GB1427158A - Composite helicopter blade - Google Patents
Composite helicopter bladeInfo
- Publication number
- GB1427158A GB1427158A GB2565273A GB2565273A GB1427158A GB 1427158 A GB1427158 A GB 1427158A GB 2565273 A GB2565273 A GB 2565273A GB 2565273 A GB2565273 A GB 2565273A GB 1427158 A GB1427158 A GB 1427158A
- Authority
- GB
- United Kingdom
- Prior art keywords
- spar
- root
- bonding
- tip
- 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
- 239000002131 composite material Substances 0.000 title 1
- 239000000945 filler Substances 0.000 abstract 2
- 238000005299 abrasion Methods 0.000 abstract 1
- 238000010276 construction Methods 0.000 abstract 1
- 239000000463 material 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
- 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)
- Laminated Bodies (AREA)
- Wind Motors (AREA)
- Moulding By Coating Moulds (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US25833372A | 1972-05-31 | 1972-05-31 | |
| US25814772A | 1972-05-31 | 1972-05-31 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1427158A true GB1427158A (en) | 1976-03-10 |
Family
ID=26946445
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2565273A Expired GB1427158A (en) | 1972-05-31 | 1973-05-30 | Composite helicopter blade |
Country Status (6)
| Country | Link |
|---|---|
| JP (1) | JPS4943394A (https=) |
| AU (1) | AU5909073A (https=) |
| DE (1) | DE2327393A1 (https=) |
| FR (1) | FR2186380B1 (https=) |
| GB (1) | GB1427158A (https=) |
| IT (1) | IT988810B (https=) |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5074753A (en) * | 1989-10-16 | 1991-12-24 | Bell Helicopter Textron Inc. | Rotor blade |
| GB2266085A (en) * | 1992-04-14 | 1993-10-20 | Composite Tech Pty Ltd | Aerofoil construction. |
| US5868351A (en) * | 1996-05-23 | 1999-02-09 | Bell Helicopter Textron Inc. | Rotor blade stowing system |
| EP2376766A2 (en) * | 2008-12-12 | 2011-10-19 | Aviation Enterprises Limited | Rotor blades |
| US8061994B2 (en) | 2007-12-14 | 2011-11-22 | Eurocopter | Rotorcraft blade, a rotorcraft rotor provided with said blade, and a method of fabricating said blade |
| EP2599717A1 (fr) | 2011-12-01 | 2013-06-05 | Eurocopter | Pale de rotor |
| KR101455325B1 (ko) | 2011-12-01 | 2014-10-27 | 에어버스 헬리콥터스 | 로터 블레이드 |
| EP2842726A1 (en) * | 2013-08-30 | 2015-03-04 | Bell Helicopter Textron Inc. | Method of constructing a composite assembly and composite assembly |
| EP3501979A1 (fr) * | 2017-12-22 | 2019-06-26 | Airbus Helicopters | Enveloppes aerodynamiques epaisses pour cols de pales et carenages de manchons de pales d'un rotor d'un aeronef |
| CN114030604A (zh) * | 2021-11-19 | 2022-02-11 | 中国直升机设计研究所 | 一种复合材料缠绕的拉扭条组件及其成型方法 |
| CN115817810A (zh) * | 2022-11-24 | 2023-03-21 | 南京航空航天大学 | 具有承担集中载荷桨尖的复合材料桨叶 |
| US12031453B1 (en) | 2022-12-22 | 2024-07-09 | General Electric Company | Component with spar assembly for a turbine engine |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4096012A (en) * | 1976-08-30 | 1978-06-20 | The Boeing Company | Method of forming a spar layup for an aerodynamic rotor blade |
| IT1091214B (it) * | 1977-12-05 | 1985-07-06 | Fiat Spa | Pala per motori eolici |
| FR2427494A1 (fr) * | 1978-06-01 | 1979-12-28 | Neu Sa | Perfectionnement aux pales pour ventilateurs helicoides de tres grand diametre |
| DE3006088A1 (de) * | 1980-02-19 | 1981-08-20 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Rotor eines drehfluegelflugzeugs |
| DE3014347C2 (de) * | 1980-04-15 | 1983-05-26 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Verfahren zur Herstellung von schaumkerngestützen, faserverstärkten Kunststoff-Formkörpern wie Flügel, Rotorblätter etc. großer Längen-und Breitenausdehnung |
| IT1210605B (it) * | 1981-02-05 | 1989-09-14 | Agusta Aeronaut Costr | Metodo per la realizzazione di longheroni per pale di elicottero |
| DE3113079C2 (de) * | 1981-04-01 | 1985-11-21 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Aerodynamischer Groß-Flügel und Verfahren zu dessen Herstellung |
| FR2572788B1 (fr) * | 1984-11-08 | 1987-01-30 | Hexcel Genin Sa | Structure porteuse composite |
| FR2918347B1 (fr) * | 2007-07-02 | 2010-05-07 | Eurocopter France | Pale munie d'un longeron a enroulement horizontal et procede de fabrication d'un tel longeron |
-
1973
- 1973-05-29 DE DE19732327393 patent/DE2327393A1/de active Pending
- 1973-05-30 IT IT2483173A patent/IT988810B/it active
- 1973-05-30 FR FR7321159A patent/FR2186380B1/fr not_active Expired
- 1973-05-30 GB GB2565273A patent/GB1427158A/en not_active Expired
- 1973-05-31 JP JP6173273A patent/JPS4943394A/ja active Pending
- 1973-08-09 AU AU59090/73A patent/AU5909073A/en not_active Expired
Cited By (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5074753A (en) * | 1989-10-16 | 1991-12-24 | Bell Helicopter Textron Inc. | Rotor blade |
| GB2266085A (en) * | 1992-04-14 | 1993-10-20 | Composite Tech Pty Ltd | Aerofoil construction. |
| US5868351A (en) * | 1996-05-23 | 1999-02-09 | Bell Helicopter Textron Inc. | Rotor blade stowing system |
| US8061994B2 (en) | 2007-12-14 | 2011-11-22 | Eurocopter | Rotorcraft blade, a rotorcraft rotor provided with said blade, and a method of fabricating said blade |
| CN101456451B (zh) * | 2007-12-14 | 2012-05-23 | 尤洛考普特公司 | 旋翼机桨叶、设置有所述桨叶的旋翼机旋翼以及制造所述桨叶的方法 |
| EP2376766A2 (en) * | 2008-12-12 | 2011-10-19 | Aviation Enterprises Limited | Rotor blades |
| US9085986B2 (en) | 2011-12-01 | 2015-07-21 | Airbus Helicopters | Rotor blade |
| KR101455325B1 (ko) | 2011-12-01 | 2014-10-27 | 에어버스 헬리콥터스 | 로터 블레이드 |
| EP2599717A1 (fr) | 2011-12-01 | 2013-06-05 | Eurocopter | Pale de rotor |
| FR2983457A1 (fr) * | 2011-12-01 | 2013-06-07 | Eurocopter France | Pale de rotor |
| US10723438B2 (en) | 2013-08-30 | 2020-07-28 | Bell Helicopter Textron Inc. | System and methods of constructing composite assemblies |
| EP2842726A1 (en) * | 2013-08-30 | 2015-03-04 | Bell Helicopter Textron Inc. | Method of constructing a composite assembly and composite assembly |
| EP3330063A1 (en) * | 2013-08-30 | 2018-06-06 | Bell Helicopter Textron Inc. | Method of constructing composite assemblies |
| US10858090B2 (en) | 2013-08-30 | 2020-12-08 | Bell Textron Inc. | Systems and methods of constructing composite assemblies |
| FR3075757A1 (fr) * | 2017-12-22 | 2019-06-28 | Airbus Helicopters | Enveloppes aerodynamiques epaisses pour cols de pales et carenages de manchons de pales d'un rotor d'un aeronef |
| EP3501979A1 (fr) * | 2017-12-22 | 2019-06-26 | Airbus Helicopters | Enveloppes aerodynamiques epaisses pour cols de pales et carenages de manchons de pales d'un rotor d'un aeronef |
| US10858093B2 (en) | 2017-12-22 | 2020-12-08 | Airbus Helicopters | Thick airfoil shapes for blade necks and for blade cuff fairings for an aircraft rotor |
| CN114030604A (zh) * | 2021-11-19 | 2022-02-11 | 中国直升机设计研究所 | 一种复合材料缠绕的拉扭条组件及其成型方法 |
| CN114030604B (zh) * | 2021-11-19 | 2023-05-23 | 中国直升机设计研究所 | 一种复合材料缠绕的拉扭条组件及其成型方法 |
| CN115817810A (zh) * | 2022-11-24 | 2023-03-21 | 南京航空航天大学 | 具有承担集中载荷桨尖的复合材料桨叶 |
| CN115817810B (zh) * | 2022-11-24 | 2025-10-31 | 南京航空航天大学 | 具有承担集中载荷桨尖的复合材料桨叶 |
| US12031453B1 (en) | 2022-12-22 | 2024-07-09 | General Electric Company | Component with spar assembly for a turbine engine |
Also Published As
| Publication number | Publication date |
|---|---|
| IT988810B (it) | 1975-04-30 |
| FR2186380A1 (https=) | 1974-01-11 |
| DE2327393A1 (de) | 1973-12-13 |
| JPS4943394A (https=) | 1974-04-24 |
| AU5909073A (en) | 1975-02-13 |
| FR2186380B1 (https=) | 1977-09-02 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PCNP | Patent ceased through non-payment of renewal fee |