FR2374109A1 - Structures de surface d'aeronefs - Google Patents
Structures de surface d'aeronefsInfo
- Publication number
- FR2374109A1 FR2374109A1 FR7738049A FR7738049A FR2374109A1 FR 2374109 A1 FR2374109 A1 FR 2374109A1 FR 7738049 A FR7738049 A FR 7738049A FR 7738049 A FR7738049 A FR 7738049A FR 2374109 A1 FR2374109 A1 FR 2374109A1
- Authority
- FR
- France
- Prior art keywords
- super
- surface region
- surface structures
- aircraft surface
- alloy
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/38—Constructions adapted to reduce effects of aerodynamic or other external heating
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
L'invention concerne un procédé et une couche protectrice pour une région de surface d'un aéronef. Selon l'invention, on part d'une feuille ou des feuilles d'alliage super-plastique que l'on applique sur la région de surface à protéger, en moulant la ou les feuilles d'alliage super-plastique à une température où l'alliage présente ses propriétés super-plastiques, de manière à suivre les contours de surface de la région de surface à protéger et on fixe la couche protectrice d'alliage super-plastique ainsi formée sur ladite région de surface.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB52941/76A GB1593378A (en) | 1976-12-17 | 1976-12-17 | Aircraft surface structure |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2374109A1 true FR2374109A1 (fr) | 1978-07-13 |
FR2374109B1 FR2374109B1 (fr) | 1982-04-02 |
Family
ID=10465925
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7738049A Granted FR2374109A1 (fr) | 1976-12-17 | 1977-12-16 | Structures de surface d'aeronefs |
Country Status (10)
Country | Link |
---|---|
JP (1) | JPS5378599A (fr) |
BR (1) | BR7708394A (fr) |
CA (1) | CA1094526A (fr) |
DE (1) | DE2756423A1 (fr) |
FR (1) | FR2374109A1 (fr) |
GB (1) | GB1593378A (fr) |
IN (1) | IN149367B (fr) |
IT (1) | IT1088448B (fr) |
NL (1) | NL187567C (fr) |
SE (1) | SE437004B (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5399215A (en) * | 1992-08-19 | 1995-03-21 | Societe Hispano-Suiza | Method of manufacturing assemblies composed of two bonded parts |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB8609355D0 (en) * | 1986-04-17 | 1986-09-17 | Westland Plc | Erosion shields for aerofoil surfaces |
GB0913061D0 (en) | 2009-07-28 | 2009-09-02 | Rolls Royce Plc | A method of manufacturing a reinforcing edge for a turbo machine aerofoil |
US11964782B2 (en) | 2022-07-11 | 2024-04-23 | Wing Aviation Llc | Formed-metal sheet airframe for UAVS |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2959229A (en) * | 1957-10-01 | 1960-11-08 | United Aircraft Corp | Nickel plated propeller blade |
US3065940A (en) * | 1956-06-22 | 1962-11-27 | Emil L Eckstein | Aircraft outer surface covering |
US3712566A (en) * | 1971-02-25 | 1973-01-23 | Us Navy | Supersonic vehicle control surface having a thermally protective coating |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1108081B (de) * | 1955-01-20 | 1961-05-31 | Sud Aviation | Vorrichtung zur Herstellung eines Drehfluegels |
DE2153434B2 (de) * | 1971-10-27 | 1972-11-09 | Licentia Patent Verwaltungs GmbH, 6000 Frankfurt | Befestigung von erosionsschutzkanten an flugzeugprofilen |
-
1976
- 1976-12-17 GB GB52941/76A patent/GB1593378A/en not_active Expired
-
1977
- 1977-12-08 IN IN1704/CAL/77A patent/IN149367B/en unknown
- 1977-12-13 IT IT30637/77A patent/IT1088448B/it active
- 1977-12-15 SE SE7714234A patent/SE437004B/sv not_active IP Right Cessation
- 1977-12-15 NL NLAANVRAGE7713936,A patent/NL187567C/xx not_active IP Right Cessation
- 1977-12-16 FR FR7738049A patent/FR2374109A1/fr active Granted
- 1977-12-16 CA CA293,260A patent/CA1094526A/fr not_active Expired
- 1977-12-16 BR BR7708394A patent/BR7708394A/pt unknown
- 1977-12-17 JP JP15122377A patent/JPS5378599A/ja active Granted
- 1977-12-17 DE DE19772756423 patent/DE2756423A1/de active Granted
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3065940A (en) * | 1956-06-22 | 1962-11-27 | Emil L Eckstein | Aircraft outer surface covering |
US2959229A (en) * | 1957-10-01 | 1960-11-08 | United Aircraft Corp | Nickel plated propeller blade |
US3712566A (en) * | 1971-02-25 | 1973-01-23 | Us Navy | Supersonic vehicle control surface having a thermally protective coating |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5399215A (en) * | 1992-08-19 | 1995-03-21 | Societe Hispano-Suiza | Method of manufacturing assemblies composed of two bonded parts |
Also Published As
Publication number | Publication date |
---|---|
NL187567C (nl) | 1991-11-18 |
NL7713936A (nl) | 1978-06-20 |
FR2374109B1 (fr) | 1982-04-02 |
GB1593378A (en) | 1981-07-15 |
JPS6158359B2 (fr) | 1986-12-11 |
JPS5378599A (en) | 1978-07-12 |
SE437004B (sv) | 1985-02-04 |
SE7714234L (sv) | 1978-06-18 |
NL187567B (nl) | 1991-06-17 |
IN149367B (fr) | 1981-11-21 |
DE2756423C2 (fr) | 1988-11-10 |
DE2756423A1 (de) | 1978-06-22 |
BR7708394A (pt) | 1978-07-25 |
CA1094526A (fr) | 1981-01-27 |
IT1088448B (it) | 1985-06-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |