ES2438009B1 - Airplane wings with stabilizer tubes - Google Patents
Airplane wings with stabilizer tubes Download PDFInfo
- Publication number
- ES2438009B1 ES2438009B1 ES201200764A ES201200764A ES2438009B1 ES 2438009 B1 ES2438009 B1 ES 2438009B1 ES 201200764 A ES201200764 A ES 201200764A ES 201200764 A ES201200764 A ES 201200764A ES 2438009 B1 ES2438009 B1 ES 2438009B1
- Authority
- ES
- Spain
- Prior art keywords
- wings
- plane
- tubes
- boxes
- work
- 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.)
- Active
Links
- 239000003381 stabilizer Substances 0.000 title abstract 2
- 230000000087 stabilizing effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
- B64C3/16—Frontal aspect
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/08—Aircraft not otherwise provided for having multiple wings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
- Road Paving Structures (AREA)
Abstract
Las alas de avión, con tubos estabilizadores, se caracterizan por tener una forma distinta a las habituales alas que se prolongan perpendicularmente desde el fuselaje del avión. Son cajas (2) ó (5), que pueden adquirir formas distintas, -cuadradas, paralelepipédicas o circulares-, que están rellenas de múltiples tubitos (3). En los extremos de las alas (2) se pondrán otros tubos más grandes (4) que tendrán una función estabilizadora. De esta manera, el avión funcionará como si tuviese tantas alas como pisos de tubitos (3) haya en las cajas (2), lo que permite que el avión tenga un descenso muy lento cuando no funcionen sus motores.The plane wings, with stabilizer tubes, are characterized by having a different shape than the usual wings that extend perpendicularly from the fuselage of the plane. They are boxes (2) or (5), which can acquire different shapes, -square, parallelepipedic or circular-, which are filled with multiple tubes (3). At the ends of the wings (2) will be placed other larger tubes (4) that will have a stabilizing function. In this way, the plane will work as if it had as many wings as there are tube floors (3) in the boxes (2), which allows the plane to have a very slow descent when its engines do not work.
Description
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES201200764A ES2438009B1 (en) | 2012-07-12 | 2012-07-12 | Airplane wings with stabilizer tubes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES201200764A ES2438009B1 (en) | 2012-07-12 | 2012-07-12 | Airplane wings with stabilizer tubes |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| ES2438009A1 ES2438009A1 (en) | 2014-01-15 |
| ES2438009B1 true ES2438009B1 (en) | 2014-10-28 |
Family
ID=49912577
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES201200764A Active ES2438009B1 (en) | 2012-07-12 | 2012-07-12 | Airplane wings with stabilizer tubes |
Country Status (1)
| Country | Link |
|---|---|
| ES (1) | ES2438009B1 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2546705B1 (en) * | 2014-03-25 | 2016-08-09 | Fº JAVIER PORRAS VILA | Airplane with groups of fins above and below the fuselage and wings |
| ES2547361B1 (en) * | 2014-04-04 | 2017-01-18 | Fº JAVIER PORRAS VILA | Helicopter with finned structure on lever radius and fins on propellers |
| ES2606943B1 (en) * | 2015-09-25 | 2018-01-08 | Fº JAVIER PORRAS VILA | Airplane with anti-drop tubes, with diaphragm and fins |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1001944A (en) * | 1946-07-04 | 1952-02-29 | Jet aerodyne refinements | |
| US2576294A (en) * | 1948-06-26 | 1951-11-27 | Alexander D Geraci | Airplane sustentation and control surface arrangement |
| DE1121476B (en) * | 1959-05-11 | 1962-01-04 | Gen Electric | Wing for supersonic speeds |
| DE2657714A1 (en) * | 1976-12-20 | 1978-06-22 | Reinhard Oster | Aircraft wing with cascade configuration - has horizontal aerofoil section blades mounted in frame with wing section top and bottom members |
| AU1057688A (en) * | 1987-01-03 | 1988-07-27 | Christian Taramasco | Vertical take-off and landing aircraft |
| ES2174690B1 (en) * | 1999-12-01 | 2004-09-16 | Manuel Muñoz Saiz | SUSTAINING PROVISION FOR AIRCRAFT. |
| WO2009093923A1 (en) * | 2008-01-21 | 2009-07-30 | Sergey Nikolaevich Afanasyev | Aircraft |
-
2012
- 2012-07-12 ES ES201200764A patent/ES2438009B1/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| ES2438009A1 (en) | 2014-01-15 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FG2A | Definitive protection |
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