CN113401342B - Ducted fan wing - Google Patents
Ducted fan wing Download PDFInfo
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- CN113401342B CN113401342B CN202110720641.4A CN202110720641A CN113401342B CN 113401342 B CN113401342 B CN 113401342B CN 202110720641 A CN202110720641 A CN 202110720641A CN 113401342 B CN113401342 B CN 113401342B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/52—Tilting of rotor bodily relative to fuselage
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
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- Aviation & Aerospace Engineering (AREA)
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Abstract
Description
技术领域technical field
本发明涉及涵道飞机领域,具体是一种涵道风扇机翼。The invention relates to the field of ducted aircraft, in particular to a ducted fan wing.
背景技术Background technique
涵道风扇较同样直径的孤立风扇能产生更大的升力,且风扇环括在涵道内,既可阻挡风扇气动声向外传播,又结构紧凑、安全性高。以此为升力面和飞行操纵面可构造出多种小型垂直起降无人飞行器。The ducted fan can generate greater lift than an isolated fan of the same diameter, and the fan is enclosed in the duct, which can prevent the aerodynamic sound of the fan from spreading outward, and has a compact structure and high safety. A variety of small vertical take-off and landing unmanned aerial vehicles can be constructed using this as the lifting surface and the flight control surface.
现有的涵道飞机的机翼倾角调节不便,导致涵道风扇产生的推力方向调节不便;无法对出风口的大小进行调节,导致风压无法调节,无法应对不同情况下的外界干扰气流,因此,针对以上现状,迫切需要开发一种对推力的方向调节方便,对出风口的风压调节方便,外界气流干扰小的涵道风扇机翼,以克服当前实际应用中的不足,满足当前的需求。The inclination angle of the wings of the existing ducted aircraft is inconvenient to adjust, which leads to the inconvenience of adjusting the direction of the thrust produced by the ducted fan; the size of the air outlet cannot be adjusted, resulting in the inability to adjust the wind pressure and the inability to cope with the external disturbance airflow in different situations.
发明内容Contents of the invention
本发明的目的在于提供一种涵道风扇机翼,以解决上述背景技术中提出的问题。The purpose of the present invention is to provide a ducted fan airfoil to solve the problems raised in the background art above.
为实现上述目的,本发明提供如下技术方案:To achieve the above object, the present invention provides the following technical solutions:
一种涵道风扇机翼,包括机翼,所述机翼的右侧安装有转接板,所述转接板的下方安装有涵道,所述涵道通过转接装置与转接板转动连接,所述涵道的底部安装有用于带动其摆动的摆动装置,所述摆动装置的左端与机翼相连,所述涵道内安装有风力装置,所述风力装置的右侧于涵道内安装有过滤网,所述过滤网通过螺钉与涵道可拆卸连接,所述过滤网的右侧于涵道内安装有三个延伸至其外部的口径调节装置。A ducted fan wing, comprising a wing, an adapter plate is installed on the right side of the wing, a duct is installed under the adapter plate, the duct is rotationally connected with the adapter plate through an adapter device, a swing device for driving it to swing is installed at the bottom of the duct, the left end of the swing device is connected with the wing, a wind device is installed in the duct, a filter is installed in the duct on the right side of the wind device, the filter is detachably connected to the duct by screws, and the right side of the filter is connected to the duct There are three caliber adjustment devices extending to the outside installed inside.
作为本发明进一步的方案:所述转接装置包括:转动轴、第一轴套和安装块,所述转动轴焊接于涵道的顶部,所述转动轴的左右两端分别通过轴承与第一轴套转动连接,所述第一轴套通过安装块与转接板相固定。As a further solution of the present invention: the transfer device includes: a rotating shaft, a first shaft sleeve and a mounting block, the rotating shaft is welded to the top of the duct, the left and right ends of the rotating shaft are rotationally connected to the first shaft sleeve through bearings, and the first shaft sleeve is fixed to the adapter plate through the mounting block.
作为本发明进一步的方案:所述涵道的摆动角度为0-20°。As a further solution of the present invention: the swing angle of the duct is 0-20°.
作为本发明进一步的方案:所述摆动装置包括:第一铰座、基座、伺服电机、第一齿轮、第二齿轮、螺纹杆、滚珠、螺纹套和第二铰座,所述基座通过第一铰座与机翼转动连接,所述基座上安装有伺服电机,所述伺服电机的输出轴上安装有第一齿轮,所述第一齿轮的一侧安装有与之转动配合的第二齿轮,所述第二齿轮安装于螺纹杆上,所述螺纹杆通过轴承与基座转动连接,所述螺纹杆的外侧安装有螺纹套,所述螺纹套通过多个滚珠与螺纹杆相连,所述螺纹套的顶部通过第二铰座与涵道的底部转动连接。As a further solution of the present invention: the swing device includes: a first hinge base, a base, a servo motor, a first gear, a second gear, a threaded rod, a ball, a threaded sleeve and a second hinged base. The base is rotationally connected to the wing through the first hinged base. A servo motor is installed on the base. A first gear is installed on the output shaft of the servo motor. The ball is connected with the threaded rod, and the top of the threaded sleeve is rotatably connected with the bottom of the duct through the second hinge seat.
作为本发明进一步的方案:所述风力装置包括:承载板、连接环、通孔、螺栓和风扇,所述连接环通过多个螺栓与涵道可拆卸连接,所述连接环内安装有承载板,所述承载板上均布有多个通孔,所述承载板的右侧安装有风扇。As a further solution of the present invention: the wind power device includes: a bearing plate, a connecting ring, through holes, bolts and a fan, the connecting ring is detachably connected to the duct through a plurality of bolts, a bearing plate is installed in the connecting ring, a plurality of through holes are evenly distributed on the bearing plate, and a fan is installed on the right side of the bearing plate.
作为本发明进一步的方案:三个所述口径调节装置呈圆形均布在涵道上。As a further solution of the present invention: the three diameter adjusting devices are evenly distributed on the duct in a circular shape.
作为本发明进一步的方案:所述口径调节装置包括:液压缸、压力球、调节板、弹簧、第二轴套和销轴,所述液压缸安装于涵道的外侧,所述液压缸的伸缩杆延伸至涵道内与压力球相连,所述压力球的下方安装有调节板,所述调节板的左端安装有销轴,所述销轴延伸至第二轴套内,所述销轴与第二轴套转动连接,所述涵道的内壁安装有多个与调节板相连的弹簧。As a further solution of the present invention: the caliber adjustment device includes: a hydraulic cylinder, a pressure ball, an adjustment plate, a spring, a second bushing and a pin shaft. The hydraulic cylinder is installed outside the duct. The telescopic rod of the hydraulic cylinder extends into the duct to connect with the pressure ball. An adjustment plate is installed below the pressure ball. A pin shaft is installed on the left end of the adjustment plate. The pin shaft extends into the second shaft sleeve.
作为本发明进一步的方案:所述调节板的横截面呈三分之一圆弧状。As a further solution of the present invention: the cross-section of the regulating plate is in the shape of a third of an arc.
与现有技术相比,本发明的有益效果是:该涵道风扇机翼,使用时,打开风扇可以产生推力,通过伺服电机带动第一齿轮转动,通过第一齿轮转动带动第二齿轮转动,通过第二齿轮转动带动螺纹杆转动,通过螺纹杆转动带动螺纹套移动,通过螺纹套移动带动第二铰座摆动,通过第二铰座摆动带动涵道摆动,有利于调节推力的方向;通过液压缸带动压力球移动,通过压力球移动带动调节板摆动,通过调节板摆动实现对出风口大小的调节,进而调节出风口的气压,减小外界气流对涵道出风口气流的影响;通过过滤网可以防止杂物进入到涵道内。综上所述,本发明对推力的方向调节方便,对出风口的风压调节方便,外界气流干扰小。Compared with the prior art, the beneficial effect of the present invention is: when the ducted fan wing is in use, the fan can generate thrust, the first gear is driven to rotate through the servo motor, the second gear is driven to rotate through the rotation of the first gear, the threaded rod is driven to rotate through the rotation of the second gear, the threaded sleeve is driven to move through the rotation of the threaded rod, the second hinge seat is driven to swing through the movement of the threaded sleeve, and the swing of the second hinge base is driven to swing the duct, which is beneficial to adjust the direction of thrust; The adjustment of the size of the tuyere, and then the air pressure of the air outlet, reduces the influence of the external airflow on the airflow of the air outlet of the duct; the filter can prevent debris from entering the duct. To sum up, the present invention is convenient to adjust the direction of the thrust, to adjust the wind pressure at the air outlet, and to have little interference with the external air flow.
附图说明Description of drawings
图1为本发明的结构示意图。Fig. 1 is a structural schematic diagram of the present invention.
图2为本发明中的部分立体结构示意图。Fig. 2 is a schematic diagram of a partial three-dimensional structure in the present invention.
图3为本发明结构示意图的偏转状态示意图。Fig. 3 is a schematic diagram of the deflection state of the structural diagram of the present invention.
图4为本发明的结构示意图中A处的局部视图。Fig. 4 is a partial view at A in the structural schematic diagram of the present invention.
图5为本发明的结构示意图中B-B向视图。Fig. 5 is a B-B arrow view in the structural schematic diagram of the present invention.
图中:1-机翼,2-转接板,3-涵道,4-转接装置,401-转动轴,402-第一轴套,403-安装块,5-摆动装置,501-第一铰座,502-基座,503-伺服电机,504-第一齿轮,505-第二齿轮,506-螺纹杆,507-滚珠,508-螺纹套,509-第二铰座,6-风力装置,601-承载板,602-连接环,603-通孔,604-螺栓,605-风扇,7-过滤网,8-口径调节装置,801-液压缸,802-压力球,803-调节板,804-弹簧,805-第二轴套,806-销轴。Among the figure: 1-wing, 2-adapter plate, 3-duct, 4-transfer device, 401-rotating shaft, 402-first shaft sleeve, 403-installation block, 5-swing device, 501-first hinge seat, 502-base, 503-servo motor, 504-first gear, 505-second gear, 506-thread rod, 507-ball, 508-thread sleeve, 509-second hinge seat, 6-wind device , 601-loading plate, 602-connecting ring, 603-through hole, 604-bolt, 605-fan, 7-filter, 8-diameter adjustment device, 801-hydraulic cylinder, 802-pressure ball, 803-adjusting plate, 804-spring, 805-second bushing, 806-pin.
具体实施方式Detailed ways
为使本发明实施例的目的、技术方案和优点更加清楚,下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。In order to make the purpose, technical solutions and advantages of the embodiments of the present invention more clear, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are part of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
在本发明实施例的描述中,需要说明的是,除非另有明确的规定和限定,术语“第一”“第二”“第三”是为了清楚说明产品部件进行的编号,不代表任何实质性区别。“上”“下”“左”“右”的方向均以附图所示方向为准。对于本领域的普通技术人员而言,可以根据具体情况理解上述术语在本发明实施例中的具体含义。In the description of the embodiments of the present invention, it should be noted that, unless otherwise specified and limited, the terms "first", "second" and "third" are for the purpose of clearly describing the numbering of product components and do not represent any substantial difference. The directions of "up", "down", "left" and "right" are all subject to the directions shown in the attached drawings. Those of ordinary skill in the art can understand the specific meanings of the above terms in the embodiments of the present invention according to specific situations.
需要说明的是,除非另有明确的规定和限定,术语“连接”应做广义理解,例如,可以是直接相连,也可以通过中间媒介间接相连。对于本领域的普通技术人员而言,可以具体情况理解上述术语在发明实施例中的具体含义。It should be noted that, unless otherwise specified and limited, the term "connection" should be understood in a broad sense, for example, it may be a direct connection or an indirect connection through an intermediary. Those of ordinary skill in the art can understand the specific meanings of the above terms in the embodiments of the invention in specific situations.
实施例Example
请参阅图1~5,本发明实施例中,一种涵道风扇机翼,包括机翼1,所述机翼1的右侧安装有转接板2,所述转接板2的下方安装有涵道3,所述涵道3通过转接装置4与转接板2转动连接,所述转接装置4包括:转动轴401、第一轴套402和安装块403,所述转动轴401焊接于涵道3的顶部,所述转动轴401的左右两端分别通过轴承与第一轴套402转动连接,所述第一轴套402通过安装块403与转接板2相固定,所述涵道3的底部安装有用于带动其摆动的摆动装置5,所述摆动装置5的左端与机翼1相连,所述涵道3的摆动角度为0-20°,所述摆动装置5包括:第一铰座501、基座502、伺服电机503、第一齿轮504、第二齿轮505、螺纹杆506、滚珠507、螺纹套508和第二铰座509,所述基座502通过第一铰座501与机翼1转动连接,所述基座502上安装有伺服电机503,所述伺服电机503的输出轴上安装有第一齿轮504,所述第一齿轮504的一侧安装有与之转动配合的第二齿轮505,所述第二齿轮505安装于螺纹杆506上,所述螺纹杆506通过轴承与基座502转动连接,所述螺纹杆506的外侧安装有螺纹套508,所述螺纹套508通过多个滚珠507与螺纹杆506相连,所述螺纹套508的顶部通过第二铰座509与涵道3的底部转动连接,所述涵道3内安装有风力装置6,所述风力装置6包括:承载板601、连接环602、通孔603、螺栓604和风扇605,所述连接环602通过多个螺栓604与涵道3可拆卸连接,所述连接环602内安装有承载板601,所述承载板601上均布有多个通孔603,所述承载板601的右侧安装有风扇605,所述风力装置6的右侧于涵道3内安装有过滤网7,所述过滤网7通过螺钉与涵道3可拆卸连接,所述过滤网7的右侧于涵道3内安装有三个延伸至其外部的口径调节装置8,三个所述口径调节装置8呈圆形均布在涵道3上,所述口径调节装置8包括:液压缸801、压力球802、调节板803、弹簧804、第二轴套805和销轴806,所述液压缸801安装于涵道3的外侧,所述液压缸801的伸缩杆延伸至涵道3内与压力球802相连,所述压力球802的下方安装有调节板803,所述调节板803的横截面呈三分之一圆弧状,所述调节板803的左端安装有销轴806,所述销轴806延伸至第二轴套805内,所述销轴806与第二轴套805转动连接,所述涵道3的内壁安装有多个与调节板803相连的弹簧804。使用时,打开风扇605可以产生推力,通过伺服电机503带动第一齿轮504转动,通过第一齿轮504转动带动第二齿轮505转动,通过第二齿轮505转动带动螺纹杆506转动,通过螺纹杆506转动带动螺纹套508移动,通过螺纹套508移动带动第二铰座509摆动,通过第二铰座509摆动带动涵道3摆动,有利于调节推力的方向;通过液压缸801带动压力球802移动,通过压力球802移动带动调节板803摆动,通过调节板803摆动实现对出风口大小的调节,进而调节出风口的气压,减小外界气流对涵道3出风口气流的影响;通过过滤网7可以防止杂物进入到涵道3内。Please refer to FIGS. 1 to 5. In an embodiment of the present invention, a ducted fan wing includes a wing 1. An adapter plate 2 is installed on the right side of the wing 1. A duct 3 is installed below the adapter plate 2. The duct 3 is rotationally connected with the adapter plate 2 through an adapter device 4. The adapter device 4 includes: a rotating shaft 401, a first sleeve 402 and a mounting block 403. The rotating shaft 401 is welded to the top of the duct 3. The shaft sleeve 402 is rotationally connected, the first shaft sleeve 402 is fixed with the adapter plate 2 through the mounting block 403, the bottom of the duct 3 is equipped with a swing device 5 for driving it to swing, the left end of the swing device 5 is connected with the wing 1, and the swing angle of the duct 3 is 0-20°. 07. Thread sleeve 508 and second hinge seat 509. The base 502 is rotationally connected with the wing 1 through the first hinge seat 501. A servo motor 503 is installed on the base 502. A first gear 504 is installed on the output shaft of the servo motor 503. A second gear 505 is installed on one side of the first gear 504 to rotate with it. The second gear 505 is installed on a threaded rod 506. The threaded rod 506 is connected to the base 502 through a bearing. The outer side of 06 is equipped with a threaded sleeve 508, the threaded sleeve 508 is connected with the threaded rod 506 through a plurality of balls 507, the top of the threaded sleeve 508 is connected to the bottom of the duct 3 through the second hinge seat 509, and the wind power device 6 is installed in the duct 3, and the wind power device 6 includes: a bearing plate 601, a connecting ring 602, a through hole 603, bolts 604 and a fan 605. A bearing plate 601 is installed in the connecting ring 602, a plurality of through holes 603 are evenly distributed on the bearing plate 601, a fan 605 is installed on the right side of the bearing plate 601, a filter screen 7 is installed in the duct 3 on the right side of the wind power device 6, and the filter screen 7 is detachably connected with the duct 3 by screws. Caliber adjustment device 8 includes: hydraulic cylinder 801, pressure ball 802, adjustment plate 803, spring 804, second bushing 805 and pin 806. The hydraulic cylinder 801 is installed outside the duct 3. The telescopic rod of the hydraulic cylinder 801 extends into the duct 3 and connects with the pressure ball 802. An adjustment plate 803 is installed under the pressure ball 802. The cross section of the adjustment plate 803 is one-third arc-shaped. shaft 806 , the pin shaft 806 extends into the second shaft sleeve 805 , the pin shaft 806 is rotationally connected with the second shaft sleeve 805 , and the inner wall of the duct 3 is provided with a plurality of springs 804 connected with the adjustment plate 803 . When in use, turn on the fan 605 to generate thrust, drive the first gear 504 to rotate through the servo motor 503, drive the second gear 505 to rotate through the rotation of the first gear 504, rotate the threaded rod 506 through the rotation of the second gear 505, drive the threaded sleeve 508 to move through the rotation of the threaded rod 506, drive the second hinge seat 509 to swing through the movement of the threaded sleeve 508, and drive the swing of the duct 3 through the swing of the second hinge base 509, which is conducive to adjusting the direction of the thrust; drive the pressure ball through the hydraulic cylinder 801 802 moves, and the adjustment plate 803 is driven to swing by the movement of the pressure ball 802, and the adjustment of the size of the air outlet is realized by the swing of the adjustment plate 803, and then the air pressure of the air outlet is adjusted to reduce the influence of the external air flow on the air flow at the air outlet of the duct 3; the filter screen 7 can prevent foreign matter from entering the duct 3.
该涵道风扇机翼,使用时,打开风扇605可以产生推力,通过伺服电机503带动第一齿轮504转动,通过第一齿轮504转动带动第二齿轮505转动,通过第二齿轮505转动带动螺纹杆506转动,通过螺纹杆506转动带动螺纹套508移动,通过螺纹套508移动带动第二铰座509摆动,通过第二铰座509摆动带动涵道3摆动,有利于调节推力的方向;通过液压缸801带动压力球802移动,通过压力球802移动带动调节板803摆动,通过调节板803摆动实现对出风口大小的调节,进而调节出风口的气压,减小外界气流对涵道3出风口气流的影响;通过过滤网7可以防止杂物进入到涵道3内。The ducted fan wing, when in use, opens the fan 605 to generate thrust. The servo motor 503 drives the first gear 504 to rotate, the first gear 504 rotates to drive the second gear 505 to rotate, the second gear 505 rotates to drive the threaded rod 506 to rotate, the threaded rod 506 rotates to drive the threaded sleeve 508 to move, the threaded sleeve 508 moves to drive the second hinge seat 509 to swing, and the second hinge seat 509 swings to drive the duct 3 to swing, which is beneficial to adjust the direction of thrust; The cylinder 801 drives the pressure ball 802 to move, and the movement of the pressure ball 802 drives the adjustment plate 803 to swing, and the adjustment plate 803 swings to realize the adjustment of the size of the air outlet, and then adjust the air pressure of the air outlet to reduce the influence of the external air flow on the air flow at the air outlet of the duct 3; the filter screen 7 can prevent debris from entering the duct 3.
对于本领域技术人员而言,显然本发明不限于上述示范性实施例的细节,而且在不背离本发明的精神或基本特征的情况下,能够以其他的具体形式实现本发明。因此,无论从哪一点来看,均应将实施例看作是示范性的,而且是非限制性的,本发明的范围由所附权利要求而不是上述说明限定,因此旨在将落在权利要求的等同要件的含义和范围内的所有变化囊括在本发明内。不应将权利要求中的任何附图标记视为限制所涉及的权利要求。It will be apparent to those skilled in the art that the invention is not limited to the details of the above-described exemplary embodiments, but that the invention can be embodied in other specific forms without departing from the spirit or essential characteristics of the invention. Therefore, no matter from which point of view, all the embodiments should be regarded as exemplary and non-restrictive, and the scope of the present invention is defined by the appended claims rather than the above description, so all changes within the meaning and scope of the equivalent elements of the claims are intended to be included in the present invention. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (5)
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3841174A1 (en) * | 1987-10-13 | 1990-06-28 | Kastens Karl | Propeller fan |
CN103925115A (en) * | 2014-04-24 | 2014-07-16 | 北京航空航天大学 | Pull rod bearing translation-type front duct ejector in variable cycle engine adjustable mechanism |
CN107380428A (en) * | 2017-09-04 | 2017-11-24 | 广西悟空科技有限公司 | Dish-style rotor craft |
CN107642434A (en) * | 2017-09-22 | 2018-01-30 | 常俊红 | A kind of power adjustable is without magnetic shaftless ducted fan engine |
CN208291467U (en) * | 2018-05-10 | 2018-12-28 | 中国民航大学 | A kind of double ducted fan vector power short take-off and landing devices of fixed-wing |
CN112443423A (en) * | 2020-11-24 | 2021-03-05 | 南京航空航天大学 | Jet propulsion power system of air-driven ducted fan |
-
2021
- 2021-06-28 CN CN202110720641.4A patent/CN113401342B/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3841174A1 (en) * | 1987-10-13 | 1990-06-28 | Kastens Karl | Propeller fan |
CN103925115A (en) * | 2014-04-24 | 2014-07-16 | 北京航空航天大学 | Pull rod bearing translation-type front duct ejector in variable cycle engine adjustable mechanism |
CN107380428A (en) * | 2017-09-04 | 2017-11-24 | 广西悟空科技有限公司 | Dish-style rotor craft |
CN107642434A (en) * | 2017-09-22 | 2018-01-30 | 常俊红 | A kind of power adjustable is without magnetic shaftless ducted fan engine |
CN208291467U (en) * | 2018-05-10 | 2018-12-28 | 中国民航大学 | A kind of double ducted fan vector power short take-off and landing devices of fixed-wing |
CN112443423A (en) * | 2020-11-24 | 2021-03-05 | 南京航空航天大学 | Jet propulsion power system of air-driven ducted fan |
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