CA2320606C - Protective edge members for composite flexures - Google Patents
Protective edge members for composite flexures Download PDFInfo
- Publication number
- CA2320606C CA2320606C CA002320606A CA2320606A CA2320606C CA 2320606 C CA2320606 C CA 2320606C CA 002320606 A CA002320606 A CA 002320606A CA 2320606 A CA2320606 A CA 2320606A CA 2320606 C CA2320606 C CA 2320606C
- Authority
- CA
- Canada
- Prior art keywords
- composite
- yoke
- ply
- edge
- flexure
- 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 - Lifetime
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 68
- 230000001681 protective effect Effects 0.000 title abstract description 4
- 239000011152 fibreglass Substances 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 2
- 230000033001 locomotion Effects 0.000 description 23
- 230000032798 delamination Effects 0.000 description 12
- 238000005452 bending Methods 0.000 description 8
- 230000000694 effects Effects 0.000 description 5
- 238000005461 lubrication Methods 0.000 description 5
- 230000007704 transition Effects 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 230000003068 static effect Effects 0.000 description 4
- 238000012423 maintenance Methods 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 125000004122 cyclic group Chemical group 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000004224 protection Effects 0.000 description 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/33—Rotors having flexing arms
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49318—Repairing or disassembling
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49337—Composite blade
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24777—Edge feature
- Y10T428/24785—Edge feature including layer embodying mechanically interengaged strands, strand portions or strand-like strips [e.g., weave, knit, etc.]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Golf Clubs (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/407,691 US6375426B1 (en) | 1999-09-28 | 1999-09-28 | Protective edge members for composite flexures |
| US09/407,691 | 1999-09-28 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2320606A1 CA2320606A1 (en) | 2001-03-28 |
| CA2320606C true CA2320606C (en) | 2009-02-24 |
Family
ID=23613135
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002320606A Expired - Lifetime CA2320606C (en) | 1999-09-28 | 2000-09-26 | Protective edge members for composite flexures |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US6375426B1 (enExample) |
| EP (1) | EP1088754B1 (enExample) |
| JP (1) | JP2001122195A (enExample) |
| KR (1) | KR100726201B1 (enExample) |
| CA (1) | CA2320606C (enExample) |
| DE (2) | DE1088754T1 (enExample) |
Families Citing this family (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6708921B2 (en) * | 2001-04-20 | 2004-03-23 | Bell Helicopter Textron, Inc. | Composite flapping flexure |
| US6581365B1 (en) * | 2001-12-07 | 2003-06-24 | Harris Corporation | Controlling thermally induced beam twist |
| DE10348981B4 (de) * | 2003-10-22 | 2009-04-09 | Eurocopter Deutschland Gmbh | Rotor, insbesondere für ein Drehflugzeug |
| KR100600595B1 (ko) * | 2005-06-01 | 2006-07-13 | 동아전기부품 주식회사 | 프리히터용 방열부 |
| FR2893914B1 (fr) | 2005-11-29 | 2008-05-23 | Eurocopter France | Protection antichoc d'une piece mecanique. |
| CN102066197B (zh) * | 2008-04-21 | 2014-02-12 | 鲍里斯·安德烈耶夫·博罗维京 | 垂直起降旋翼机 |
| US10059438B2 (en) * | 2011-12-26 | 2018-08-28 | Textron Innovations Inc. | Hub assembly with grease lubricated roller bearing and tension-torsion strap |
| CN102795338B (zh) * | 2012-07-27 | 2014-10-08 | 北京卫星制造厂 | 一种微小型无人机碳纤维旋翼的制备方法 |
| EP2772430B1 (en) * | 2013-02-27 | 2016-06-29 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Partly cruciform flexbeam and method of manufacturing such a flexbeam |
| EP2783981B1 (en) | 2013-03-28 | 2017-03-15 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Bar of composite matrix material |
| US9499262B2 (en) | 2013-08-02 | 2016-11-22 | Bell Helicopter Textron Inc. | Composite flexure for tiltrotor rotor system |
| EP3038909B1 (en) * | 2013-08-28 | 2019-05-08 | Sikorsky Aircraft Corporation | Rotor hub for rotary wing aircraft |
| EP2883790B1 (en) | 2013-12-10 | 2017-11-22 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Beam for a rotorcraft rotor and rotorcraft rotor |
| EP2899121B1 (en) | 2014-01-22 | 2016-11-16 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Flexbeam unit for a bearingless or a hinge- and bearingless multi-blade rotor of a rotary wing aircraft |
| US11001375B2 (en) * | 2019-03-18 | 2021-05-11 | The Boeing Company | Structurally tunable cores |
| CN112550669B (zh) * | 2020-12-11 | 2023-06-27 | 中国直升机设计研究所 | 一种跷跷板式无轴承尾桨毂及直升机尾桨 |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4189283A (en) | 1978-07-12 | 1980-02-19 | The United States Of America As Represented By The Secretary Of The Navy | Rotor hub for a helicopter |
| US4293276A (en) * | 1978-10-27 | 1981-10-06 | Textron Inc. | Laminated composite rotor yoke |
| US4466774A (en) | 1982-08-30 | 1984-08-21 | United Technologies Corporation | Composite flexbeam joint |
| US4966802A (en) | 1985-05-10 | 1990-10-30 | The Boeing Company | Composites made of fiber reinforced resin elements joined by adhesive |
| US4898515A (en) | 1986-07-23 | 1990-02-06 | United Technologies Corporation | External wrap of composite flexbeam |
| US4746272A (en) * | 1986-07-23 | 1988-05-24 | United Technologies Corporation | Lobed composite flexbeam |
| US4818179A (en) | 1987-07-30 | 1989-04-04 | United Technologies Corporation | Composite helicopter rotor hub |
| CA2069125A1 (en) | 1991-07-01 | 1993-01-02 | Gary J. Jacaruso | Composite forming tool |
| TW244340B (enExample) | 1992-07-21 | 1995-04-01 | Akzo Nv | |
| US5431538A (en) | 1993-07-01 | 1995-07-11 | United Technologies Corporation | Hybrid composite flexbeam for a helicopter bearingless main rotor assembly |
| US5690474A (en) * | 1996-07-18 | 1997-11-25 | Sikorsky Aircraft Corporation | Optimized composite flexbeam for helicopter tail rotors |
| US5820344A (en) * | 1997-06-27 | 1998-10-13 | Mcdonnell Douglas Corporation | Contoured flexure strap for helicopter rotor system |
-
1999
- 1999-09-28 US US09/407,691 patent/US6375426B1/en not_active Expired - Lifetime
-
2000
- 2000-09-26 CA CA002320606A patent/CA2320606C/en not_active Expired - Lifetime
- 2000-09-27 EP EP00203352A patent/EP1088754B1/en not_active Expired - Lifetime
- 2000-09-27 DE DE1088754T patent/DE1088754T1/de active Pending
- 2000-09-27 JP JP2000293303A patent/JP2001122195A/ja active Pending
- 2000-09-27 KR KR1020000056687A patent/KR100726201B1/ko not_active Expired - Lifetime
- 2000-09-27 DE DE60001784T patent/DE60001784T2/de not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| EP1088754A2 (en) | 2001-04-04 |
| US6375426B1 (en) | 2002-04-23 |
| KR100726201B1 (ko) | 2007-06-11 |
| DE1088754T1 (de) | 2001-10-11 |
| EP1088754A3 (en) | 2002-04-03 |
| DE60001784D1 (de) | 2003-04-30 |
| EP1088754B1 (en) | 2003-03-26 |
| KR20010050665A (ko) | 2001-06-15 |
| DE60001784T2 (de) | 2003-12-04 |
| JP2001122195A (ja) | 2001-05-08 |
| CA2320606A1 (en) | 2001-03-28 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2320606C (en) | Protective edge members for composite flexures | |
| JP2547289B2 (ja) | ヘリコプター用ローター装置のピッチハウジング構造体 | |
| US4051289A (en) | Composite airfoil construction | |
| US4293276A (en) | Laminated composite rotor yoke | |
| US5431538A (en) | Hybrid composite flexbeam for a helicopter bearingless main rotor assembly | |
| US4971641A (en) | Method of making counterrotating aircraft propeller blades | |
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| KR20000057691A (ko) | 헬리콥터 주회전 날개용 복합 팁 캡 조립체 | |
| US6708921B2 (en) | Composite flapping flexure | |
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| CA1095664A (en) | Composite airfoil construction | |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKEX | Expiry |
Effective date: 20200928 |