CN113756992B - Gas driven missile swing spray pipe - Google Patents
Gas driven missile swing spray pipe Download PDFInfo
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- CN113756992B CN113756992B CN202110968608.3A CN202110968608A CN113756992B CN 113756992 B CN113756992 B CN 113756992B CN 202110968608 A CN202110968608 A CN 202110968608A CN 113756992 B CN113756992 B CN 113756992B
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- missile
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/97—Rocket nozzles
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
- F02K9/805—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control servo-mechanisms or control devices therefor
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
- Nozzles (AREA)
Abstract
The application provides a gas-driven missile swinging spray pipe, which comprises a combustion chamber and two single-shaft swinging double-spray-pipe assemblies, wherein the two single-shaft swinging double-spray-pipe assemblies are arranged on the same end surface of the combustion chamber in parallel and symmetrical arrangement; the single-shaft swinging double-nozzle assembly is connected into the combustion chamber through a pipeline group; the two single-shaft swinging double-nozzle assemblies have the same components and symmetrical structures; the single-shaft swinging double-nozzle assembly is completely assembled by splicing. The application provides a gas driven guided missile swing spray tube, it is lower to the requirement of power, only need insert standard missile-borne power and make the operation that the electro-magnet work can control whole swing spray tube. This application adopts concatenation formula symmetric design, becomes different short sections with inside gas circuit passageway split, and the part structure after the split is simple for the processing production degree of difficulty greatly reduced reduces manufacturing cost, and control method is simple effective.
Description
Technical Field
The application relates to the technical field of missile thrust vector control equipment, in particular to a gas-driven missile swinging spray pipe.
Background
The traditional rocket engine jet pipe can only provide thrust in the direction of a missile shaft, and the missile needs to adjust the attitude by means of asymmetric aerodynamic moment generated by deflection of an aerodynamic rudder piece. Along with the gradual improvement of the missile on the maneuverability, the attack angle is larger and larger, and the aerodynamic rudder piece cannot meet the combat requirement easily. In contrast, the thrust vector technology generates the torque required for controlling the missile by controlling the deviation of the main thrust relative to the missile axis, does not rely on aerodynamic force, and can generate large control torque even at low speed or high altitude. The thrust vector control system using the swinging spray pipe has the advantages of high control efficiency, small thrust loss and low energy requirement of a control mechanism. Thrust vector control techniques are therefore increasingly being used.
A commonly used technical means is that a servo motor is used as a source of a swinging driving force of a spray pipe, but the servo motor is complex in mechanical structure and high in manufacturing cost, and is difficult to integrate into the integral design of a missile.
Disclosure of Invention
The application provides a gas driven guided missile swing spray tube, guided missile swing spray tube includes: the single-shaft swinging double-nozzle assembly comprises a combustion chamber and two single-shaft swinging double-nozzle assemblies which are arranged on the same end surface of the combustion chamber in parallel and symmetrical arrangement; the single-shaft swinging double-nozzle assembly is connected into the combustion chamber through a pipeline assembly;
the two single-shaft swinging double-nozzle assemblies have the same components and symmetrical structures; the single-shaft swinging double-nozzle assembly is completely assembled by splicing.
Optionally, any single-shaft swinging double-nozzle assembly is in an axisymmetric structure with the center line of the central seat;
the center seat is arranged in the middle of the single-shaft swinging double-nozzle assembly; the central seat is a cuboid;
two symmetrical side surfaces of the central seat are respectively provided with a step-shaped lateral swing spray pipe bracket through screws; the two lateral swing spray pipe brackets have the same structure;
the lateral swing spray pipe support is far away from the outermost side step of the center seat, and a spray pipe ball head base is installed on the lateral swing spray pipe support through screws.
Optionally, the nozzle ball base is of a hollow structure, the lower part of the nozzle ball base is cylindrical, and the nozzle ball base is one of the pipeline groups connected with the combustion chamber; the middle part extends outwards on the basis of the cylinder; the upper part is a ball head.
Optionally, a nozzle ball base is connected with a ball socket nozzle through a shaft hole reserved at the ball head position and a nozzle rotating shaft; the ball and socket spout swings about the spout axis.
Optionally, a shaft hole is reserved in the swing nozzle support (4), and the shape of the shaft hole is matched with that of the cylindrical thrust shaft (11);
end face covers (5) are symmetrically arranged at two ends of the swinging spray pipe bracket (4) respectively; the gap between the two end caps and the thrust shaft (11) forms a first air chamber (14-4) and a second air chamber (14-5) respectively.
Optionally, a square through hole is arranged in the middle of the thrust shaft (11); the ball socket spray pipe (6) is embedded into the square through hole through a convex part to form a revolute pair.
Optionally, the center of the inside of the central seat (9) is a cylindrical through hole, and two sides of the cylindrical through hole are respectively a plurality of stages of concentric circular steps;
a strip cylindrical gas path control shaft is arranged at the cylindrical through hole;
two ends of the air path control shaft are connected with one side of the magnetic suction block through preset processed threads;
the other ends of the magnetic blocks are respectively provided with an electromagnet; the electromagnet is cylindrical; a movable space is reserved between the magnetic suction block and the electromagnet;
the electromagnet is fixed at the position, closest to the round step of the shell, in the center seat through a magnet cover.
Optionally, one side of the cylindrical surface of the gas path control shaft is connected with a gas inlet channel which is positioned at the lower half part of the single-shaft swinging double-nozzle assembly and is vertically arranged; the filter is connected with the central seat through the air inlet channel;
the preset position of the gas path control shaft cylindrical surface is connected with the first channel and the second channel;
the first channel and the second channel are in a splayed structure and are symmetrically distributed;
the other end of the first channel is connected with the first air chamber;
the other end of the second channel is connected with the second air chamber;
the other side of the cylindrical surface of the gas path control shaft is respectively connected with one end of a first gas outlet channel and one end of a second gas outlet channel which are positioned on the upper half part of the single-shaft swinging double-nozzle assembly and are vertically arranged;
the other ends of the first air outlet channel and the second air outlet channel are in contact with the outside air.
Optionally, the gas circuit control shaft is provided with a plurality of concave sections and a plurality of convex sections at intervals in sequence from one end to the other end.
Optionally, in the process that the air path control shaft moves towards any end, any concave section is in contact with any channel, and the channel is in a communication state; if any convex section is contacted with any channel, the channel and the fuel gas are in a separated state;
the channel comprises the air inlet channel, the first channel, the second channel, the first air outlet channel and the second air outlet channel.
The application provides a gas driven guided missile swing spray tube, it is lower to the requirement of power, only need insert standard missile-borne power and make the operation that the electro-magnet work can control whole swing spray tube. This application introduces the engine gas as swing spray tube control power supply, and control torque is far greater than general electric machine control torque, effectively improves the wobbling frequency of spray tube, and the delay condition of consequently controlling can be improved, and when the powder charge burning ended, the control power supply also disappeared simultaneously, does not have the extravagant phenomenon of energy. Simultaneously, this application adopts concatenation formula symmetrical design, with the different short sections of inside gas circuit passageway split, the part simple structure after the split for the processing production degree of difficulty greatly reduced reduces manufacturing cost. The air path control shaft is designed with three symmetrical concave sections to realize the control of the combination of 5 paths of channels, the total displacement of the air path control shaft is only 2mm, the control is quick and effective, secondary boring of a center hole of the center seat is not needed, the processing procedures are reduced, and the control method is simple and effective.
Drawings
FIG. 1 is a schematic structural diagram of a gas-powered missile swinging nozzle provided by an embodiment of the application;
FIG. 2 is a schematic diagram illustrating a single axis swing dual nozzle assembly according to an exemplary embodiment of the present disclosure;
FIG. 3 is a drawing of a thrust shaft coupled to a ball and socket nozzle provided in accordance with an embodiment of the present application;
FIG. 4 is a top cross-sectional view of a single-axis swing dual nozzle assembly according to an embodiment of the present application;
FIG. 5 is a left side cross-sectional view of a single axis swing dual nozzle assembly according to an embodiment of the present application;
FIG. 6 is a perspective view of an internal passageway of a single axis swing dual nozzle assembly in accordance with an exemplary embodiment of the present application;
fig. 7 is a schematic view of an air path control shaft according to an embodiment of the present application.
Detailed Description
To make the objects, technical solutions and advantages of the present application more clear, the following detailed description of the embodiments of the present application will be made with reference to the accompanying drawings.
Refer to fig. 1, which schematically illustrates a structural diagram of a gas-powered missile swinging nozzle provided in an embodiment of the present application.
The gas-driven missile swinging nozzle provided by the embodiment of the application comprises a combustion chamber 1 and two single-shaft swinging double-nozzle assemblies which are arranged on the same end surface of the combustion chamber 1 in parallel and symmetrical arrangement. The single-shaft swinging double-nozzle assembly is connected into the combustion chamber 1 through a pipeline set.
The two single-shaft swinging double-nozzle assemblies are identical in component and symmetrical in structure. The single-shaft swinging double-nozzle assembly is completely assembled by splicing.
In the embodiment of the application, all the components are spliced, the structure is simple, the integral forming method in the traditional method is not adopted, and meanwhile, the problem of difficulty in manufacturing caused by the integral forming method is avoided.
Fig. 2 is a schematic structural diagram of a single-shaft swinging dual nozzle assembly according to an embodiment of the present disclosure.
Any single-shaft swinging double-nozzle assembly is in an axisymmetric structure with the center line of the central seat 9.
Wherein, center seat 9 is arranged at the middle position of the single-shaft swinging double-nozzle assembly. The central seat 9 is a rectangular parallelepiped.
Two symmetrical side surfaces of the central seat 9 are respectively provided with a step-shaped lateral swing nozzle support 4 through screws. The two laterally oscillating lance holders 4 are of identical construction.
And a spray pipe ball head base 7 is arranged at the outermost step of the lateral swing spray pipe bracket 4 far away from the central seat 9 through screws.
Fig. 3 is a schematic diagram of a thrust shaft and ball-and-socket nozzle connection provided in accordance with an embodiment of the present invention.
Specifically, the nozzle bulb base 7 is a hollow structure, and the lower portion of the nozzle bulb base is cylindrical and is one of the pipeline groups used for being connected with the combustion chamber. The middle part extends outwards on the basis of the cylinder. The upper part is a ball head.
A nozzle ball base 7 is connected with a ball socket nozzle 6 through a shaft hole reserved at the ball head position and a nozzle rotating shaft 10. The ball-and-socket nozzle 6 oscillates about the nozzle axis 10. The bottom surface of the ball socket spray pipe 6 is cut at a swinging angle according to needs, and when the cutting surface of the ball socket spray pipe 6 is in contact with the surface of the middle part of the spray pipe ball head base 7, the limitation on the swinging angle is realized. The actual cutting angle can be adjusted as required by the actual swing angle.
And a shaft hole is reserved in the swing nozzle support 4, and the shape of the shaft hole is matched with that of the cylindrical thrust shaft 11.
End covers 5 are symmetrically arranged at two ends of the swinging nozzle support 4 respectively. The gap between the two end caps and the thrust shaft 11 forms a first air chamber 14-4 and a second air chamber 14-5, respectively.
The pressure difference between the first 14-4 and second 14-5 chambers will force the inferential shaft 11 to move in the shaft hole.
The middle of the thrust shaft 11 is provided with a square through hole. The ball socket nozzle 6 is embedded into the square through hole through the convex part to form a revolute pair.
The axial translation of the thrust shaft 11 is converted by the bulge into a rotation of the ball-and-socket nozzle 6 about the nozzle axis 10.
FIG. 4 is a top cross-sectional view of a single axis swing dual nozzle assembly according to an embodiment of the present application.
As clearly shown in fig. 4, the center of the center base 9 is a cylindrical through hole, and the two sides of the cylindrical through hole are respectively provided with multiple stages of concentric circular steps.
The cylindrical through hole is provided with a strip cylindrical air passage control shaft 12. The air passage control shaft 12 in the embodiment of the present application may be turned from a cylindrical metal rod.
Two ends of the air path control shaft 12 are connected with one side of the magnetic suction block 13 through preset processed threads.
The other ends of the magnetic blocks 13 are respectively provided with an electromagnet 3. The electromagnet 3 is cylindrical. A movable space is reserved between the magnetic block 13 and the electromagnet 3.
The electromagnet 3 is fixed at the round step closest to the shell in the center seat 9 through the magnet cover 2.
When the electromagnet 3 on any one side is electrified, the magnetic suction block 13 is attracted to drive the air path control shaft 12 to move between the electromagnet 3 and the central seat 9 along the axial direction, and the total stroke is 2 mm. By the arrangement, when the electrified magnet is switched, the magnetic attraction can be quickly and in place.
In the embodiment of the application, a plurality of channels are provided, which are key factors for realizing swing, different channels are combined and connected, and corresponding torque is provided for the swing of the ball socket nozzle 6. The passageway generally is long and thin hole, but the integrated into one piece technique among the prior art makes the manufacturing of long and thin hole very difficult, but this application adopts the mosaic structure design, has effectively shortened the length of every hole to the processing degree of difficulty has been reduced.
FIG. 5 is a left side sectional view of a single axis swing double nozzle assembly according to an embodiment of the present application. FIG. 6 is a perspective view of the internal passage of a single axis oscillating dual nozzle assembly according to an embodiment of the present application.
The channels in the embodiments of the present application will be described in detail below in conjunction with other components provided in the embodiments of the present application. The channels include an inlet channel 14-1, a first channel 14-2, a second channel 14-3, a first outlet channel 14-6, and a second outlet channel 14-7.
One side of the cylindrical surface of the air path control shaft 12 is connected with an air inlet channel 14-1 which is positioned at the lower half part of the single-shaft swinging double-nozzle assembly and is vertically arranged. The filter 8 is connected to the central seat 9 by means of an inlet duct 14-1.
It should be noted that the inlet duct 14-1 is the second duct set. The residue of the fuel gas is filtered by the filter 8, so that the blockage of the inner channel of the single-shaft swinging double-jet pipe group is prevented.
The air path control shaft 12 is connected to the first passage 14-2 and the second passage 14-3 at predetermined positions on the cylindrical surface thereof.
The first channel 14-2 and the second channel 14-3 are in a splayed structure and are symmetrically distributed.
The other end of the first passage 14-2 is connected to the first air chamber 14-4.
It should be noted that the first channel 14-2 and the second channel 14-3 are formed by splicing a hole in the center seat 9 and a hole in the lateral swing nozzle support 4, and a small groove is milled at the splicing position to install a red copper gasket 15, so that the air tightness of the connection is ensured.
The other end of the second passage 14-3 is connected to the second air chamber 14-5.
The other side of the cylindrical surface of the gas path control shaft 12 is respectively connected with one end of a first gas outlet channel 14-6 and one end of a second gas outlet channel 14-7 which are vertically arranged on the upper half part of the single-shaft swinging double-nozzle assembly.
The other ends of the first outlet channel 14-6 and the second outlet channel 14-7 are in contact with the outside air.
Fig. 7 is a schematic view of an air passage control shaft according to an embodiment of the present disclosure.
In the embodiment of the present application, the air path control shaft 12 is sequentially provided with a plurality of concave sections and a plurality of convex sections at intervals from one end to the other end. As shown in FIG. 7, the gas path control shaft comprises a concave section 16-1-1, a convex section 16-2-1, a concave section 16-1-2, a convex section 16-2-2 and a concave section 16-1-3 in sequence from one end to the other end.
When any concave section is contacted with any channel in the process of moving towards either end of the air path control shaft 12, the channel is in a communication state. If any convex section is contacted with any channel, the channel is separated from the gas.
The working process of the gas-driven missile swinging nozzle provided by the application is specifically explained in combination with a specific working process.
If the left electromagnet 3 is electrified and the right electromagnet is not electrified, the left magnetic attraction block 13 is attracted to the electromagnet 3 under the action of magnetic force to drive the gas path control shaft 12 to move towards the left side, the concave section 16-1-2 in the center of the gas path control shaft 12 enables the gas inlet channel 14-1 to be simultaneously communicated with the first channel 14-2, and the convex section 16-2-1 and the convex section 16-2-2 enable the second channel 14-3 and the first gas outlet channel 14-6 to be in an isolated state and cannot be communicated with the gas inlet channel 14-1. Thus, the combustion gas comes out of the combustion chamber 1, passes through the intake passage 14-1, passes through the first passage 14-2, and then reaches the first air chamber 14-4. At this time, the pressure in the first air chamber 14-4 is equal to the great pressure in the combustion chamber.
Meanwhile, the right concave section 16-1-3 of the air passage control shaft 12 connects the second outlet channel 14-7 with the second channel 14-3, and the second channel 14-3 communicates with the second air chamber 14-5. The pressure in the second air chamber 14-5 is at the ambient atmospheric pressure.
The pressure intensity in the first air chamber 14-4 at one side of the thrust shaft 11 is equal to the huge pressure intensity in the combustion chamber, and the atmospheric pressure of the second air chamber 14-5 at the other side of the thrust shaft 11 is equal to the huge pressure intensity in the combustion chamber, so that when the thrust shaft is subjected to the huge thrust force towards the right, the thrust shaft 11 rapidly translates towards the right, and simultaneously drives the ball socket spray pipe 6 to rotate towards the left around the spray pipe rotating shaft 10.
Similarly, when the magnet on the right side is electrified, the ball socket nozzle 6 can be rotated rightwards. Since the first channel 14-2 and the second channel 14-3 are respectively symmetrical about the air path control axis 12, that is, two air chambers in the same direction of the two thrust shafts 11 are communicated, the motion of the two thrust shafts is completely consistent, and the swing of the two ball-and-socket nozzles 6 on the single-shaft swing double-nozzle assembly is always synchronous.
Referring to fig. 1, when the connection line of the two groups of nozzles is in the horizontal plane, the two groups of nozzles can swing up and down in the same direction, and when the two groups of nozzles swing in the same direction, 4 nozzles deflect in the same direction to control the pitching channel. When the connecting line of the two groups of spray pipes is positioned on a vertical plane, the two groups of spray pipes can swing left and right to control a yawing channel. At any time, the two groups of spray pipes deflect towards opposite directions, so that the projectile body can roll clockwise or anticlockwise, and the rolling channel is controlled. When the connecting line of the two groups of spray pipes is not positioned on a vertical plane or a horizontal plane, thrust vector control under any flight attitude can be realized by only combining an attitude control algorithm and carrying out combined calculation on pitching, yawing and rolling. The two groups of single-shaft swinging double spray pipes have 4 electromagnets to be controlled, but the electrifying states of the electromagnets on each group of single-shaft swinging double spray pipes are opposite, and the electrifying state of the electromagnet on the opposite side is determined as long as the electrifying state of the electromagnet is determined in each group of single-shaft swinging double spray pipes, so that the two pairs of electromagnets are only 0/1-0/1, 0/1-1/0, 1/0-0/1 and 1/0-1/0 in on-off combination, and in actual control, the pitching, yawing and rolling control of the projectile body can be realized only by two control channels, and the design difficulty of a control system is greatly reduced.
The application provides a gas driven guided missile swing spray tube is different from using motor drive's swing spray tube, and is lower to the requirement of power, only needs to insert standard missile-borne power and makes the operation that the whole swing spray tube can be controlled in the work of electro-magnet. This application introduces the engine gas as swing spray tube control power supply, and control torque is far greater than general motor control torque, effectively improves the wobbling frequency of spray tube, and consequently the delay condition of control can be improved, and when the powder charge burning ended, the control power supply also disappeared simultaneously, does not have the extravagant phenomenon of energy. Simultaneously, this application adopts concatenation formula symmetrical design, with the different short sections of inside gas circuit passageway split, the part simple structure after the split for the processing production degree of difficulty greatly reduced reduces manufacturing cost. The air path control shaft is designed with three symmetrical concave sections to realize the control of the combination of 5 paths of channels, the total displacement of the air path control shaft is only 2mm, the control is quick and effective, secondary boring of a center hole of the center seat is not needed, the processing procedures are reduced, and the control method is simple and effective.
The above-described embodiments of the present application do not limit the scope of the present application.
Claims (5)
1. A gas powered missile swinging nozzle, comprising: the device comprises a combustion chamber (1) and two single-shaft swinging double-nozzle assemblies which are arranged on the same end surface of the combustion chamber (1) and are symmetrically arranged in parallel; the single-shaft swinging double-nozzle assembly is connected into the combustion chamber (1) through a pipeline group;
the two single-shaft swinging double-nozzle assemblies have the same components and symmetrical structures; the single-shaft swinging double-nozzle assembly is completely assembled by splicing;
any single-shaft swinging double-nozzle assembly is in an axisymmetric structure by taking the central line of the central seat (9);
the center seat (9) is arranged in the middle of the single-shaft swinging double-nozzle assembly; the central seat (9) is a cuboid;
two symmetrical side surfaces of the central seat (9) are respectively provided with a step-shaped lateral swing spray pipe bracket (4) through screws; the two lateral swing spray pipe brackets (4) have the same structure;
the lateral swing spray pipe support (4) is far away from the outermost side step of the central seat (9), and a spray pipe ball head base (7) is installed through screws;
the nozzle ball head base (7) is of a hollow structure, the lower part of the nozzle ball head base is cylindrical, and the nozzle ball head base is one of pipeline groups used for being connected with the combustion chamber; the middle part extends outwards on the basis of the cylinder; the upper part is a ball head;
a nozzle ball base (7) is connected with a ball socket nozzle (6) through a shaft hole reserved at the ball head position and a nozzle rotating shaft (10); the ball socket nozzle (6) swings around the nozzle rotating shaft (10);
a shaft hole is reserved in the swing nozzle support (4), and the shape of the shaft hole is matched with that of the cylindrical thrust shaft (11);
end face covers (5) are symmetrically arranged at two ends of the swinging spray pipe bracket (4) respectively; the gaps between the two end face covers and the thrust shaft (11) form a first air chamber (14-4) and a second air chamber (14-5) respectively;
the center of the interior of the central seat (9) is a cylindrical through hole, and two sides of the cylindrical through hole are respectively provided with a plurality of stages of concentric circular steps;
a strip cylindrical gas path control shaft (12) is arranged at the cylindrical through hole;
two ends of the air path control shaft (12) are connected with one side of the magnetic suction block (13) through preset and processed threads;
the other ends of the magnetic blocks (13) are respectively provided with an electromagnet (3); the electromagnet (3) is cylindrical; a movable space is reserved between the magnetic suction block (13) and the electromagnet (3);
the electromagnet (3) is fixed at a round step closest to the shell in the center seat (9) through a magnet cover (2).
2. Missile swinging lance according to claim 1, characterized in that a square through hole is provided in the middle of the thrust shaft (11); the ball socket spray pipe (6) is embedded into the square through hole through a convex part to form a revolute pair.
3. The missile swinging nozzle according to claim 2, wherein one side of the cylindrical surface of the gas path control shaft (12) is connected with a vertically arranged gas inlet channel (14-1) which is positioned at the lower half part of the single-shaft swinging double-nozzle assembly; the filter (8) is connected with the central seat (9) through the air inlet channel (14-1);
the preset position of the cylindrical surface of the gas path control shaft (12) is connected with the first channel (14-2) and the second channel (14-3);
the first channel (14-2) and the second channel (14-3) are in a splayed structure and are symmetrically distributed;
the other end of the first channel (14-2) is connected with the first air chamber (14-4);
the other end of the second channel (14-3) is connected with the second air chamber (14-5);
the other side of the cylindrical surface of the gas path control shaft (12) is respectively connected with one end of a first gas outlet channel (14-6) and one end of a second gas outlet channel (14-7) which are positioned at the upper half part of the single-shaft swinging double-nozzle assembly and are vertically arranged;
the other ends of the first air outlet channel (14-6) and the second air outlet channel (14-7) are in contact with the outside air.
4. Missile swinging lance according to claim 3, wherein the gas path control shaft (12) has a plurality of concave sections and a plurality of convex sections spaced in sequence from one end to the other.
5. Missile swinging nozzle according to claim 4, characterized in that the air passage control shaft (12) is in communication state when any concave section is in contact with any channel during movement to either end; if any convex section is contacted with any channel, the channel and the fuel gas are in a separated state;
the channels include the inlet channel (14-1), the first channel (14-2), the second channel (14-3), the first outlet channel (14-6), and the second outlet channel (14-7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110968608.3A CN113756992B (en) | 2021-08-23 | 2021-08-23 | Gas driven missile swing spray pipe |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110968608.3A CN113756992B (en) | 2021-08-23 | 2021-08-23 | Gas driven missile swing spray pipe |
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| CN113756992A CN113756992A (en) | 2021-12-07 |
| CN113756992B true CN113756992B (en) | 2022-08-19 |
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| CN202110968608.3A Active CN113756992B (en) | 2021-08-23 | 2021-08-23 | Gas driven missile swing spray pipe |
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Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3016427A1 (en) * | 1980-04-29 | 1983-04-07 | Bayern-Chemie Gesellschaft für flugchemische Antriebe mbH, 8261 Aschau | Drive for jet rudders or discharge nozzles of rocket motors - has working cylinder of movable ring sector, with stationary sealing piston |
| CN101025128A (en) * | 2006-02-24 | 2007-08-29 | 同济大学 | Axial symmetric vector spray-pipe A9 action emergency resetting hydraulic system |
| CN107529369B (en) * | 2012-03-01 | 2015-01-14 | 北京理工大学 | A kind of double venturi formula jet executive component |
| CN107525676A (en) * | 2017-08-31 | 2017-12-29 | 南京理工大学 | The simple fictitious load of thrust vectoring engine gas rudder and test device |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3045743B1 (en) * | 2015-12-17 | 2018-08-24 | Safran Nacelles | HYDRAULIC ROTO-LINEAR PUSH-INVERTER AND VARIABLE SECTION TUBE ACTUATOR |
| US11384850B2 (en) * | 2020-02-14 | 2022-07-12 | Hamilton Sundstrand Corporation | Hydraulic control valves for ram air turbine stow actuators |
-
2021
- 2021-08-23 CN CN202110968608.3A patent/CN113756992B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3016427A1 (en) * | 1980-04-29 | 1983-04-07 | Bayern-Chemie Gesellschaft für flugchemische Antriebe mbH, 8261 Aschau | Drive for jet rudders or discharge nozzles of rocket motors - has working cylinder of movable ring sector, with stationary sealing piston |
| CN101025128A (en) * | 2006-02-24 | 2007-08-29 | 同济大学 | Axial symmetric vector spray-pipe A9 action emergency resetting hydraulic system |
| CN107529369B (en) * | 2012-03-01 | 2015-01-14 | 北京理工大学 | A kind of double venturi formula jet executive component |
| CN107525676A (en) * | 2017-08-31 | 2017-12-29 | 南京理工大学 | The simple fictitious load of thrust vectoring engine gas rudder and test device |
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| CN113756992A (en) | 2021-12-07 |
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