FR2748718B1 - Pale a vulnerabilite reduite pour rotors de giravions, et son procede de fabrication - Google Patents
Pale a vulnerabilite reduite pour rotors de giravions, et son procede de fabricationInfo
- Publication number
- FR2748718B1 FR2748718B1 FR8514926A FR8514926A FR2748718B1 FR 2748718 B1 FR2748718 B1 FR 2748718B1 FR 8514926 A FR8514926 A FR 8514926A FR 8514926 A FR8514926 A FR 8514926A FR 2748718 B1 FR2748718 B1 FR 2748718B1
- Authority
- FR
- France
- Prior art keywords
- giravions
- rotors
- blade
- manufacturing
- reduced vulnerability
- 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
- 238000004519 manufacturing process Methods 0.000 title 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)
- Moulding By Coating Moulds (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8514926A FR2748718B1 (fr) | 1985-10-09 | 1985-10-09 | Pale a vulnerabilite reduite pour rotors de giravions, et son procede de fabrication |
IT8621803A IT8621803A0 (it) | 1985-10-09 | 1986-09-24 | Pala a ridotta vulnerabilita' per rotori di aerogiri e suo procedimento di fabbricazione.! |
GB8623981A GB2315723B (en) | 1985-10-09 | 1986-10-06 | A low-vulnerability helicopter rotor blade |
CA000520143A CA1340478C (fr) | 1985-10-09 | 1986-10-09 | Pale a vulnerabilite reduite pour rotors de giravions et son procede de fabrication |
DE3634510A DE3634510C1 (de) | 1985-10-09 | 1986-10-09 | Rotorblatt mit verringerter Verletzbarkeit für Drehflügler-Rotoren und Verfahren zur Herstellung desselben |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8514926A FR2748718B1 (fr) | 1985-10-09 | 1985-10-09 | Pale a vulnerabilite reduite pour rotors de giravions, et son procede de fabrication |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2748718A1 FR2748718A1 (fr) | 1997-11-21 |
FR2748718B1 true FR2748718B1 (fr) | 1998-12-24 |
Family
ID=9323654
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8514926A Expired - Fee Related FR2748718B1 (fr) | 1985-10-09 | 1985-10-09 | Pale a vulnerabilite reduite pour rotors de giravions, et son procede de fabrication |
Country Status (5)
Country | Link |
---|---|
CA (1) | CA1340478C (fr) |
DE (1) | DE3634510C1 (fr) |
FR (1) | FR2748718B1 (fr) |
GB (1) | GB2315723B (fr) |
IT (1) | IT8621803A0 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8282040B1 (en) | 2009-04-30 | 2012-10-09 | Lockheed Martin Corporation | Composite aircraft wing |
US11015461B2 (en) * | 2017-12-21 | 2021-05-25 | General Electric Company | Composite hollow blade and a method of forming the composite hollow blade |
FR3091724B1 (fr) | 2019-01-15 | 2021-01-22 | Safran Aircraft Engines | Aube ou Pale d'hélice composite pour aéronef intégrant une mousse de conformation |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1275279B (de) * | 1965-10-06 | 1968-08-14 | Boelkow Gmbh | Verfahren zum Herstellen eines Verbundbauteils aus glasfaserverstaerktem Kunststoff |
US4083656A (en) * | 1975-03-21 | 1978-04-11 | Textron, Inc. | Composite rotor blade |
US4316701A (en) * | 1976-08-30 | 1982-02-23 | The Boeing Company | Composite aerodynamic rotor blade assembly |
US4316700A (en) * | 1979-04-03 | 1982-02-23 | Schramm Burford J | Unitary, bonded-together helicopter rotorblade |
BR8406224A (pt) * | 1983-12-19 | 1985-10-01 | Goodyear Tire & Rubber | Mangueira flexivel e processo para sua fabricacao |
-
1985
- 1985-10-09 FR FR8514926A patent/FR2748718B1/fr not_active Expired - Fee Related
-
1986
- 1986-09-24 IT IT8621803A patent/IT8621803A0/it unknown
- 1986-10-06 GB GB8623981A patent/GB2315723B/en not_active Expired - Fee Related
- 1986-10-09 CA CA000520143A patent/CA1340478C/fr not_active Expired - Fee Related
- 1986-10-09 DE DE3634510A patent/DE3634510C1/de not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2748718A1 (fr) | 1997-11-21 |
DE3634510C1 (de) | 1998-02-26 |
GB2315723A (en) | 1998-02-11 |
CA1340478C (fr) | 1999-04-06 |
GB8623981D0 (en) | 1997-11-19 |
GB2315723B (en) | 1998-06-24 |
IT8621803A0 (it) | 1986-09-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
TP | Transmission of property | ||
ST | Notification of lapse |