WO2021218703A1 - 一种飞碟飞行器 - Google Patents

一种飞碟飞行器 Download PDF

Info

Publication number
WO2021218703A1
WO2021218703A1 PCT/CN2021/088338 CN2021088338W WO2021218703A1 WO 2021218703 A1 WO2021218703 A1 WO 2021218703A1 CN 2021088338 W CN2021088338 W CN 2021088338W WO 2021218703 A1 WO2021218703 A1 WO 2021218703A1
Authority
WO
WIPO (PCT)
Prior art keywords
flying
cabin
bracket
propeller
electromagnetic
Prior art date
Application number
PCT/CN2021/088338
Other languages
English (en)
French (fr)
Inventor
耿起志
Original Assignee
Geng Qizhi
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Geng Qizhi filed Critical Geng Qizhi
Priority to DE212021000318.4U priority Critical patent/DE212021000318U1/de
Publication of WO2021218703A1 publication Critical patent/WO2021218703A1/zh

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/001—Flying saucers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/003—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
    • B64C39/006—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a vertical axis
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/02—Arrangements or adaptations of signal or lighting devices

Definitions

  • the invention relates to the technical field of aircraft, in particular to a flying saucer aircraft.
  • a flying saucer aircraft including a saucer body, a flying propeller, and a landing bracket.
  • the middle of the saucer body is provided with an electromagnetic track in the circumferential direction, and the electromagnetic track is recessed inward from the center.
  • "Concave"-shaped track the electromagnetic track is provided with an electromagnetic levitation vehicle matched with it, and the flying paddle is connected to the outer surface of the electromagnetic levitation vehicle, and can be driven by the electromagnetic levitation vehicle to rotate around the dish body along the electromagnetic track, so
  • a turbojet bracket is also provided on both sides of the disk body and located at the lower part of the flying propeller.
  • the turbojet bracket is connected with a turbojet.
  • the turbojet on one side of the disk body is vertically arranged. One side is horizontally arranged, the lowering bracket is arranged at the bottom of the dish body, and the lowering bracket is a folding bracket.
  • a flight paddle protective cover is provided on the outside of the flying paddle, and a flight paddle protective cover is provided on the outside of the flying paddle.
  • the upper and lower ends of the ring-shaped protective bracket respectively extend in the direction of the dish body and are provided with a net body and a lower net body capable of covering the flying paddle, and the ends of the net body and the lower net body are connected with the dish body.
  • the flying propeller includes an annular flying propeller bracket arranged on the outside of the electromagnetic levitation vehicle, and the annular flying propeller bracket is provided with several blades circumferentially.
  • the blade is an inclined blade with an included angle with the horizontal plane.
  • the dish body includes a center cabin with an electromagnetic track, the upper part of the center cabin is provided with an upper propulsion device placement cabin, a control center placement cabin, and a driving device placement cabin, and the lower part of the center cabin is provided There are a lower propulsion device placement cabin and a power supply device placement cabin for the upper propulsion device placement cabin, the control center placement cabin, the driving device placement cabin, and the lower propulsion device placement cabin.
  • the top of the driving device placement cabin is Open and close the top hatch.
  • an escape ejection seat is provided in the driving device placement cabin.
  • the bottom of the dish body is provided with an inverted cabin door, the inner side of the inverted cabin door is provided with a step, the dish body is provided with an access channel from the inverted cabin door to the driving device placement cabin, and the access channel is provided with There are vertical ladders arranged along the entrance and exit channels.
  • the upper propulsion device is placed on the cabin body, and the control center is placed on the outer surface of the cabin body with solar panels.
  • the openable top hatch cover is a transparent hatch cover.
  • a number of illuminating lamps are also provided on the outer side of the annular protective bracket.
  • the present invention has the following advantages: the aircraft of this application can be used as a new aircraft for transportation, travel, exploration and other activities; the aircraft of this application does not require a special runway for take-off and landing, can take off and land vertically, and can fly in the air At the same time, the direction of the propulsion device is controlled by the direction of the transverse turbojet under the flight propeller protective cover or the upper and lower propulsion device chambers, so that the direction can be easily changed.
  • Fig. 1 is a schematic diagram of the structure of a flying saucer aircraft of the present invention.
  • Fig. 2 is a schematic diagram of the structure of a protective cover of a flying propeller in a flying saucer aircraft of the present invention.
  • Fig. 3 is a schematic diagram of the structure of an electromagnetic orbit in a flying saucer aircraft of the present invention.
  • Fig. 4 is a schematic structural diagram of a flying paddle in a flying saucer aircraft of the present invention.
  • Fig. 5 is a schematic diagram of the structure of the upper and lower steps in a flying saucer aircraft of the present invention.
  • Dish body 1.1, center cabin, 1.2, upper propulsion device placement cabin, 1.3, control center placement cabin, 1.4, driving device placement cabin, 1.5, lower propulsion device placement cabin, 1.6 ,
  • the power supply device is placed in the cabin, 2.
  • Flying propeller 2.1, Annular flying propeller bracket, 2.2, propeller blade, 3, landing bracket, 4, electromagnetic track, 5, electromagnetic levitation vehicle, 6, turbojet bracket, 7, turbine Jet, 8, flight propeller protective cover, 8.1, ring protection bracket, 8.2, net body, 8.3, lower net body, 9, flip hatch, 10, access channel, 11, up and down stairs, 12, lighting.
  • a flying saucer aircraft is characterized in that it comprises a dish body 1, a flying propeller 2, a landing bracket 3, the middle of the dish body 1 is provided with an electromagnetic track 4 in the circumferential direction, and the electromagnetic track 4 is recessed inward from the center.
  • “Concave”-shaped track the electromagnetic track 4 is provided with an electromagnetic levitation vehicle 5 matching it, and the flying paddle 2 is connected to the outer surface of the electromagnetic levitation vehicle 5, and can be driven by the electromagnetic levitation vehicle 5 along the electromagnetic track
  • the disc body 1 rotates.
  • a turbojet support 6 is also provided on both sides of the disc body 1 and located at the lower part of the flying propeller 2.
  • the turbojet support 6 is rotatably connected with a turbojet 7, and the disc
  • the turbojet 7 on one side of the body 1 is arranged vertically, and the other side is arranged horizontally.
  • the landing bracket 3 is arranged at the bottom of the dish body 1, and the landing bracket 3 is a folding bracket.
  • the flying propeller 2 is provided with a flying propeller protective cover 8 which includes an annular protective bracket 8.1 arranged on the outside of the flying propeller 2 and on the same horizontal plane.
  • the upper and lower ends of the ring-shaped protective bracket 8.1 extend in the direction of the dish 1 and can cover the flying paddle 2 on the net body 8.2 and the lower net body 8.3.
  • the ends of the net body 8.2 and the lower net body 8.3 are all connected to the dish body 1 .
  • the setting of the flying propeller protective cover 8 does not affect air circulation, and can prevent floating objects and birds from entering the rotor blades.
  • the flying propeller 2 includes an annular flying propeller bracket 2.1 arranged outside the electromagnetic levitation vehicle 5, and the annular flying propeller bracket 2.1 is provided with several blades 2.2 in the outer circumferential direction.
  • the blade 2.2 is an inclined blade with an included angle with the horizontal plane.
  • the dish body 1 includes a central cabin 1.1 equipped with an electromagnetic track 4, the upper part of the central cabin 1.1 is provided with an upper propulsion device placement cabin 1.2, and a control center placement cabin 1.1 1.3 and the driving device placement cabin 1.4, the lower part of the center cabin 1.1 is provided with a lower propulsion device placement cabin 1.5 and a cabin for the upper propulsion device 1.2, a control center placement cabin 1.3, a driving device placement cabin 1.4, and a lower propulsion device
  • the power supply device for placing the power supply in the cabin 1.5 is placed in the cabin 1.6, and the top of the driving device placement cabin 1.4 is an openable top hatch.
  • the electromagnetic track 4 is a central recessed track
  • the electromagnetic levitation vehicle 5 is embedded in the central recess of the electromagnetic track 4
  • the magnetic poles of the electromagnetic levitation vehicle 5 and the electromagnetic track 4 repel the magnetic poles.
  • the electromagnetic levitation vehicle 5 is wound around the disc body 1 along the electromagnetic track 4 by using the traction force of the electromagnetic coil set inside the electromagnetic track 4
  • it rotates it drives a circle of flying propeller 2 outside the electromagnetic levitation vehicle 5 to rotate.
  • the upward force of the flying propeller 2 is large enough to drive the entire dish 1 to levitate upwards, and then use the flying propeller to protect the lower part of the cover.
  • the vertical turbojet aircraft slightly pushes the rear of the flying saucer upwards, so that the flying paddle sucks air from top to bottom, and then sucks air from the top to the back, imitating the propulsion of a helicopter, so as to realize the suspension of the flying saucer.
  • the flying saucer when the flying saucer is started, the rotor blades rotate, and its strong centrifugal force will cause the whole disk body to rotate, so at the same time, start the horizontal turbojet set under the flying blade protection cover to control the stability of the disk body.
  • the direction of the transverse turbojet set under the protective cover of the flying propeller can be adjusted by increasing and decreasing the rotation speed.
  • the directional control propulsion device arranged in the propulsion device chambers on the upper and lower layers of the dish body can be set to work left and right to achieve direction adjustment. For example, when turning to the left, start the direction control propulsion device on the right side, Turn to the left. When turning to the right, the direction control propulsion device on the left can be activated, and the disc body is turned to the right. It can also be used in the future when the flying saucer is applied to outer space, in an environment where there is no air, it can be propelled by activating this propulsion device. The direction of the propulsion device can be adjusted by the direction of the propulsion device room.
  • the power supply group in the power supply machine room can be set as a battery pack or a nuclear power pack, and the power supply device is placed in the lower part of the dish body. After the power supply device is installed, the flying saucer can keep the center of gravity downward, so as not to tilt or somersault;
  • an escape ejection seat is provided in the driving device placement cabin 1.4.
  • the control center placement cabin is also provided with a large parachute and jetting device for landing the flying saucer aircraft, and its outlet is connected to the center of the piloting device placement cabin.
  • the flying saucer is flying in the air
  • the synchronous automatic top hatch is opened, or directly blasted, and then a large parachute is ejected for the flying saucer to land, which can greatly improve the safety of the flying saucer.
  • the chairs pop out of the cabin together. The pilot pulls away the parachute he wears, throws away the seat, and descends.
  • the ejection method of military aircraft can be borrowed to ensure the safety of the pilot and the ejection posture of the pilot's head up, and then throw the parachute.
  • the bottom of the dish body 1 is provided with an inverted cabin door 9, the inner side of the inverted cabin door 9 is provided with a step, and the dish body 1 is provided with an inverted cabin door 9 to
  • the entry and exit passage 10 of the driving device placement cabin 1.4 is provided with a simple upper and lower ladder 11 that goes up and down along the entry and exit passage 10 in the entry and exit passage 10.
  • solar panels are laid on the outer surfaces of the upper propulsion device placement cabin 1.2 and the control center placement cabin 1.3.
  • the openable top hatch cover is a transparent hatch cover.
  • the outer side of the ring protection bracket 8.1 is also provided with several lighting lamps 12, which can be turned on at night for lighting and beautification during take-off and landing.
  • one end of the flying saucer can be equipped with a headlight .
  • the invention can be used as a new aircraft for transportation, travel, exploration and other activities; it can be used as a spacecraft; it can be used as a flying saucer simulation toy.

Abstract

一种飞碟飞行器，包括碟体（1）、飞行桨（2）、降落支架（3），所述碟体（1）中部周向设有电磁轨道（4），所述电磁轨道（4）为中部向内凹陷的"凹"字型轨道，所述电磁轨道（4）内设置有与其配合的电磁悬浮车（5），所述飞行桨（2）连接于电磁悬浮车（5）外表面，并可在电磁悬浮车（5）的带动下沿电磁轨道绕碟体（1）转动，所述碟体（1）两侧并位于飞行桨（2）下部的位置上还设有涡轮喷气机支架（6），所述涡轮喷气机支架（6）上可转动连接有涡轮喷气机（7），所述降落支架（3）设置于碟体底部，所述降落支架为折叠支架，该飞行器可以作为一种新的飞行器，进行运输、旅行、勘探等活动，起降不需要专用跑道，可以垂直起降，可以在空中飞行的同时，通过涡轮喷气机方便的转换方向。

Description

一种飞碟飞行器 技术领域
本发明涉及飞行器技术领域，具体是指一种飞碟飞行器。
背景技术
现有的飞行器主要是飞机、滑翔机、直升机、热气球，对于碟形飞行器，目前主要体现在影视当中和图画当中，而且飞机飞行有很多限制条件，如：需要有专用的跑道，另一方面现有的飞行器都不是中心对称结构，在空中飞行时，遇到异常气流，受干扰较严重，并具有转向不灵活的缺陷。所以创造一种新的以碟形为主的飞行器，显得很有必要，并且可以使我们的飞行器多一个种类。
发明内容
为解决上述技术问题，本发明提供的技术方案为：一种飞碟飞行器，包括碟体、飞行桨、降落支架，所述碟体中部周向设有电磁轨道，所述电磁轨道为中部向内凹陷的“凹”字型轨道，所述电磁轨道内设置有与其配合的电磁悬浮车，所述飞行桨连接于电磁悬浮车外表面，并可在电磁悬浮车的带动下沿电磁轨道绕碟体转动，所述碟体两侧并位于飞行桨下部的位置上还设有涡轮喷气机支架，所述涡轮喷气机支架上连接有涡轮喷气机，所述碟体一侧的涡轮喷气机为竖向设置，另一侧为横向设置，所述降落支架设置于碟体底部，所述降落支架为折叠支架。
作为改进，所述飞行桨外部设有飞行桨保护罩，所述飞行桨外部设有飞行桨保护罩，所述飞行桨保护罩包括设置于飞行桨外部并与其处于同一水平面的环形保护支架，所述环形保护支架上下两端分别向碟体方向延伸设置的能覆盖飞行桨的上网体、下网体，所述上网体、下网体末端均与碟体连接。
作为改进，所述飞行桨包括设置于电磁悬浮车外部的环形飞行桨支架，所述环形飞行桨支架外部周向设有数个桨叶。
作为改进，所述桨叶为与水平面设有夹角的倾斜桨叶。
作为改进，所述碟体包括设有电磁轨道的中心舱体，所述中心舱体上部设有上推进装置放置舱体、控制中心放置舱体及驾驶装置放置舱，所述中心舱体下部设有下推进装置放置舱体以及为上推进装置放置舱体、控制中心放置舱体、驾驶装置放置舱、下推进装置放置舱体供电的供电装置放置舱体，所述驾驶装置放置舱顶部为可开合顶舱盖。
作为改进，所述驾驶装置放置舱内设有逃生弹射座椅。
作为改进，所述碟体底部设有翻转舱门，所述翻转舱门内侧面设有阶梯，所述碟体内设有从翻转舱门至驾驶装置放置舱的进出通道，所述进出通道内设有沿进出通道设置的竖向阶梯。
作为改进，所述上推进装置放置舱体、控制中心放置舱体外表面上铺设有太阳能电池板。
作为改进，所述可开合顶舱盖为透明舱盖。
作为改进，所述环形保护支架外侧还设有数个照明灯。
采用以上结构后，本发明具有如下优点：本申请飞行器可以作为一种新的飞行器，进行运输、旅行、勘探等活动；本申请飞行器起降不需要专用跑道，可以垂直起降，可以在空中飞行的同时，通过飞行桨保护罩下方的横向涡轮喷气机或上下两层推进装置室的方向控制推进装置，方便地转换方向。
附图说明
图1是本发明一种飞碟飞行器的结构示意图。
图2是本发明一种飞碟飞行器中飞行桨保护罩的结构示意图。
图3是本发明一种飞碟飞行器中电磁轨道的结构示意图。
图4是本发明一种飞碟飞行器中飞行桨的结构示意图。
图5是本发明一种飞碟飞行器中上下阶梯的结构示意图。
如图所示：1、碟体，1.1、中心舱体，1.2、上推进装置放置舱体，1.3、控制中心放置舱体，1.4、驾驶装置放置舱，1.5、下推进装置放置舱体，1.6、供电装置放置舱体，2、飞行桨，2.1、环形飞行桨支架，2.2、桨叶，3、降落支架，4、电磁轨道，5、电磁悬浮车，6、涡轮喷气机支架，7、涡轮喷气机，8、飞行桨保护罩，8.1、环形保护支架，8.2、上网体，8.3、下网体，9、翻转舱门，10、进出通道，11、上下阶梯，12、照明灯。
具体实施方式
结合附图，一种飞碟飞行器，其特征在于，包括碟体1、飞行桨2、降落支架3，所述碟体1中部周向设有电磁轨道4，所述电磁轨道4为中部向内凹陷的“凹”字型轨道，所述电磁轨道4内设置有与其配合的电磁悬浮车5，所述飞行桨2连接于电磁悬浮车5外表面，并可在电磁悬浮车5的带动下沿电磁轨道绕碟体1转动，所述碟体1两侧并位于飞行桨2下部的位置上还设有涡轮喷气机支架6，所述涡轮喷气机支架6上可转动连接有涡轮喷气机7，所述碟体1一侧的涡轮喷气机7为竖向设置，另一侧为横向设置，所述降落支架3设置于碟体1底部，所述降落支架3为折叠支架。
作为本实施例较佳实施方案的是，所述飞行桨2外部设有飞行桨保护罩8，所述飞行桨保护罩8包括设置于飞行桨2外部并与其处于同一水平面的环形保护支架8.1，所述环形保护支架8.1上下两端分别向碟体1方向延伸设置的能覆盖飞行桨2的上网体8.2、下网体8.3，所述上网体8.2、下网体8.3末端均与碟体1连接。飞行桨保护罩8的设置不影响空气流通，可防止空中漂浮物及鸟类进入旋翼叶片内。
作为本实施例较佳实施方案的是，所述飞行桨2包括设置于电磁悬浮车5外部的环形飞行桨支架2.1，所述环形飞行桨支架2.1外部周向设有数个桨叶2.2。
作为本实施例较佳实施方案的是，所述桨叶2.2为与水平面设有夹角的倾斜桨叶。
作为本实施例较佳实施方案的是，所述碟体1包括设有电磁轨道4的中心舱体1.1，所述中心舱体1.1上部设有上推进装置放置舱体1.2、控制中心放置舱体1.3及驾驶装置放置舱1.4，所述中心舱体1.1下部 设有下推进装置放置舱体1.5以及为上推进装置放置舱体1.2、控制中心放置舱体1.3、驾驶装置放置舱1.4、下推进装置放置舱体1.5供电的供电装置放置舱体1.6，所述驾驶装置放置舱1.4顶部为可开合顶舱盖。
作为本实施例较佳实施方案的是，所述电磁轨道4为中心凹进轨道，电磁悬浮车5镶嵌于电磁轨道4中心凹进部分，电磁悬浮车5与电磁轨道4的磁极为相斥磁极，保持电磁悬浮车5与电磁轨道4中间及上下不相接触，为悬浮状态，当启动电源后，利用电磁轨道4内部设置的电磁线圈牵引力，使电磁悬浮车5沿电磁轨道4绕碟体1旋转起来，带动电磁悬浮车5外围的一圈飞行桨2旋转起来，当转速达到一定速度，飞行桨2向上的作用力足够大，带动整个碟体1向上悬浮起来，然后用飞行浆保护罩下方的竖向涡轮喷气机将飞碟后部稍稍向上推起，使飞行桨由从上往下吸入空气，变为从前上方往后下方吸入空气，模仿直升机的推进方式向前推进，以此实现飞碟悬浮与飞行的目的，当飞碟启动，旋翼叶片旋转起来，其强大的离心力会使整个碟体跟着旋转起来，因此同时启动设置与飞行桨保护罩下方的横向涡轮喷气机来进行控制碟体稳定。
所述设置于飞行桨保护罩下方的横向涡轮喷气机，可通过提高和降低转速，来调整方向。
所述设置于碟体上下两层推进装置室的方向控制推进装置，可设置成左右交互工作，来实现方向调整，如：当向左转向时，启动右侧的方向控制推进装置，碟体可转向左侧。当向右转向时，可启动左侧的方向控制推进装置，碟体则转向右侧。也可以用于未来飞碟应用于外层空间时，在没有空气的环境下，可通过启用此推进装置来进行推进。可通过推进装置室的方向控制推进装置，来进行调整方向。
所述供电机房内的供电组可设置为电池组或核电组，供电装置放置舱体于碟体下部，在安装供电装置后可使飞碟保持重心向下，不至于倾斜或翻跟头；
作为本实施例较佳实施方案的是，所述驾驶装置放置舱1.4内设有逃生弹射座椅。
作为本实施例较佳实施方案的是，所述控制中心放置舱内部还设有为飞碟飞行器降落的大型降落伞和喷射装置，其出口连接于驾驶装置放置舱中心位置，当飞碟在空中飞行过程中出现故障或者断电时，同步自动顶舱盖打开，或直接爆破，然后喷射出大型降落伞给飞碟降落，可大大提高飞碟的安全性，如大型降落伞喷射失败，通过逃生弹射座椅连人带座椅一起弹出舱外，飞行员拉开身上穿戴的降落伞，扔掉座椅，进行降落，可以借用军用飞机的弹射方式，保证飞行员的安全和飞行员头部向上的弹射姿势，然后抛出降落伞。
作为本实施例较佳实施方案的是，所述碟体1底部设有翻转舱门9，所述翻转舱门9内侧面设有阶梯，所述碟体1内设有从翻转舱门9至驾驶装置放置舱1.4的进出通道10，所述进出通道10内设有沿进出通道10上下的简易上下阶梯11。
作为本实施例较佳实施方案的是，所述上推进装置放置舱体1.2、控制中心放置舱体1.3外表面上铺设有太阳能电池板。
作为本实施例较佳实施方案的是，所述可开合顶舱盖为透明舱盖。
作为本实施例较佳实施方案的是，所述环形保护支架8.1外侧还设有数个照明灯12，在夜晚可开启灯光，用于起飞和降落时照明与美化，另外飞碟的一端可设置大灯。
以本发明结构为基础，可作为一种新的飞行器，进行运输、旅行、勘探等活动；可作为航天飞行器使用；可作为飞碟仿真玩具等。
以上对本发明及其实施方式进行了描述，这种描述没有限制性，附图中所示的也只是本发明的实施方式之一，实际的结构并不局限于此。总而言之如果本领域的普通技术人员受其启示，在不脱离本发明创造宗旨的情况下，不经创造性的设计出与该技术方案相似的结构方式及实施例，均应属于本发明的保护范围。

Claims (10)

  1. 一种飞碟飞行器，其特征在于，包括碟体、飞行桨、降落支架，所述碟体中部周向设有电磁轨道，所述电磁轨道为中部向内凹陷的“凹”字型轨道，所述电磁轨道内设置有与其配合的电磁悬浮车，所述飞行桨连接于电磁悬浮车外表面，并可在电磁悬浮车的带动下沿电磁轨道绕碟体转动，所述碟体两侧并位于飞行桨下部的位置上还设有涡轮喷气机支架，所述涡轮喷气机支架上连接有涡轮喷气机，所述碟体一侧的涡轮喷气机为竖向设置，另一侧为横向设置，所述降落支架设置于碟体底部，所述降落支架为折叠支架。
  2. 根据权利要求1所述的一种飞碟飞行器，其特征在于，所述飞行桨外部设有飞行桨保护罩，所述飞行桨保护罩包括设置于飞行桨外部并与其处于同一水平面的环形保护支架，所述环形保护支架上下两端分别向碟体方向延伸设置的能覆盖飞行桨的上网体、下网体，所述上网体、下网体末端均与碟体连接。
  3. 根据权利要求2所述的一种飞碟飞行器，其特征在于，所述飞行桨包括设置于电磁悬浮车外部的环形飞行桨支架，所述环形飞行桨支架外部周向设有数个桨叶。
  4. 根据权利要求3所述的一种飞碟飞行器，其特征在于，所述桨叶为与水平面设有夹角的倾斜桨叶。
  5. 根据权利要求1所述的一种飞碟飞行器，其特征在于，所述碟体包括设有电磁轨道的中心舱体，所述中心舱体上部设有上推进装置放置舱体、控制中心放置舱体及驾驶装置放置舱，所述中心舱体下部设有下推进装置放置舱体以及为上推进装置放置舱体、控制中心放置舱体、驾驶装置放置舱、下推进装置放置舱体供电的供电装置放置舱体，所述驾驶装置放置舱顶部为可开合顶舱盖。
  6. 根据权利要求5所述的一种飞碟飞行器，其特征在于所述驾驶装置放置舱内设有逃生弹射座椅。
  7. 根据权利要求5所述的一种飞碟飞行器，其特征在于，所述碟体底部设有翻转舱门，所述翻转舱门内侧面设有阶梯，所述碟体内设有从翻转舱门至驾驶装置放置舱的进出通道，所述进出通道内设有沿进出通道设置的竖向阶梯。
  8. 根据权利要求5所述的一种飞碟飞行器，其特征在于，所述上推进装置放置舱体、控制中心放置舱体外表面上铺设有太阳能电池板。
  9. 根据权利要求5所述的一种飞碟飞行器，其特征在于，所述可开合顶舱盖为透明舱盖。
  10. 根据权利要求2所述的一种飞碟飞行器，其特征在于，所述环形保护支架外侧还设有数个照明灯。
PCT/CN2021/088338 2020-04-26 2021-04-20 一种飞碟飞行器 WO2021218703A1 (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE212021000318.4U DE212021000318U1 (de) 2020-04-26 2021-04-20 Fliegendes Untertassen-Luftfahrzeug

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN202010336463.0A CN111409825A (zh) 2020-04-26 2020-04-26 一种飞碟飞行器
CN202010336463.0 2020-04-26

Publications (1)

Publication Number Publication Date
WO2021218703A1 true WO2021218703A1 (zh) 2021-11-04

Family

ID=71488429

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2021/088338 WO2021218703A1 (zh) 2020-04-26 2021-04-20 一种飞碟飞行器

Country Status (6)

Country Link
US (1) US20210331797A1 (zh)
JP (1) JP3231509U (zh)
CN (1) CN111409825A (zh)
DE (1) DE212021000318U1 (zh)
RU (1) RU208389U1 (zh)
WO (1) WO2021218703A1 (zh)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111409825A (zh) * 2020-04-26 2020-07-14 耿起志 一种飞碟飞行器

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101693470A (zh) * 2009-10-30 2010-04-14 北京工业大学 一种磁悬浮电动力旋翼飞碟
CN102398678A (zh) * 2011-09-19 2012-04-04 张斌 飞碟
CN102556350A (zh) * 2012-02-10 2012-07-11 杜云鹏飞 太阳能电磁动力碟形航空器
CN106005412A (zh) * 2016-07-08 2016-10-12 夏建国 飞碟型垂直起降高速电磁飞机
US20200012296A1 (en) * 2019-08-27 2020-01-09 Intel Corporation Unmanned aerial vehicle landing area detection
CN111409825A (zh) * 2020-04-26 2020-07-14 耿起志 一种飞碟飞行器
CN212220551U (zh) * 2020-04-26 2020-12-25 耿起志 一种飞碟飞行器

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201176263Y (zh) * 2007-09-04 2009-01-07 刘新广 磁飞碟
FR2955831B1 (fr) * 2010-02-03 2012-02-17 Erick Pierre Raymond Bremont Dirigeable aeromaritime lenticulaire a geometrie variable a propulsion solaire electrique et turboreacteurs, equipe d'un convertisseur de poussee central par turbos helices contrarotatives
EA201100937A1 (ru) * 2011-05-23 2012-05-30 Владимир Федорович Полещук Летательный аппарат полещука
CN102642618A (zh) * 2012-04-17 2012-08-22 张斌 飞碟

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101693470A (zh) * 2009-10-30 2010-04-14 北京工业大学 一种磁悬浮电动力旋翼飞碟
CN102398678A (zh) * 2011-09-19 2012-04-04 张斌 飞碟
CN102556350A (zh) * 2012-02-10 2012-07-11 杜云鹏飞 太阳能电磁动力碟形航空器
CN106005412A (zh) * 2016-07-08 2016-10-12 夏建国 飞碟型垂直起降高速电磁飞机
US20200012296A1 (en) * 2019-08-27 2020-01-09 Intel Corporation Unmanned aerial vehicle landing area detection
CN111409825A (zh) * 2020-04-26 2020-07-14 耿起志 一种飞碟飞行器
CN212220551U (zh) * 2020-04-26 2020-12-25 耿起志 一种飞碟飞行器

Also Published As

Publication number Publication date
DE212021000318U1 (de) 2022-10-31
CN111409825A (zh) 2020-07-14
RU208389U1 (ru) 2021-12-16
US20210331797A1 (en) 2021-10-28
JP3231509U (ja) 2021-04-08

Similar Documents

Publication Publication Date Title
US6086016A (en) Gyro stabilized triple mode aircraft
US6698685B2 (en) Circular vertical take off and landing aircraft
JP4603222B2 (ja) 飛行機及び飛行機の操縦方法
US5351911A (en) Vertical takeoff and landing (VTOL) flying disc
US8181903B2 (en) Aircraft having the ability for hovering flight, fast forward flight, gliding flight, short take-off, short landing, vertical take-off and vertical landing
US6581872B2 (en) Circular vertical take off & landing aircraft
US5178344A (en) VTOL aircraft
US4014483A (en) Lighter-than-air craft
US20110180673A1 (en) Taking off and landing airplane using variable rotary wings
RU2617014C1 (ru) Летательный аппарат
US10597153B1 (en) Heliplane craft
US3582021A (en) Vertical takeoff and landing aircraft and method of operation
CN105711831A (zh) 垂直起降的固定翼无人机
WO2021218703A1 (zh) 一种飞碟飞行器
CN212220551U (zh) 一种飞碟飞行器
RU2422309C1 (ru) Комбинированный летательный аппарат
CN205554576U (zh) 一种多轴螺旋桨与旋翼组合飞行升力装置
US3469804A (en) Rotary and circular saucer-shaped airfoil aircraft
WO2009044998A1 (en) Taking off and landing airplane using variable rotary wings
CN106364665A (zh) 飞行动力系统及飞行器
CN105799927A (zh) 一种涵道环固定翼直升机
WO2023059209A1 (en) The method of obtaining lift and thrust for horizontal flight of vertical take-off and landing flying machine while maintaining the horizontal stability of the machine's flight and the machine to implement this method
WO2002070342A1 (en) Circular vertical take-off and landing aircraft
CN206691363U (zh) 一种能垂直起降的三角翼飞行器
CN206218208U (zh) 飞行动力系统及飞行器

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 21795536

Country of ref document: EP

Kind code of ref document: A1

122 Ep: pct application non-entry in european phase

Ref document number: 21795536

Country of ref document: EP

Kind code of ref document: A1