ATE522438T1 - Rotorschaufel aus einem faserverstärkten verbundstoffmaterial - Google Patents
Rotorschaufel aus einem faserverstärkten verbundstoffmaterialInfo
- Publication number
- ATE522438T1 ATE522438T1 AT09400020T AT09400020T ATE522438T1 AT E522438 T1 ATE522438 T1 AT E522438T1 AT 09400020 T AT09400020 T AT 09400020T AT 09400020 T AT09400020 T AT 09400020T AT E522438 T1 ATE522438 T1 AT E522438T1
- Authority
- AT
- Austria
- Prior art keywords
- blade
- section
- reinforced composite
- rotor
- rotor blade
- Prior art date
Links
- 239000000463 material Substances 0.000 title abstract 2
- 239000003733 fiber-reinforced composite Substances 0.000 title 1
- 230000008878 coupling Effects 0.000 abstract 2
- 238000010168 coupling process Methods 0.000 abstract 2
- 238000005859 coupling reaction Methods 0.000 abstract 2
- 239000002131 composite material Substances 0.000 abstract 1
- 239000000835 fiber Substances 0.000 abstract 1
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
-
- 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
- B64C27/48—Root attachment to rotor head
-
- 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
- B64C2027/4733—Rotor blades substantially made from particular materials
- B64C2027/4736—Rotor blades substantially made from particular materials from composite materials
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP09400020A EP2246260B1 (de) | 2009-04-29 | 2009-04-29 | Rotorschaufel aus einem faserverstärkten Verbundstoffmaterial |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE522438T1 true ATE522438T1 (de) | 2011-09-15 |
Family
ID=41326097
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT09400020T ATE522438T1 (de) | 2009-04-29 | 2009-04-29 | Rotorschaufel aus einem faserverstärkten verbundstoffmaterial |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US8926280B2 (de) |
| EP (1) | EP2246260B1 (de) |
| AT (1) | ATE522438T1 (de) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8511928B2 (en) * | 2011-07-25 | 2013-08-20 | GM Global Technology Operations LLC | Error-proof tube connection |
| FR2991289B1 (fr) * | 2012-06-04 | 2015-03-27 | Etienne Jean Rampal | Dispositif d'attache rapide a jeux reduits des pales sur rotors d'aeronefs ou eoliennes |
| CN103895865A (zh) * | 2012-12-25 | 2014-07-02 | 中国直升机设计研究所 | 一种新型复合材料桨尖结构 |
| US9682773B2 (en) * | 2013-06-25 | 2017-06-20 | The Boeing Company | Systems and methods for blade attachment |
| US20170043859A1 (en) * | 2015-08-12 | 2017-02-16 | Gulfstream Aerospace Corporation | Trailing edge components, aircraft structures including trailing edge components and methods for manufacturing trailing edge components |
| US11919627B2 (en) * | 2022-08-04 | 2024-03-05 | Lockheed Martin Corporation | Commonly manufactured rotor blade |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4299538A (en) | 1978-12-06 | 1981-11-10 | United Technologies Corporation | Cross beam rotor |
| DE3244725C1 (de) | 1982-12-03 | 1984-03-01 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Rotorblatt aus Faserverbundkunststoff |
| FR2616409B1 (fr) * | 1987-06-09 | 1989-09-15 | Aerospatiale | Pale en materiaux composites et son procede de fabrication |
| CA2042532C (en) * | 1990-05-30 | 2002-03-12 | Francis E. Byrnes | Spar-to-hub joint for a flexbeam helicopter rotor |
| IL102867A (en) * | 1991-08-28 | 1998-02-08 | United Technologies Corp | Bearingless main motor assembly torque tube and method for fabricating same |
| CA2198717C (en) * | 1994-08-31 | 2005-03-15 | William C. Reinfelder | Fiber reinforced composite spar for a rotary wing aircraft and method of manufacture thereof |
| FR2740379B1 (fr) * | 1995-10-30 | 1998-01-02 | Eurocopter France | Procede de fabrication d'une pale en materiau composite pour rotor d'helicoptere, et pale pouvant etre obtenue par un tel procede |
| FR2740380B1 (fr) * | 1995-10-30 | 1998-01-02 | Eurocopter France | Procede de fabrication d'une pale a pas variable en materiau composite pour rotor d'helicoptere |
| US5738494A (en) * | 1996-07-18 | 1998-04-14 | Sikorsky Aircraft Corporation | Optimized composite flexbeam for helicopter rotors |
| US5810285A (en) * | 1996-12-20 | 1998-09-22 | Sikorsky Aircraft Corporation | Drive shaft casing for a ducted fan anti-torque device |
| US7665969B2 (en) * | 2005-01-24 | 2010-02-23 | Bell Helicopter Textron Inc. | Assembly for providing flexure to blade system |
-
2009
- 2009-04-29 AT AT09400020T patent/ATE522438T1/de not_active IP Right Cessation
- 2009-04-29 EP EP09400020A patent/EP2246260B1/de active Active
-
2010
- 2010-04-05 US US12/753,927 patent/US8926280B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| EP2246260B1 (de) | 2011-08-31 |
| US8926280B2 (en) | 2015-01-06 |
| EP2246260A1 (de) | 2010-11-03 |
| US20100278655A1 (en) | 2010-11-04 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |