CN111655575A - 螺旋桨、动力组件及飞行器 - Google Patents
螺旋桨、动力组件及飞行器 Download PDFInfo
- Publication number
- CN111655575A CN111655575A CN201880088055.9A CN201880088055A CN111655575A CN 111655575 A CN111655575 A CN 111655575A CN 201880088055 A CN201880088055 A CN 201880088055A CN 111655575 A CN111655575 A CN 111655575A
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- CN
- China
- Prior art keywords
- hub
- blade
- propeller
- center
- attack
- 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
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- QNRATNLHPGXHMA-XZHTYLCXSA-N (r)-(6-ethoxyquinolin-4-yl)-[(2s,4s,5r)-5-ethyl-1-azabicyclo[2.2.2]octan-2-yl]methanol;hydrochloride Chemical compound Cl.C([C@H]([C@H](C1)CC)C2)CN1[C@@H]2[C@H](O)C1=CC=NC2=CC=C(OCC)C=C21 QNRATNLHPGXHMA-XZHTYLCXSA-N 0.000 description 1
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- 238000012986 modification Methods 0.000 description 1
- 238000011056 performance test Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Images
Classifications
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- 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
- B64C11/02—Hub construction
-
- 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
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
一种螺旋桨(100),其中,在距离桨毂(10)的中心为螺旋桨(100)的半径的44.0%处,桨叶(20)的攻角为18.62°±2.5°;在距离桨毂(10)的中心为螺旋桨(100)的半径的52.0%处,桨叶(20)的攻角为17.58°±2.5°;在距离桨毂(10)的中心为螺旋桨(100)的半径的68.0%处,桨叶(20)的攻角为15.05°±2.5°;在距离桨毂(10)的中心为螺旋桨(100)的半径的76.0%处,桨叶(20)的攻角为13.54°±2.5°;还涉及一种动力组件及一种飞行器。采用桨叶(20)翼型渐变的螺旋桨(100)能使得螺旋桨(100)在沿着桨叶的展向的每一段都处于最佳工作段,减少了桨叶(20)在工作时产生的噪声,使得飞行器(1000)在悬停时更安静,提高了用户体验,同时,还减少了空气阻力,提高拉力和效率,增加飞行器(1000)的续航距离以提高飞行器(1000)的飞行性能。
Description
PCT国内申请,说明书已公开。
Claims (27)
- PCT国内申请,权利要求书已公开。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2018209960734 | 2018-06-26 | ||
CN201820996073.4U CN208439418U (zh) | 2018-06-26 | 2018-06-26 | 螺旋桨、动力组件及飞行器 |
PCT/CN2018/106088 WO2020000686A1 (zh) | 2018-06-26 | 2018-09-18 | 螺旋桨、动力组件及飞行器 |
Publications (1)
Publication Number | Publication Date |
---|---|
CN111655575A true CN111655575A (zh) | 2020-09-11 |
Family
ID=65090750
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201820996073.4U Expired - Fee Related CN208439418U (zh) | 2018-06-26 | 2018-06-26 | 螺旋桨、动力组件及飞行器 |
CN201880088055.9A Pending CN111655575A (zh) | 2018-06-26 | 2018-09-18 | 螺旋桨、动力组件及飞行器 |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201820996073.4U Expired - Fee Related CN208439418U (zh) | 2018-06-26 | 2018-06-26 | 螺旋桨、动力组件及飞行器 |
Country Status (2)
Country | Link |
---|---|
CN (2) | CN208439418U (zh) |
WO (1) | WO2020000686A1 (zh) |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20120237354A1 (en) * | 2010-12-02 | 2012-09-20 | Alan Brocklehurst | Aerofoil |
CN104139849A (zh) * | 2014-08-07 | 2014-11-12 | 西北工业大学 | 一种具有提高高空桨效率的桨梢小翼及高空桨 |
CN204606209U (zh) * | 2015-04-20 | 2015-09-02 | 中国直升机设计研究所 | 一种低噪声桨尖 |
CN105923155A (zh) * | 2016-06-08 | 2016-09-07 | 南京航空航天大学 | 一种用于旋翼飞行器的低噪声桨叶 |
CN106428551A (zh) * | 2016-09-22 | 2017-02-22 | 上海未来伙伴机器人有限公司 | 多旋翼桨叶装置 |
CN207045700U (zh) * | 2017-07-28 | 2018-02-27 | 深圳市大疆创新科技有限公司 | 用于无人机的螺旋桨、动力组件及无人机 |
CN108163192A (zh) * | 2017-12-29 | 2018-06-15 | 江苏方阔航空科技有限公司 | 一种高效低噪旋翼 |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2712717A1 (de) * | 1977-03-23 | 1978-09-28 | Ver Flugtechnische Werke | Ueberkritisches tragfluegelprofil |
JP3472799B2 (ja) * | 2000-02-29 | 2003-12-02 | 防衛庁技術研究本部長 | ブレード用翼型 |
CN205366054U (zh) * | 2016-01-28 | 2016-07-06 | 深圳市大疆创新科技有限公司 | 螺旋桨、动力组件及飞行器 |
CN206155775U (zh) * | 2016-11-11 | 2017-05-10 | 深圳市大疆创新科技有限公司 | 螺旋桨、动力组件及飞行器 |
CN206954495U (zh) * | 2017-05-12 | 2018-02-02 | 深圳市蔚蓝动力有限公司 | 新型螺旋桨 |
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2018
- 2018-06-26 CN CN201820996073.4U patent/CN208439418U/zh not_active Expired - Fee Related
- 2018-09-18 WO PCT/CN2018/106088 patent/WO2020000686A1/zh active Application Filing
- 2018-09-18 CN CN201880088055.9A patent/CN111655575A/zh active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20120237354A1 (en) * | 2010-12-02 | 2012-09-20 | Alan Brocklehurst | Aerofoil |
CN104139849A (zh) * | 2014-08-07 | 2014-11-12 | 西北工业大学 | 一种具有提高高空桨效率的桨梢小翼及高空桨 |
CN204606209U (zh) * | 2015-04-20 | 2015-09-02 | 中国直升机设计研究所 | 一种低噪声桨尖 |
CN105923155A (zh) * | 2016-06-08 | 2016-09-07 | 南京航空航天大学 | 一种用于旋翼飞行器的低噪声桨叶 |
CN106428551A (zh) * | 2016-09-22 | 2017-02-22 | 上海未来伙伴机器人有限公司 | 多旋翼桨叶装置 |
CN207045700U (zh) * | 2017-07-28 | 2018-02-27 | 深圳市大疆创新科技有限公司 | 用于无人机的螺旋桨、动力组件及无人机 |
CN108163192A (zh) * | 2017-12-29 | 2018-06-15 | 江苏方阔航空科技有限公司 | 一种高效低噪旋翼 |
Also Published As
Publication number | Publication date |
---|---|
CN208439418U (zh) | 2019-01-29 |
WO2020000686A1 (zh) | 2020-01-02 |
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PB01 | Publication | ||
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WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20200911 |