General aircraft is with drawing cigarette device
阅读说明:本技术 一种通用飞机用拉烟装置 (General aircraft is with drawing cigarette device ) 是由 肖明 陈文静 符徐庆 陈博 龚倩玉 于 2020-05-21 设计创作,主要内容包括:本发明属于飞行表演设备技术领域,公开了一种通用飞机用拉烟装置。该通用飞机用拉烟装置,包括壳体,所述壳体的上表面设置有安装挂环,所述壳体内设置有供油机构,所述供油机构包括主油箱、副油箱、抽油泵、供油泵和泄压阀,所述主油箱固定安装在壳体内的左端,且主油箱的注油口位于壳体上表面的左侧并设有油盖。该通用飞机用拉烟装置,主要适用于活塞式发动机航空器,结构简单,成本较低,在使用过程中,副油箱一直处于满油状态,避免了由于飞机机动造成油液面晃动无法抽油的问题,电磁阀可防止管路中存在负压时烟油泄漏,泄压阀可防止管路压力过大而使油管爆裂,大大的提高了本设备的可靠性。(The invention belongs to the technical field of flight performance equipment, and discloses a smoke drawing device for a general airplane. This general aircraft is with drawing cigarette device, including the casing, the upper surface of casing is provided with the installation link, be provided with fuel feeding mechanism in the casing, fuel feeding mechanism includes main tank, bellytank, oil-well pump, fuel feed pump and relief valve, main tank fixed mounting is at the left end in the casing, and the oiling mouth of main tank is located the left side of casing upper surface and is equipped with the oil cap. This general aircraft is with drawing cigarette device mainly is applicable to piston engine airborne vehicle, simple structure, and the cost is lower, and in the use, the bellytank is in full oily state always, has avoided because the aircraft maneuver causes the oil liquid level to rock the problem of unable oil pumping, and the tobacco tar leaks when the solenoid valve can prevent to have the negative pressure in the pipeline, and the relief valve can prevent that pipeline pressure is too big and make oil pipe burst, great improvement the reliability of this equipment.)
1. The utility model provides a general aircraft is with drawing cigarette device, includes casing (1), the upper surface of casing (1) is provided with installation link (2), be provided with fuel feeding mechanism (3), its characterized in that in casing (1): the oil supply mechanism (3) comprises a main oil tank (31), an auxiliary oil tank (32), an oil well pump (33), an oil supply pump (34) and a pressure release valve (35), the main oil tank (31) is fixedly arranged at the left end in the shell (1), an oil filling port of the main oil tank (31) is positioned at the left side of the upper surface of the shell (1) and is provided with an oil cover (36), the auxiliary oil tank (32) is fixedly connected to the bottom wall of the shell (1) and is positioned at the right side of the main oil tank (31), an oil outlet of the main oil tank (31) is communicated with an oil inlet in the middle of the left wall of the auxiliary oil tank (32) through the oil well pump (33), an oil outlet of the right wall of the auxiliary oil tank (32) is respectively and fixedly communicated with a liquid inlet of the pressure release valve (35) and a liquid outlet of an electromagnetic valve (38) through a three-way pipe I (37), and an oil return port of the pressure release valve (35, and a liquid outlet of the electromagnetic valve (38) is communicated with a material spraying mechanism (4).
2. A smoke pulling apparatus for a general purpose aircraft according to claim 1, wherein: spout material mechanism (4) and include arc (41), oil pocket (42) and communicating pipe (43), the one end of communicating pipe (43) is fixed with the liquid outlet of solenoid valve (38) and is linked together, arc (41) comprise five oil spout modules (411), and connect through connecting membrane (412) between five oil spout modules (411) are adjacent, oil pocket (42) are seted up in oil spout module (411), oil spout hole (413) have been seted up at the top of oil spout module (411), the one end opening of oil pocket (42) is located oil spout hole (413) diapire, the other end opening of oil pocket (42) is located the right side of oil spout module (411) and the fixed one end that communicates shunt tubes (44), the other end of five shunt tubes (44) all communicates with the other end of communicating pipe (43).
3. A smoke pulling apparatus for a general purpose aircraft according to claim 1, wherein: oil spout module (411) are triangular prism form and its right-hand member downwarping and are the couple form, connect membrane (412) and be the rubber membrane, and connect membrane (412) and connect and accomodate groove (5) diapire in oil spout module (411) side.
4. A smoke pulling apparatus for a general purpose aircraft according to claim 3, wherein: the section of the oil cavity (42) of the oil injection module (411) is V-shaped, the turning part of the oil cavity (42) is positioned at the left end of the oil injection module (411), and the oil injection module (411) is fixedly connected with the right end of the shell (1) through an elastic rope (6).
5. A smoke pulling apparatus for a general purpose aircraft according to claim 3, wherein: spout material mechanism (4) and still include location magnetic stripe (7), location magnetic stripe (7) bond in the constant head tank of oil spout module (411) lower surface left end.
6. A smoke pulling apparatus for a general purpose aircraft according to claim 1, wherein: the two ends of the oil injection hole (413) are respectively located on the left side and the right side of the oil injection module (411), the left end of the oil injection hole (413) is flat, the axial length range of a long shaft of the oil injection hole is eight-ten centimeters, the right end opening of the oil injection hole (413) is circular, and the aperture range of the oil injection hole is three-five centimeters.
Technical Field
The invention relates to the technical field of flight performance equipment, in particular to a smoke drawing device for a general airplane.
Background
General aircraft are when carrying out the flight performance, often can be in the air through release smog, increase the sight, the release of smog is exactly accomplished by drawing the cigarette device, general aircraft draws the cigarette device, mainly adopt the solid to draw the cigarette device, through burning solid drawing the cigarette bullet at aircraft wing or fin, accomplish and draw the cigarette, or adopt the tobacco tar, realize drawing the cigarette through discharging the tobacco tar atomizing, but either kind of mode all is in order to cause extra pollution when drawing the cigarette, and the performance aircraft often accompanies the action of rolling in drawing the cigarette, the condition of disconnected cigarette easily appears, influence the sight effect.
Disclosure of Invention
The invention aims to provide a smoke drawing device for a general airplane, which is convenient to operate, suitable for piston engine aircrafts and good in smoke drawing effect.
In order to achieve the purpose, the invention is realized by the following technical scheme: a smoke drawing device for a general airplane comprises a shell, wherein the upper surface of the shell is provided with a mounting hanging ring, the oil supply mechanism is arranged in the shell and comprises a main oil tank, an auxiliary oil tank, an oil well pump, an oil supply pump and a pressure release valve, the main oil tank is fixedly arranged at the left end in the shell, and the oil filling port of the main oil tank is positioned on the left side of the upper surface of the shell and is provided with an oil cover, the auxiliary oil tank is fixedly connected with the bottom wall of the shell and is positioned on the right side of the main oil tank, and the oil outlet of the main oil tank is communicated with the oil inlet in the middle of the left wall of the auxiliary oil tank through an oil well pump, the oil outlet of the right wall of the auxiliary oil tank is respectively and fixedly communicated with a liquid inlet of a pressure release valve and a liquid inlet of an electromagnetic valve through a three-way pipe, the liquid outlets of the pressure release valve are respectively communicated with the oil return opening of the main oil tank and the oil return opening of the auxiliary oil tank through a two-way pipe, and the liquid outlet of the electromagnetic valve is.
Preferably, spout material mechanism and include arc, oil pocket and communicating pipe, the one end of communicating pipe is fixed with the liquid outlet of solenoid valve and is communicate, and the arc comprises five oil spout modules, and connects through connecting the membrane between five oil spout modules are adjacent, and the oil pocket is seted up in the oil spout module, and the nozzle opening has been seted up at the top of oil spout module, and the one end opening of oil pocket is located the nozzle opening diapire, and the other end opening of oil pocket is located the right side of oil spout module and the fixed one end that communicates there is the shunt tubes, and the other end of five shunt tubes all communicates with the other end of communicating pipe.
Preferably, the oil spout module is triangular prism form and its right-hand member downwarping and is the couple form, and the design of couple form is convenient to hang the oil spout module at the gas vent of aircraft, utilizes the high temperature tail gas heating atomizing tobacco tar of aircraft, connect the membrane for the rubber membrane, and connect the membrane and connect the groove diapire of accomodating in oil spout module side, connect the distance between each oil spout module of change that the oil spout module can be convenient with connecting the membrane, can draw the width of cigarette to the nimble change of different demands.
Preferably, the section of the oil cavity of the oil injection module is V-shaped, the turning part of the oil cavity is positioned at the left end of the oil injection module, and the oil injection module is fixedly connected with the right end of the shell through an elastic rope.
Preferably, the material spraying mechanism further comprises a positioning magnetic strip, and the positioning magnetic strip is bonded in a positioning groove in the left end of the lower surface of the oil spraying module.
Preferably, two ends of the oil spray hole are respectively located at the left side and the right side of the oil spray module, the left end of the oil spray hole is flat, the axial length range of a long shaft of the oil spray hole is eight-ten centimeters, the right end opening of the oil spray hole is circular, and the aperture range of the oil spray hole is three-five centimeters.
By adopting the technical scheme, the invention has the beneficial effects that:
1. this general aircraft is with drawing cigarette device mainly is applicable to piston engine airborne vehicle, simple structure, and the cost is lower, and in the use, the bellytank is in full oily state always, has avoided because the aircraft maneuver causes the oil liquid level to rock the problem of unable oil pumping, and the tobacco tar leaks when the solenoid valve can prevent to have the negative pressure in the pipeline, and the relief valve can prevent that pipeline pressure is too big and make oil pipe burst, great improvement the reliability of this equipment.
2. This general aircraft is with drawing cigarette device, the arc adopts the disconnect-type design, installs in the aircraft blast pipe, utilizes high temperature waste gas atomizing tobacco tar, helps realizing the miniaturization of device, saves the cost to utilize its disconnect-type design can be through adjusting the play cigarette width that the cigarette was drawn in the distance change between each oil spout module, the practicality is higher.
3. This general aircraft is with drawing cigarette device, the oil pocket of V-arrangement joins in marriage and the left slope design of oil spout module can improve heat exchange efficiency, makes the tobacco tar just can obtain preheating in the oil pocket, can fully atomize after the blowout, and oil pocket outlet design is in the oil spout hole simultaneously, and the structural design of cooperation oil spout hole can be with the fast-speed blowout of tobacco tar when having avoided the tobacco tar to pollute the blast pipe.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a top view of the present invention;
3 FIG. 33 3 is 3 a 3 cross 3- 3 sectional 3
FIG. 4 is a schematic diagram of a fuel injection module according to the present invention;
fig. 5 is a sectional view of an injection module according to the invention.
In the figure: the device comprises a shell 1, a
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 embodiments, and all other embodiments obtained by a person of ordinary skill in the art without creative efforts based on the embodiments of the present invention belong to the protection scope of the present invention.
Referring to fig. 1-5, the present invention provides a technical solution: a general smoke exhaust device for an airplane comprises a shell 1, wherein an
The material spraying mechanism 4 comprises an arc-
The cross-section of
Spout material mechanism 4 and still including location magnetic stripe 7, location magnetic stripe 7 bonds in the constant head tank of
The both ends of
When the general smoke drawing device for the airplane works, before equipment is mounted, smoke oil is injected into a main oil tank 31, after a shell 1 is hung on an airplane body, an arc-
when the smoke is drawn, the
In summary, the following steps: the smoke drawing device for the general airplane is mainly suitable for piston engine aircrafts, has a simple structure and lower cost, and can prevent smoke from leaking when negative pressure exists in a pipeline and prevent an oil pipe from bursting due to overlarge pipeline pressure by the electromagnetic valve, so that the reliability of the device is greatly improved; the arc-shaped plate is in a separated design and is arranged in the airplane exhaust pipe, the high-temperature waste gas is used for atomizing the tobacco tar, the miniaturization of the device is facilitated, the cost is saved, the separated design is utilized, the smoke outlet width of the smoke can be changed by adjusting the distance between the oil injection modules, and the practicability is higher; the design of the V-shaped oil cavity and the slope on the left side of the oil injection module can improve the heat exchange efficiency, so that the tobacco tar can be preheated in the oil cavity, the tobacco tar can be fully atomized after being sprayed out, meanwhile, the oil cavity outlet is designed in the oil injection hole, and the tobacco tar is prevented from polluting the exhaust pipe and can be sprayed out at a high speed by matching the structural design of the oil injection hole.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
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