FR2348105A1 - Pale pour rotor d'helicoptere - Google Patents
Pale pour rotor d'helicoptereInfo
- Publication number
- FR2348105A1 FR2348105A1 FR7708501A FR7708501A FR2348105A1 FR 2348105 A1 FR2348105 A1 FR 2348105A1 FR 7708501 A FR7708501 A FR 7708501A FR 7708501 A FR7708501 A FR 7708501A FR 2348105 A1 FR2348105 A1 FR 2348105A1
- Authority
- FR
- France
- Prior art keywords
- blade
- helicopter rotor
- helicopter
- rotor
- 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
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/02—Formulas of curves
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/675,664 US4028003A (en) | 1976-04-12 | 1976-04-12 | Torsionally compliant helicopter rotor blade with improved stability and performance characteristics |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2348105A1 true FR2348105A1 (fr) | 1977-11-10 |
Family
ID=24711483
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7708501A Pending FR2348105A1 (fr) | 1976-04-12 | 1977-03-22 | Pale pour rotor d'helicoptere |
Country Status (9)
Country | Link |
---|---|
US (1) | US4028003A (fr) |
JP (1) | JPS52124697A (fr) |
BR (1) | BR7702255A (fr) |
CA (1) | CA1078357A (fr) |
DE (1) | DE2711507A1 (fr) |
FR (1) | FR2348105A1 (fr) |
GB (1) | GB1527835A (fr) |
IL (1) | IL51704A (fr) |
IT (1) | IT1076141B (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2397328A1 (fr) * | 1977-07-13 | 1979-02-09 | United Technologies Corp | Pales et rotors d'helicopteres ameliores |
FR2413264A1 (fr) * | 1978-01-03 | 1979-07-27 | Secr Defence Brit | Voilure portante pour aerodyne et aerodyne equipe d'une telle voilure |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES525921A0 (es) * | 1983-09-26 | 1984-08-01 | Pilar Banolas De Ayala M | Perfeccionamientos en helices de sustentacion para aeronaves |
US4655685A (en) * | 1985-12-16 | 1987-04-07 | United Technologies Corporation | Helicopter main rotor blade having a short span slot near the tip end |
US4792280A (en) * | 1987-04-27 | 1988-12-20 | United Technologies Corporation | Helicopter rotor flexbeam |
US5137228A (en) * | 1990-05-07 | 1992-08-11 | Vaughen Jack F | Rotary wing with torsionally flexible blades |
US5597138A (en) * | 1991-09-30 | 1997-01-28 | Arlton; Paul E. | Yaw control and stabilization system for helicopters |
JPH09254894A (ja) * | 1996-03-26 | 1997-09-30 | Commuter Herikoputa Senshin Gijutsu Kenkyusho:Kk | フラップ付ヘリコプタブレードおよびこれを用いたロータ制御装置 |
US5749540A (en) * | 1996-07-26 | 1998-05-12 | Arlton; Paul E. | System for controlling and automatically stabilizing the rotational motion of a rotary wing aircraft |
US6059532A (en) * | 1997-10-24 | 2000-05-09 | Alliedsignal Inc. | Axial flow turbo-machine fan blade having shifted tip center of gravity axis |
PL2123557T3 (pl) * | 2008-05-22 | 2011-10-31 | Agustawestland Spa | Łopatka wirnika ogonowego równoważącego moment obrotowy śmigłowca |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB613288A (en) * | 1945-06-21 | 1948-11-24 | Rotary Res Corp | Rotor blade |
FR2153253A1 (fr) * | 1971-09-22 | 1973-05-04 | United Aircraft Corp | |
FR2231565A1 (fr) * | 1973-06-04 | 1974-12-27 | United Aircraft Corp |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2754918A (en) * | 1950-09-21 | 1956-07-17 | United Aircraft Corp | Weighted blade for rotary wing aircraft |
US3237697A (en) * | 1963-02-11 | 1966-03-01 | Boeing Co | Helicopter rotor blade |
US3232349A (en) * | 1964-12-02 | 1966-02-01 | Enstrom Corp | Rotor system utilizing centrifugal deflection of non-radial blades |
US3310117A (en) * | 1966-04-08 | 1967-03-21 | Parsons Corp | Helicopter spar having integral mass and stiffness control provisions |
US3484174A (en) * | 1968-04-08 | 1969-12-16 | Kaman Corp | Rotary wing system |
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 |
GB1262704A (en) * | 1968-08-10 | 1972-02-02 | Messerschmitt Boelkow Blohm | Helicopter rotor blade |
US3561702A (en) * | 1968-11-01 | 1971-02-09 | Edward B Jones | Swept wing variable pitch sailplane |
FR2041747A1 (fr) * | 1969-05-20 | 1971-02-05 | Sud Aviation | |
US3926536A (en) * | 1970-10-15 | 1975-12-16 | Westland Aircraft Ltd | Semi-rigid rotor systems for rotary wing aircraft |
US3728045A (en) * | 1971-09-22 | 1973-04-17 | United Aircraft Corp | Helicopter blade |
US3822105A (en) * | 1971-09-22 | 1974-07-02 | United Aircraft Corp | Helicopter blade |
US3721507A (en) * | 1971-09-22 | 1973-03-20 | United Aircraft Corp | Blade for high speed helicopter |
US3874820A (en) * | 1974-04-08 | 1975-04-01 | United Aircraft Corp | Hingeless in-plane rotor blade design |
US3999886A (en) * | 1974-10-10 | 1976-12-28 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Hingeless helicopter rotor with improved stability |
-
1976
- 1976-04-12 US US05/675,664 patent/US4028003A/en not_active Expired - Lifetime
-
1977
- 1977-01-26 CA CA270,512A patent/CA1078357A/fr not_active Expired
- 1977-03-16 DE DE19772711507 patent/DE2711507A1/de active Granted
- 1977-03-21 IL IL51704A patent/IL51704A/xx unknown
- 1977-03-22 FR FR7708501A patent/FR2348105A1/fr active Pending
- 1977-03-29 GB GB13232/77A patent/GB1527835A/en not_active Expired
- 1977-04-08 IT IT22279/77A patent/IT1076141B/it active
- 1977-04-11 BR BR7702255A patent/BR7702255A/pt unknown
- 1977-04-12 JP JP4195877A patent/JPS52124697A/ja active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB613288A (en) * | 1945-06-21 | 1948-11-24 | Rotary Res Corp | Rotor blade |
FR2153253A1 (fr) * | 1971-09-22 | 1973-05-04 | United Aircraft Corp | |
FR2231565A1 (fr) * | 1973-06-04 | 1974-12-27 | United Aircraft Corp |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2397328A1 (fr) * | 1977-07-13 | 1979-02-09 | United Technologies Corp | Pales et rotors d'helicopteres ameliores |
FR2413264A1 (fr) * | 1978-01-03 | 1979-07-27 | Secr Defence Brit | Voilure portante pour aerodyne et aerodyne equipe d'une telle voilure |
Also Published As
Publication number | Publication date |
---|---|
DE2711507C2 (fr) | 1987-07-30 |
CA1078357A (fr) | 1980-05-27 |
BR7702255A (pt) | 1978-01-17 |
GB1527835A (en) | 1978-10-11 |
DE2711507A1 (de) | 1977-10-20 |
JPS52124697A (en) | 1977-10-19 |
IT1076141B (it) | 1985-04-24 |
US4028003A (en) | 1977-06-07 |
IL51704A (en) | 1981-07-31 |
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