CN108263597A - 盘式螺旋桨 - Google Patents
盘式螺旋桨 Download PDFInfo
- Publication number
- CN108263597A CN108263597A CN201810285664.5A CN201810285664A CN108263597A CN 108263597 A CN108263597 A CN 108263597A CN 201810285664 A CN201810285664 A CN 201810285664A CN 108263597 A CN108263597 A CN 108263597A
- Authority
- CN
- China
- Prior art keywords
- air
- flow
- disc
- type screw
- energy consumption
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
- B64C11/20—Constructional features
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
本申请涉及一种盘式螺旋桨,一种通过弯曲叶片和倾斜的凸起肋道,使高压气流对弯曲叶片形成的反推力和倾斜凸起肋道对气流产生的离心力来完成助力现象,形成小马拉大车原理降低能耗。
Description
图1是本研发的原理。主气道1,用于螺旋桨旋转压迫气流通道。2方向气道,用于气流通过动力舱的接收和改变方向来稳定机身和控制方向。3动力舱,用于储存发动机.燃料和接收方向气流,还有客舱和盘式螺旋桨的链接.4客舱,用于驾驶和载客。5链接轴,用于客舱.动力舱的链接和控制盘式螺旋桨的角度,使机身前进或后退。6叶片正面图,用于角度旋转压迫空气。7气道正面图。8气道侧面图。9弯曲叶片,用于出气口的高压气流对弯曲叶片形成的反推力使叶片加速旋转,形成助力现象。10叶片。11凸起肋道正面图,用于肋道倾斜角度和旋转角度形成直线运动,倾斜的肋道使上下气流向外排放,减少页片面的气流摩擦,使气流形成离心力向外排放,在叶片的高速旋转下利用气流的离心力形成助力现象。12凸起肋道横截面。
通过弯曲叶片和倾斜的凸起肋道,使高压气流对弯曲叶片形成的反推力和倾斜凸起肋道对气流产生的离心力来完成助力现象,形成小马拉大车原理降低能耗。
Claims (3)
1.使用倾斜的带肋风道对气流向外输出,通过旋转使加压的气流产生空气的离心力,助于螺旋桨旋转,降低能耗。
2.使用弯曲叶面,让高压气流对弯曲叶面施行反推力,助于螺旋桨旋转,降低能耗。
3.利用螺旋桨的气流分隔和动力舱接收气流的方向改变来控制机身稳定和方向。
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810285664.5A CN108263597A (zh) | 2018-03-23 | 2018-03-23 | 盘式螺旋桨 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810285664.5A CN108263597A (zh) | 2018-03-23 | 2018-03-23 | 盘式螺旋桨 |
Publications (1)
Publication Number | Publication Date |
---|---|
CN108263597A true CN108263597A (zh) | 2018-07-10 |
Family
ID=62777476
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201810285664.5A Pending CN108263597A (zh) | 2018-03-23 | 2018-03-23 | 盘式螺旋桨 |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN108263597A (zh) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2277372Y (zh) * | 1996-03-14 | 1998-04-01 | 吴季忠 | 离心式低空飞行器 |
CN102233951A (zh) * | 2010-04-28 | 2011-11-09 | 鄂雨松 | 飞碟发动机 |
CN102367064A (zh) * | 2011-05-26 | 2012-03-07 | 郑霞 | 盘式螺旋桨 |
US20160023754A1 (en) * | 2014-07-08 | 2016-01-28 | Lilium GmbH | Vertical take-off aircraft |
WO2016170419A2 (en) * | 2015-04-24 | 2016-10-27 | KREITMAYER MCKENZIE, Janja | Air vessel |
-
2018
- 2018-03-23 CN CN201810285664.5A patent/CN108263597A/zh active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2277372Y (zh) * | 1996-03-14 | 1998-04-01 | 吴季忠 | 离心式低空飞行器 |
CN102233951A (zh) * | 2010-04-28 | 2011-11-09 | 鄂雨松 | 飞碟发动机 |
CN102367064A (zh) * | 2011-05-26 | 2012-03-07 | 郑霞 | 盘式螺旋桨 |
US20160023754A1 (en) * | 2014-07-08 | 2016-01-28 | Lilium GmbH | Vertical take-off aircraft |
WO2016170419A2 (en) * | 2015-04-24 | 2016-10-27 | KREITMAYER MCKENZIE, Janja | Air vessel |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US10934011B2 (en) | Fluidic propulsive system and thrust and lift generator for aerial vehicles | |
US6669137B1 (en) | Air vehicle having rotor/scissors wing | |
US11987352B2 (en) | Fluid systems that include a co-flow jet | |
EP2252796A1 (de) | Kreisflügel - aktinischer fluidantrieb (af) | |
US20240150026A1 (en) | Fluidic propulsive system | |
US2885160A (en) | Circulatory jet airfoils | |
US20170037779A1 (en) | Aircraft boundary layer removal with auxilliary power unit suction | |
CN108263597A (zh) | 盘式螺旋桨 | |
US10577086B2 (en) | High efficiency stall proof airfoil and means of control | |
US20220009617A1 (en) | Vertical take off and landing aircraft with fluidic propulsion system | |
WO2021242463A9 (en) | Vertical take off and landing aircraft with fluidic propulsion system | |
CN113226925A (zh) | 自适应的竖直起降推进系统 | |
US20220009627A1 (en) | Vertical take off and landing aircraft with fluidic propulsion system | |
CN105000178A (zh) | 节能喉管无舵式直升机 | |
WO2023021095A1 (en) | A system for lift, propulsion and control of an airborne craft | |
Catana et al. | Global Study of the Performance of a Propeller with a Variable Pitch and a Variable Diameter | |
Razvan-Marius et al. | Global Study of the Performance of a Propeller with a Variable Pitch and a Variable Diameter. | |
WO2011146021A1 (en) | Self-powered yaw control and anti-spin device for fixed wing aircraft | |
CN107499493A (zh) | 一种飞行器 | |
Schmidt | Propeller simulation with PropSim |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180710 |
|
WD01 | Invention patent application deemed withdrawn after publication |