CA2195413A1 - Lift enhancing tip vortex generation technology - Google Patents
Lift enhancing tip vortex generation technologyInfo
- Publication number
- CA2195413A1 CA2195413A1 CA002195413A CA2195413A CA2195413A1 CA 2195413 A1 CA2195413 A1 CA 2195413A1 CA 002195413 A CA002195413 A CA 002195413A CA 2195413 A CA2195413 A CA 2195413A CA 2195413 A1 CA2195413 A1 CA 2195413A1
- Authority
- CA
- Canada
- Prior art keywords
- foil
- vortex
- methods
- tip
- beneficial
- 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
-
- 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
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Methods for using tip generated vortices to improve performance of foils. These methods include generating substantially streamwise beneficial vortex (74) near the outboard end (60) of a foil (82). This beneficial vortex (74) spins in the opposite direction of an induced drag vortex (62), and is used to create an upwash field (76) which neutralizes induced drag by deflecting the flow behind the trailing edge (56) at an upward angle. Upwash field (76) causes the lift vector (118) on the foil (82) to tilt forward, thereby creating a forward directed force of induced thrust upon the foil (82). Beneficial vortex (74) is also used to contain and compress the high pressure field existing along the attacking surface of the foil (82). Embodiments include a twist (66) along the span of a foil (82b), an anhedral tip droop having a divergent axis of droop curvature (86), a movable vortex flap (102), a cone shaped vortex flap network (162). Methods for reducing overall tip vorticity are disclosed.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/276,407 | 1994-07-18 | ||
US08/276,407 US5634613A (en) | 1994-07-18 | 1994-07-18 | Tip vortex generation technology for creating a lift enhancing and drag reducing upwash effect |
PCT/US1995/009051 WO1996003215A2 (en) | 1994-07-18 | 1995-07-18 | Lift enhancing tip vortex generation technology |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2195413A1 true CA2195413A1 (en) | 1996-02-08 |
CA2195413C CA2195413C (en) | 2005-10-25 |
Family
ID=35311693
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002195413A Expired - Lifetime CA2195413C (en) | 1994-07-18 | 1995-07-18 | Lift enhancing tip vortex generation technology |
Country Status (1)
Country | Link |
---|---|
CA (1) | CA2195413C (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115885915A (en) * | 2022-11-24 | 2023-04-04 | 武汉理工大学 | Multi-point oxygen supply device |
-
1995
- 1995-07-18 CA CA002195413A patent/CA2195413C/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115885915A (en) * | 2022-11-24 | 2023-04-04 | 武汉理工大学 | Multi-point oxygen supply device |
CN115885915B (en) * | 2022-11-24 | 2023-06-27 | 武汉理工大学 | Multi-point oxygen supply device |
Also Published As
Publication number | Publication date |
---|---|
CA2195413C (en) | 2005-10-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKEX | Expiry |
Effective date: 20150720 |