MX2018006942A - Pala de rotor de autogiro. - Google Patents

Pala de rotor de autogiro.

Info

Publication number
MX2018006942A
MX2018006942A MX2018006942A MX2018006942A MX2018006942A MX 2018006942 A MX2018006942 A MX 2018006942A MX 2018006942 A MX2018006942 A MX 2018006942A MX 2018006942 A MX2018006942 A MX 2018006942A MX 2018006942 A MX2018006942 A MX 2018006942A
Authority
MX
Mexico
Prior art keywords
region
profile
rotor blade
blade
autogyro rotor
Prior art date
Application number
MX2018006942A
Other languages
English (en)
Inventor
Fraundorfer Christoph
ZÖEBISCH Andre
Original Assignee
Fraundorfer Christoph
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 Fraundorfer Christoph filed Critical Fraundorfer Christoph
Publication of MX2018006942A publication Critical patent/MX2018006942A/es

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/467—Aerodynamic features
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/02—Gyroplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/473—Constructional features

Abstract

La presente invención se relaciona con una pala de rotor de autogiro para la generación de sustentación mediante auto-rotación, comprendiendo una región de perfil interior (9) que tiene en el lado de la raíz un primer perfil (21c), una región de perfil principal (10) en el lado de punta que tiene un segundo perfil (21e) diferente del primer perfil (21c) y una curva de profundidad de perfil (22) que disminuye monótonamente en la dirección longitudinal de la pala de rotor de autogiro (1) de la región de la raíz de pala (2) hacia la punta de pala (3). De acuerdo a la invención, la pala de rotor de autogiro (1) tiene una torsión mostrando una curva de torsión (23) que disminuye monótonamente de la región de la raíz de pala (2) hacia la punta de pala (3), la curva de torsión (23) teniendo una gradiente variable en la región de perfil interior (9) y/o en la región de perfil principal (10), de tal manera que la curva de torsión (23) está arqueada en forma cóncava en la región mencionada (9, 10).
MX2018006942A 2015-12-10 2016-12-02 Pala de rotor de autogiro. MX2018006942A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102015121502.0A DE102015121502A1 (de) 2015-12-10 2015-12-10 Tragschrauberrotorblatt zur autorotatorischen Auftriebserzeugung
PCT/EP2016/079520 WO2017097669A1 (de) 2015-12-10 2016-12-02 Tragschrauberrotorblatt

Publications (1)

Publication Number Publication Date
MX2018006942A true MX2018006942A (es) 2018-11-29

Family

ID=57542980

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2018006942A MX2018006942A (es) 2015-12-10 2016-12-02 Pala de rotor de autogiro.

Country Status (16)

Country Link
US (1) US11338913B2 (es)
EP (1) EP3386854B1 (es)
JP (1) JP6899841B2 (es)
CN (1) CN108698687B (es)
AU (1) AU2016365585B2 (es)
BR (1) BR112018011610B1 (es)
CA (1) CA3007866A1 (es)
DE (1) DE102015121502A1 (es)
ES (1) ES2807750T3 (es)
IL (1) IL259885B2 (es)
MX (1) MX2018006942A (es)
PH (1) PH12018501230A1 (es)
PL (1) PL3386854T3 (es)
RU (1) RU2729115C2 (es)
WO (1) WO2017097669A1 (es)
ZA (1) ZA201803848B (es)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109229364B (zh) * 2018-10-23 2019-06-11 西北工业大学 应用于高速直升机旋翼反流区的类椭圆翼型
CN112429217A (zh) * 2020-11-26 2021-03-02 广东国士健科技发展有限公司 一种双层旋翼结构的飞行器

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE506701C (de) * 1930-09-08 Cierva Autogiro Co Ltd Flugzeug mit frei umlaufenden, vom Fahrtwind angetriebenen Fluegeln
DE502860C (de) * 1928-10-27 1930-07-19 Cierva Autogiro Co Ltd Flugzeug mit frei umlaufenden Fluegeln
GB452366A (en) 1935-01-16 1936-08-17 Cierva Juan De La Improvements in and relating to aircraft with autorotative wings
US2247034A (en) * 1938-12-22 1941-06-24 Autogiro Co Of America Aircraft sustaining rotor
US2272439A (en) * 1939-12-16 1942-02-10 Autogiro Co Of America Aircraft sustaining rotor blade
US2477113A (en) * 1942-02-19 1949-07-26 Autogiro Co Of America Rotor blade for rotative winged aircraft
US2447113A (en) 1947-05-05 1948-08-17 Nat Cylinder Gas Co Holding mechanism for welding stud ferrules
US2917255A (en) * 1958-08-01 1959-12-15 William Hunter A Boyd Self-regulating rotochute
FR1369600A (fr) * 1963-07-23 1964-08-14 Electric Auto Lite Co Hélice, notamment pour avions à décollage et atterrissage verticaux
CA988906A (en) * 1973-06-04 1976-05-11 United Aircraft Corporation Helicopter blade
ES8406336A1 (es) * 1983-09-26 1984-08-01 Pilar Banolas De Ayala M Perfeccionamientos en helices de sustentacion para aeronaves
FR2689852B1 (fr) * 1992-04-09 1994-06-17 Eurocopter France Pale pour voilure tournante d'aeronef, a extremite en fleche.
US5727754A (en) * 1995-08-31 1998-03-17 Cartercopters, L.L.C. Gyroplane
US6641365B2 (en) 1998-02-20 2003-11-04 Abraham E. Karem Optimum speed tilt rotor
JP4358435B2 (ja) 1998-02-20 2009-11-04 イー． カーレム，エイブラハム 最適速度ロータ
US6497385B1 (en) * 2000-11-08 2002-12-24 Continuum Dynamics, Inc. Rotor blade with optimized twist distribution
US7252479B2 (en) 2005-05-31 2007-08-07 Sikorsky Aircraft Corporation Rotor blade for a high speed rotary-wing aircraft
US8128376B2 (en) * 2005-08-15 2012-03-06 Abe Karem High performance outboard section for rotor blades
US7857598B2 (en) * 2006-06-26 2010-12-28 Aerovel Corporation Variable-twist rotor blade controlled by hub pitch angle and rotational speed
US8403255B2 (en) * 2009-08-14 2013-03-26 Frederick W. Piasecki Compound aircraft with autorotation
RU97111U1 (ru) * 2010-03-31 2010-08-27 Юрий Петрович Андреев Лопасть
US8862310B2 (en) 2012-06-06 2014-10-14 Simmonds Precision Products, Inc. Determining rotorcraft collective adjustment during ground test

Also Published As

Publication number Publication date
CA3007866A1 (en) 2017-06-15
WO2017097669A1 (de) 2017-06-15
CN108698687B (zh) 2021-09-24
PH12018501230B1 (en) 2019-02-04
RU2018123993A (ru) 2020-01-10
ES2807750T3 (es) 2021-02-24
DE102015121502A1 (de) 2017-06-14
PH12018501230A1 (en) 2019-02-04
BR112018011610A8 (pt) 2022-11-01
US20190152594A1 (en) 2019-05-23
US11338913B2 (en) 2022-05-24
IL259885B (en) 2022-12-01
RU2018123993A3 (es) 2020-03-06
IL259885A (en) 2018-07-31
EP3386854B1 (de) 2020-05-27
JP6899841B2 (ja) 2021-07-07
PL3386854T3 (pl) 2020-11-02
RU2729115C2 (ru) 2020-08-04
JP2019500278A (ja) 2019-01-10
AU2016365585B2 (en) 2021-05-27
CN108698687A (zh) 2018-10-23
AU2016365585A1 (en) 2018-07-05
BR112018011610B1 (pt) 2023-01-17
BR112018011610A2 (pt) 2018-11-27
ZA201803848B (en) 2022-12-21
IL259885B2 (en) 2023-04-01
EP3386854A1 (de) 2018-10-17

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