CA2054807C - Methode et appareil de modification d'ailes d'avion - Google Patents
Methode et appareil de modification d'ailes d'avion Download PDFInfo
- Publication number
- CA2054807C CA2054807C CA002054807A CA2054807A CA2054807C CA 2054807 C CA2054807 C CA 2054807C CA 002054807 A CA002054807 A CA 002054807A CA 2054807 A CA2054807 A CA 2054807A CA 2054807 C CA2054807 C CA 2054807C
- Authority
- CA
- Canada
- Prior art keywords
- wing
- leading edge
- flap
- modification
- tip
- 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 - Lifetime
Links
- 238000002715 modification method Methods 0.000 title description 2
- 238000012986 modification Methods 0.000 claims abstract description 58
- 230000004048 modification Effects 0.000 claims abstract description 58
- 241000499489 Castor canadensis Species 0.000 claims abstract description 20
- 235000011779 Menyanthes trifoliata Nutrition 0.000 claims abstract description 20
- 241001233242 Lontra Species 0.000 claims abstract description 11
- 239000000853 adhesive Substances 0.000 description 6
- 230000001070 adhesive effect Effects 0.000 description 6
- 238000009434 installation Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 5
- 229910000547 2024-T3 aluminium alloy Inorganic materials 0.000 description 4
- 229920000260 silastic Polymers 0.000 description 4
- 229920005830 Polyurethane Foam Polymers 0.000 description 3
- 239000011496 polyurethane foam Substances 0.000 description 3
- 241001274197 Scatophagus argus Species 0.000 description 2
- 238000005553 drilling Methods 0.000 description 2
- 239000000945 filler Substances 0.000 description 2
- 239000006260 foam Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- SUBDBMMJDZJVOS-UHFFFAOYSA-N 5-methoxy-2-{[(4-methoxy-3,5-dimethylpyridin-2-yl)methyl]sulfinyl}-1H-benzimidazole Chemical compound N=1C2=CC(OC)=CC=C2NC=1S(=O)CC1=NC=C(C)C(OC)=C1C SUBDBMMJDZJVOS-UHFFFAOYSA-N 0.000 description 1
- 241000985905 Candidatus Phytoplasma solani Species 0.000 description 1
- VVQNEPGJFQJSBK-UHFFFAOYSA-N Methyl methacrylate Chemical compound COC(=O)C(C)=C VVQNEPGJFQJSBK-UHFFFAOYSA-N 0.000 description 1
- 229920005372 Plexiglas® Polymers 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000011152 fibreglass Substances 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 238000013101 initial test Methods 0.000 description 1
- 230000000873 masking effect Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000003607 modifier Substances 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/58—Wings provided with fences or spoilers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Agricultural Chemicals And Associated Chemicals (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA002054807A CA2054807C (fr) | 1991-11-01 | 1991-11-01 | Methode et appareil de modification d'ailes d'avion |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA002054807A CA2054807C (fr) | 1991-11-01 | 1991-11-01 | Methode et appareil de modification d'ailes d'avion |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2054807A1 CA2054807A1 (fr) | 1993-05-02 |
| CA2054807C true CA2054807C (fr) | 2002-08-20 |
Family
ID=4148684
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002054807A Expired - Lifetime CA2054807C (fr) | 1991-11-01 | 1991-11-01 | Methode et appareil de modification d'ailes d'avion |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA2054807C (fr) |
-
1991
- 1991-11-01 CA CA002054807A patent/CA2054807C/fr not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| CA2054807A1 (fr) | 1993-05-02 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US5213287A (en) | Wing modification method and apparatus | |
| US5407153A (en) | System for increasing airplane fuel mileage and airplane wing modification kit | |
| AU687466B2 (en) | Multi-purpose aircraft | |
| US6098922A (en) | Lifting-fuselage/wing aircraft having low induced drag | |
| US5114097A (en) | Aircraft | |
| US5769358A (en) | Lifting-fuselage/wing aircraft having an elliptical forebody | |
| US3411738A (en) | Airfoil tip | |
| CA2291275A1 (fr) | Extremites d'aile carrossees a bord d'attaque arrondi | |
| GB2144688A (en) | Underwing engine installation for aircraft | |
| US4489905A (en) | Nacelle-pylon configuration for an aircraft and method of using the same | |
| US5496001A (en) | T-38 aircraft modified with an F-5 wing | |
| US4132375A (en) | Vortex-lift roll-control device | |
| EP3243742A1 (fr) | Joint d'aéronef | |
| Shevell et al. | Aerodynamic design features of the DC-9. | |
| GB2583332A (en) | Aircraft wing | |
| Olason et al. | Aerodynamic design philosophy of the Boeing 737. | |
| CA2054807C (fr) | Methode et appareil de modification d'ailes d'avion | |
| US3406929A (en) | Aerofoils | |
| EP0221204B1 (fr) | Avion supersonique | |
| US12269593B2 (en) | Wing assemblies and aircraft | |
| US7487935B2 (en) | Aircraft having variable incidence wing and air cushion landing system | |
| US2960286A (en) | Means for providing directional stability | |
| Edi | Investigation of the application of hybrid laminar flow control and variable camber wing design for regional aircraft | |
| RU2051839C1 (ru) | Сверхзвуковой летательный аппарат | |
| Paterson | Aerodynamic Design Features of the C‐5A: An account of some of the problems encountered and the solutions adopted in the design of the Galaxy |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKEX | Expiry | ||
| MKEX | Expiry |
Effective date: 20111101 |