ES479237A1 - Perfeccionamientos en la formacion de palas de rotor princi-pal para helicopteros. - Google Patents
Perfeccionamientos en la formacion de palas de rotor princi-pal para helicopteros.Info
- Publication number
- ES479237A1 ES479237A1 ES479237A ES479237A ES479237A1 ES 479237 A1 ES479237 A1 ES 479237A1 ES 479237 A ES479237 A ES 479237A ES 479237 A ES479237 A ES 479237A ES 479237 A1 ES479237 A1 ES 479237A1
- Authority
- ES
- Spain
- Prior art keywords
- spar
- nose
- nose spar
- trailing edges
- blade
- 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.)
- Expired
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
- B64C27/473—Constructional features
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Perfeccionamientos en la formación de palas de rotor principal para helicópteros, caracterizados porque comprenden: formar por rodillos un larguero en forma de C; formar por rodillos un canal de cierre, sujetar el canal de cierre dentro de los cantos posteriores del larguero, formar por rodillos una tira protectora configurada para comprender una parte delantera del larguero, formar por rodillos un bloque de ataque y dejar confinado el bloque de ataque dentro de la tira protectora sujeto a la parte delantera del larguero, y unir duplicadores del cuerpo a las superficies exteriores del larguero por detrás de la tira protectora, quedando medio superpuestos los duplicadores por revestimiento de la pala
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/893,050 US4275994A (en) | 1978-04-03 | 1978-04-03 | Roll formed blade structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES479237A1 true ES479237A1 (es) | 1979-12-01 |
Family
ID=25400942
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES479237A Expired ES479237A1 (es) | 1978-04-03 | 1979-04-03 | Perfeccionamientos en la formacion de palas de rotor princi-pal para helicopteros. |
Country Status (12)
| Country | Link |
|---|---|
| US (1) | US4275994A (es) |
| JP (1) | JPS54131298A (es) |
| AR (1) | AR224118A1 (es) |
| AU (1) | AU521499B2 (es) |
| BR (1) | BR7901815A (es) |
| CA (1) | CA1101817A (es) |
| DE (1) | DE2900834A1 (es) |
| ES (1) | ES479237A1 (es) |
| FR (1) | FR2421798A1 (es) |
| GB (1) | GB2017615B (es) |
| IL (1) | IL56979A (es) |
| IT (1) | IT1114058B (es) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AU576968B2 (en) * | 1985-08-01 | 1988-09-08 | Vergola Pty Ltd | Louvre blade forming machine |
| SU1539865A1 (ru) * | 1986-07-14 | 1990-01-30 | Предприятие П/Я В-8803 | Электрический разъем с нулевым усилием стыковки |
| US5782607A (en) * | 1996-12-11 | 1998-07-21 | United Technologies Corporation | Replaceable ceramic blade insert |
| DE102007013291B4 (de) * | 2007-03-16 | 2010-04-15 | Eurocopter Deutschland Gmbh | Rotorblatt für einen lagerlosen Rotor eines Drehflügelflugzeugs |
| JP4402160B1 (ja) * | 2009-03-02 | 2010-01-20 | 山田 正明 | 模型回転翼航空機の回転翼、及びその回転翼の製造方法 |
| US7976275B2 (en) * | 2010-08-30 | 2011-07-12 | General Electric Company | Wind turbine rotor blade assembly having an access window and related methods |
| US8057189B2 (en) * | 2010-12-15 | 2011-11-15 | General Electric Company | Wind turbine blade with modular leading edge |
| US20130199934A1 (en) | 2012-02-06 | 2013-08-08 | United Technologies Corporation | Electroformed sheath |
| BR112015019303A2 (pt) * | 2013-03-01 | 2017-07-18 | Gen Electric | conjuntos de aerofólio e aerofólio |
| EP3374262B1 (en) * | 2015-11-09 | 2021-02-24 | Sikorsky Aircraft Corporation | Rotor blade structures |
| CN105775124A (zh) * | 2016-03-08 | 2016-07-20 | 哈尔滨飞机工业集团有限责任公司 | 直升机主桨叶动平衡特殊调整方法 |
| FR3070371B1 (fr) * | 2017-08-31 | 2022-09-23 | Airbus Helicopters | Pale, rotor muni de cette pale et aeronef muni de ce rotor |
| US11046420B2 (en) * | 2019-10-23 | 2021-06-29 | The Boeing Company | Trailing edge flap having a waffle grid interior structure |
| US11725524B2 (en) | 2021-03-26 | 2023-08-15 | General Electric Company | Engine airfoil metal edge |
| US11767607B1 (en) | 2022-07-13 | 2023-09-26 | General Electric Company | Method of depositing a metal layer on a component |
Family Cites Families (28)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2596818A (en) * | 1947-05-08 | 1952-05-13 | Piasecki Helicopter Corp | Rotor blade |
| US2574980A (en) * | 1947-06-05 | 1951-11-13 | Piasecki Helicopter Corp | Rotary wing blade |
| FR1009798A (fr) * | 1948-06-25 | 1952-06-03 | Const Aeronautiques Du Ct Soc | Perfectionnements à la construction des pales de voilures tournantes |
| FR1113837A (fr) * | 1953-10-21 | 1956-04-04 | Parsons Corp | Voilure rotative sustentatrice, notamment pour hélicoptères |
| US2884078A (en) * | 1953-10-21 | 1959-04-28 | Parsons Corp | Rotor blade structure having spanwise reinforcing members |
| US3002567A (en) * | 1953-10-21 | 1961-10-03 | Parsons Corp | Spar for sustaining rotors |
| US2884077A (en) * | 1953-10-21 | 1959-04-28 | Parsons Corp | Rotor blade having a gap-bonded aft structure and method of fabricating same |
| GB744437A (en) * | 1953-10-29 | 1956-02-08 | Bristol Aeroplane Co Ltd | Improvements in or relating to rotor blades for helicopters and like rotary wing aircraft |
| US2965530A (en) * | 1954-08-18 | 1960-12-20 | Parsons Corp | Method for joining dissimilar materials |
| US2828531A (en) * | 1955-06-21 | 1958-04-01 | Cyril Bath Co | Method of making a helicopter blade |
| US2863513A (en) * | 1955-12-12 | 1958-12-09 | Bell Aircraft Corp | Helicopter rotor blade |
| US3200477A (en) * | 1962-11-21 | 1965-08-17 | Enstrom Corp | Helicopter tail rotor structure and method of construction |
| US3217807A (en) * | 1964-08-28 | 1965-11-16 | Bell Aerospace Corp | Rotor blade |
| GB1150123A (en) * | 1967-02-08 | 1969-04-30 | Westland Aircraft Ltd | Improvements in or relating to the Construction of Rotor Blades for Rotary Wing Aircraft |
| GB1214858A (en) * | 1968-05-20 | 1970-12-09 | Westland Aircraft Ltd | Improvements in or relating to the construction of rotor blades for rotary wing aircraft |
| US3528753A (en) * | 1968-06-14 | 1970-09-15 | United Aircraft Corp | Helicopter blade with non-homogeneous structural spar |
| US3674379A (en) * | 1969-01-30 | 1972-07-04 | Siai Marchetti Spa | Helicopter rotor blade |
| AU459383B2 (en) * | 1971-05-17 | 1975-03-27 | Textron Inc. | Advanced geometry main rotor blade |
| US3829240A (en) * | 1971-05-17 | 1974-08-13 | Textron Inc | Advanced geometry main rotor blade |
| US3799700A (en) * | 1971-05-17 | 1974-03-26 | Textron Inc | Main rotor blade construction |
| US3813186A (en) * | 1972-10-10 | 1974-05-28 | Textron Inc | Rotor blade shear reinforcement |
| FR2234130B1 (es) * | 1973-05-14 | 1976-04-30 | Kamov Nikolai | |
| JPS5016298A (es) * | 1973-05-30 | 1975-02-20 | ||
| US4022546A (en) * | 1974-01-03 | 1977-05-10 | Textron, Inc. | Helicopter rotor blade |
| US3874820A (en) * | 1974-04-08 | 1975-04-01 | United Aircraft Corp | Hingeless in-plane rotor blade design |
| GB1537380A (en) * | 1976-05-06 | 1978-12-29 | Westland Aircraft Ltd | Fibre-reinforced plastics structures |
| US4095322A (en) * | 1976-08-30 | 1978-06-20 | The Boeing Company | Method of fabricating a composite aerodynamic rotorblade assembly |
| US4150920A (en) * | 1977-12-02 | 1979-04-24 | The United States Of America As Represented By The Secretary Of The Army | Rotor blade tipweight assembly |
-
1978
- 1978-04-03 US US05/893,050 patent/US4275994A/en not_active Expired - Lifetime
-
1979
- 1979-01-11 AU AU43299/79A patent/AU521499B2/en not_active Ceased
- 1979-01-11 DE DE19792900834 patent/DE2900834A1/de active Granted
- 1979-01-26 AR AR275312A patent/AR224118A1/es active
- 1979-01-30 CA CA320,492A patent/CA1101817A/en not_active Expired
- 1979-01-30 JP JP885379A patent/JPS54131298A/ja active Pending
- 1979-02-01 IT IT7947859A patent/IT1114058B/it active
- 1979-02-14 FR FR7903697A patent/FR2421798A1/fr active Granted
- 1979-02-15 GB GB7905431A patent/GB2017615B/en not_active Expired
- 1979-03-26 BR BR7901815A patent/BR7901815A/pt unknown
- 1979-03-29 IL IL56979A patent/IL56979A/xx unknown
- 1979-04-03 ES ES479237A patent/ES479237A1/es not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPS54131298A (en) | 1979-10-12 |
| AR224118A1 (es) | 1981-10-30 |
| IL56979A (en) | 1983-10-31 |
| IT7947859A0 (it) | 1979-02-01 |
| AU4329979A (en) | 1979-10-18 |
| GB2017615B (en) | 1982-04-21 |
| GB2017615A (en) | 1979-10-10 |
| CA1101817A (en) | 1981-05-26 |
| FR2421798A1 (fr) | 1979-11-02 |
| DE2900834A1 (de) | 1979-10-04 |
| FR2421798B1 (es) | 1983-10-21 |
| IT1114058B (it) | 1986-01-27 |
| DE2900834C2 (es) | 1988-05-19 |
| BR7901815A (pt) | 1979-11-20 |
| US4275994A (en) | 1981-06-30 |
| AU521499B2 (en) | 1982-04-08 |
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