ES232026A1 - UN PROCEDIMIENTO PARA LA OBTENCIoN DE REVESTIMIENTOS INFLABLES - Google Patents
UN PROCEDIMIENTO PARA LA OBTENCIoN DE REVESTIMIENTOS INFLABLESInfo
- Publication number
- ES232026A1 ES232026A1 ES0232026A ES232026A ES232026A1 ES 232026 A1 ES232026 A1 ES 232026A1 ES 0232026 A ES0232026 A ES 0232026A ES 232026 A ES232026 A ES 232026A ES 232026 A1 ES232026 A1 ES 232026A1
- Authority
- ES
- Spain
- Prior art keywords
- leading edge
- airfoil
- altering
- edge shape
- wing
- 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
- 238000000576 coating method Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
- B64C3/46—Varying camber by inflatable elements
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tents Or Canopies (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
Abstract
Un procedimiento para la obtención de revestimientos inflables para el borde de ataque de un ala o plano de avión caracterizado por las particularidades siguientes tomadas por separado o en combinación.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US547664A US2937826A (en) | 1955-11-18 | 1955-11-18 | Means for altering the leading edge shape of an airfoil |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES232026A1 true ES232026A1 (es) | 1957-04-16 |
Family
ID=24185611
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES0232026A Expired ES232026A1 (es) | 1955-11-18 | 1956-11-19 | UN PROCEDIMIENTO PARA LA OBTENCIoN DE REVESTIMIENTOS INFLABLES |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US2937826A (es) |
| ES (1) | ES232026A1 (es) |
Families Citing this family (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3074232A (en) * | 1959-07-25 | 1963-01-22 | Soyer Robert | Devices forming the mouthpieces of air admission pipes for jet engines for aircraft |
| US3623684A (en) * | 1970-02-18 | 1971-11-30 | Goodyear Tire & Rubber | Deicing device |
| US4185373A (en) * | 1977-10-25 | 1980-01-29 | General Dynamics Corporation | Method of manufacturing an inflatable air inlet duct |
| US4961549A (en) * | 1985-04-24 | 1990-10-09 | The B. F. Goodrich Company | Asymmetrical pneumatic deicer |
| US5248116A (en) * | 1992-02-07 | 1993-09-28 | The B. F. Goodrich Company | Airfoil with integral de-icer using overlapped tubes |
| US5681010A (en) * | 1995-10-13 | 1997-10-28 | Lockheed Missiles & Space Co., Inc. | Inflatable deployable control structures for aerospace vehicles |
| US6015115A (en) * | 1998-03-25 | 2000-01-18 | Lockheed Martin Corporation | Inflatable structures to control aircraft |
| WO2002020350A2 (en) | 2000-09-07 | 2002-03-14 | Goodrich Corporation | Method of providing an aircraft wing with an airfoil for low speed flight |
| US6443394B1 (en) | 2000-09-21 | 2002-09-03 | The B.F. Goodrich Company | Inflatable airfoil device |
| US6786457B2 (en) * | 2002-10-10 | 2004-09-07 | The Boeing Company | Geometric morphing wing with layers |
| US7195210B2 (en) * | 2002-10-10 | 2007-03-27 | The Boeing Company | Fiber matrix for a geometric morphing wing |
| US7798443B2 (en) * | 2006-12-18 | 2010-09-21 | The Boeing Company | Composite material for geometric morphing wing |
| US10144499B2 (en) * | 2008-09-17 | 2018-12-04 | Israel Aerospace Industries Ltd. | Aerofoil accessories and method for modifying the geometry of a wing element |
| IL216345A (en) | 2011-11-14 | 2017-09-28 | Israel Aerospace Ind Ltd | Wing and the devices for it |
| GB201420644D0 (en) * | 2014-11-20 | 2015-01-07 | Technion Res & Dev Foundation | Solid-liquid composite structures |
| ES2734680T3 (es) * | 2015-10-15 | 2019-12-11 | Airbus Operations Sl | Borde de ataque para un perfil aerodinámico |
| US10875638B2 (en) * | 2016-09-30 | 2020-12-29 | Sikorsky Aircraft Corporation | De-ice fairing bond fixture |
| EP4006333A1 (en) * | 2020-11-25 | 2022-06-01 | Siemens Gamesa Renewable Energy A/S | Turbine blade for a wind turbine |
| EP4102053A1 (en) * | 2021-06-07 | 2022-12-14 | Siemens Gamesa Renewable Energy A/S | Wind turbine blade and method for manufacturing a leading edge protection system for a wind turbine blade |
| AT525878B1 (de) * | 2022-03-24 | 2023-09-15 | Johannes Kepler Univ Linz | Fahrzeug |
| FR3167925A1 (fr) * | 2024-10-25 | 2026-05-01 | Safran Aerosystems | Systeme de degivrage du type pneumatique pour un aeronef |
| FR3167926A1 (fr) * | 2024-10-25 | 2026-05-01 | Safran Electrical & Power Tunisia | Systeme de degivrage du type pneumatique pour un aeronef |
| FR3171644A1 (fr) * | 2025-01-28 | 2026-07-31 | Airbus Operations | Aéronef comprenant au moins une structure aérodynamique non-structurelle gonflable |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1942867A (en) * | 1932-05-17 | 1934-01-09 | Goodrich Co B F | Deicer for aeroplanes |
| US2168328A (en) * | 1937-12-04 | 1939-08-08 | Walter S Diehl | Deicing means for airplanes |
| US2378528A (en) * | 1939-05-17 | 1945-06-19 | Arsandaux Louis | Supporting element for aircraft |
| US2271760A (en) * | 1939-07-19 | 1942-02-03 | Goodrich Co B F | Apparatus for preventing the accumulation of ice |
| US2320017A (en) * | 1940-07-12 | 1943-05-25 | Goodrich Co B F | Apparatus for preventing the accumulation of ice |
| US2306759A (en) * | 1940-07-23 | 1942-12-29 | Goodrich Co B F | Apparatus for improving wing slot operation |
| US2436889A (en) * | 1944-06-09 | 1948-03-02 | Goodrich Co B F | Protective apparatus for preventing accumulation of ice on airfoils |
| US2504684A (en) * | 1946-01-30 | 1950-04-18 | Goodrich Co B F | Extensible structure for varying the configuration of an aircraft surface |
-
1955
- 1955-11-18 US US547664A patent/US2937826A/en not_active Expired - Lifetime
-
1956
- 1956-11-19 ES ES0232026A patent/ES232026A1/es not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| US2937826A (en) | 1960-05-24 |
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