DE3200830C2 - Verfahren zur Herstellung von Holmen für Hubschrauber-Rotorblätter - Google Patents
Verfahren zur Herstellung von Holmen für Hubschrauber-RotorblätterInfo
- Publication number
- DE3200830C2 DE3200830C2 DE3200830A DE3200830A DE3200830C2 DE 3200830 C2 DE3200830 C2 DE 3200830C2 DE 3200830 A DE3200830 A DE 3200830A DE 3200830 A DE3200830 A DE 3200830A DE 3200830 C2 DE3200830 C2 DE 3200830C2
- Authority
- DE
- Germany
- Prior art keywords
- template
- mold
- cross member
- conveyor
- band
- 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 - Fee Related
Links
- 238000000034 method Methods 0.000 title claims description 10
- 238000004519 manufacturing process Methods 0.000 claims description 5
- 238000005520 cutting process Methods 0.000 claims description 4
- 238000000151 deposition Methods 0.000 claims 1
- 238000000465 moulding Methods 0.000 description 5
- 102000004315 Forkhead Transcription Factors Human genes 0.000 description 2
- 108090000852 Forkhead Transcription Factors Proteins 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 210000001520 comb Anatomy 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 229920003002 synthetic resin Polymers 0.000 description 1
- 239000000057 synthetic resin Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0025—Producing blades or the like, e.g. blades for turbines, propellers, or wings
-
- 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
-
- 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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
-
- 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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/12—Surface bonding means and/or assembly means with cutting, punching, piercing, severing or tearing
-
- 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
- Y10T29/49332—Propeller making
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Decoration Of Textiles (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IT8167152A IT1210605B (it) | 1981-02-05 | 1981-02-05 | Metodo per la realizzazione di longheroni per pale di elicottero |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DE3200830A1 DE3200830A1 (de) | 1982-09-09 |
| DE3200830C2 true DE3200830C2 (de) | 1994-04-28 |
Family
ID=11300016
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE3200830A Expired - Fee Related DE3200830C2 (de) | 1981-02-05 | 1982-01-14 | Verfahren zur Herstellung von Holmen für Hubschrauber-Rotorblätter |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US4407688A (enExample) |
| JP (1) | JPS57155199A (enExample) |
| DE (1) | DE3200830C2 (enExample) |
| FR (1) | FR2498979A1 (enExample) |
| GB (1) | GB2092543B (enExample) |
| IT (1) | IT1210605B (enExample) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2583259B2 (ja) * | 1988-01-08 | 1997-02-19 | 富士重工業株式会社 | ヘリコプタ用フレックスビーム |
| US5430937A (en) * | 1994-07-15 | 1995-07-11 | United Technologies Corporation | Apparatus and methods for fabricating a helicopter main rotor blade |
| US5832605A (en) * | 1997-04-16 | 1998-11-10 | Sikorsky Aircraft Corporation | Methods for fabricating a helicopter main rotor blade |
| US5836062A (en) * | 1997-04-16 | 1998-11-17 | Sikorsky Aircraft Corporation | Apparatus for assembling a helicopter main rotor blade subassembly |
| US5862576A (en) * | 1997-04-16 | 1999-01-26 | Sikorsky Aircraft Corporation | Apparatus for installing a leading-edge sheath onto a helicopter main rotor blade subassembly |
| US6717712B2 (en) | 2000-01-06 | 2004-04-06 | Donnelly Corporation | Exterior mirror plano-auxiliary reflective element assembly |
| US8012291B2 (en) * | 2006-12-11 | 2011-09-06 | The Boeing Company | Backing film removal system and method for fiber placement machine |
| DK2524134T3 (da) | 2010-01-14 | 2014-08-11 | Neptco Inc | Rotorvingekomponenter til en vindmølle og fremgangsmåder til fremstilling deraf |
| US10137542B2 (en) | 2010-01-14 | 2018-11-27 | Senvion Gmbh | Wind turbine rotor blade components and machine for making same |
| EP2949579B1 (en) * | 2014-05-28 | 2018-05-23 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Flexbeam unit with at least one twisted flexbeam element |
| FR3023747B1 (fr) * | 2014-07-18 | 2017-03-10 | Airbus Helicopters | Procede de fabrication d'un longeron d'une pale, et de fabrication d'une pale |
| US11066188B2 (en) | 2018-08-10 | 2021-07-20 | Sikorsky Aircraft Corporation | Method and apparatus for locating and forming fastener holes in a replacement tip section of a rotor blade |
| US11242140B2 (en) | 2018-08-10 | 2022-02-08 | Sikorsky Aircraft Corporation | Method of removal and replacement of a tip section of a rotor blade |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3057767A (en) * | 1958-04-01 | 1962-10-09 | Poly Ind Inc | Method of making compressor blades |
| FR1443155A (fr) * | 1965-03-24 | 1966-06-24 | Sud Aviation | Perfectionnements apportés aux pales d'hélicoptère et à leurs procédés et appareillages de fabrication |
| US3775219A (en) * | 1971-04-05 | 1973-11-27 | Goldsworthy Eng Inc | Composite-tape placement head |
| DE2327393A1 (de) * | 1972-05-31 | 1973-12-13 | United Aircraft Corp | Zusammengesetztes hubschrauber-rotorblatt |
| US3962506A (en) * | 1974-04-29 | 1976-06-08 | Fiber Science, Inc. | Multi-chambered cellular structure and method for manufacture |
| US4120610A (en) * | 1974-05-16 | 1978-10-17 | Textron, Inc. | Helicopter blade structure |
| US3943020A (en) * | 1974-12-05 | 1976-03-09 | Fiber Science, Inc. | Filament wound blade and method for manufacturing same |
| GB1560829A (en) * | 1975-08-26 | 1980-02-13 | Hawker Siddeley Dynamics Ltd | Manufacture of propeller blades |
| US4096012A (en) * | 1976-08-30 | 1978-06-20 | The Boeing Company | Method of forming a spar layup for an aerodynamic rotor blade |
| US4133711A (en) * | 1977-07-11 | 1979-01-09 | Grumman Aerospace Corporation | Automated integrated composite lamination system |
-
1981
- 1981-02-05 IT IT8167152A patent/IT1210605B/it active
-
1982
- 1982-01-06 US US06/337,443 patent/US4407688A/en not_active Expired - Lifetime
- 1982-01-07 GB GB8200456A patent/GB2092543B/en not_active Expired
- 1982-01-14 DE DE3200830A patent/DE3200830C2/de not_active Expired - Fee Related
- 1982-01-28 FR FR8201366A patent/FR2498979A1/fr active Granted
- 1982-02-05 JP JP57016497A patent/JPS57155199A/ja active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| US4407688A (en) | 1983-10-04 |
| JPS57155199A (en) | 1982-09-25 |
| IT1210605B (it) | 1989-09-14 |
| FR2498979B1 (enExample) | 1985-05-03 |
| GB2092543A (en) | 1982-08-18 |
| JPH0336720B2 (enExample) | 1991-06-03 |
| GB2092543B (en) | 1984-06-06 |
| IT8167152A0 (it) | 1981-02-05 |
| FR2498979A1 (fr) | 1982-08-06 |
| DE3200830A1 (de) | 1982-09-09 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 8110 | Request for examination paragraph 44 | ||
| 8127 | New person/name/address of the applicant |
Owner name: AGUSTA S.P.A., CASCINA COSTA DI SAMARATE, VARESE, |
|
| 8128 | New person/name/address of the agent |
Representative=s name: ZENZ, J., DIPL.-ING., 4300 ESSEN HELBER, F., DIPL. |
|
| D2 | Grant after examination | ||
| 8364 | No opposition during term of opposition | ||
| 8327 | Change in the person/name/address of the patent owner |
Owner name: AGUSTA S.P.A., SAMARATE, IT |
|
| 8339 | Ceased/non-payment of the annual fee |