |
| US20180313297A1 (en) | Turbofan nacelle including a reverser flap | |
| US3280560A (en) | Aircraft jet propulsion power plant | |
| US2802333A (en) | Variable area and direction changing propulsive nozzle | |
| US3734411A (en) | Air brake for jets | |
| US3136500A (en) | Housings for jet propulsion gas turbine engines | |
| CN102753808A (en) | Secondary-air nozzle of a two-flow jet engine having separated flows including a grid thrust reverser | |
| US20120079804A1 (en) | Cowl assembly | |
| US3820626A (en) | Method of and device for attenuating the noise produced by a jet engine nozzle | |
| US3620022A (en) | Thrust reverser for jet propulsion engines | |
| CN104533661B (en) | Thrust-vectoring Nozzle | |
| CN109850128A (en) | Multi-stage blowing circulation volume high-lift device and aircraft | |
| CN109367762A (en) | Tilting duct aircraft auxiliary rudder surface control device | |
| US3024602A (en) | Arrangements for deflecting the jet expelled from a discharge nozzle or from a reaction-propulsion unit | |
| CN105697194A (en) | Binary plug type spray pipe with reactive thrust function |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |