GB2224253A - Removable flexible aerofoil section - Google Patents
Removable flexible aerofoil section Download PDFInfo
- Publication number
- GB2224253A GB2224253A GB8825569A GB8825569A GB2224253A GB 2224253 A GB2224253 A GB 2224253A GB 8825569 A GB8825569 A GB 8825569A GB 8825569 A GB8825569 A GB 8825569A GB 2224253 A GB2224253 A GB 2224253A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aerofoil section
- removable
- removable flexible
- flexible
- attached
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
- B64C31/028—Hang-glider-type aircraft; Microlight-type aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62J—CYCLE SADDLES OR SEATS; AUXILIARY DEVICES OR ACCESSORIES SPECIALLY ADAPTED TO CYCLES AND NOT OTHERWISE PROVIDED FOR, e.g. ARTICLE CARRIERS OR CYCLE PROTECTORS
- B62J17/00—Weather guards for riders; Fairings or stream-lining parts not otherwise provided for
- B62J17/10—Ventilation or air guiding devices forming part of fairings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62K—CYCLES; CYCLE FRAMES; CYCLE STEERING DEVICES; RIDER-OPERATED TERMINAL CONTROLS SPECIALLY ADAPTED FOR CYCLES; CYCLE AXLE SUSPENSIONS; CYCLE SIDE-CARS, FORECARS, OR THE LIKE
- B62K19/00—Cycle frames
- B62K19/02—Cycle frames characterised by material or cross-section of frame members
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Earth Drilling (AREA)
Abstract
An aerofoil section e.g. on exposed tubing on a hang glider or pedal cycle has a body 1 which is removable so that it can be replaced on a repaired construction and is flexible in order that under adverse loads will not deform or fracture. <IMAGE>
Description
REMOVABLE FLEXIBLE AEROFOIL SECTION
Constructions subjected to low speed airflow are subject of parasitic drag which can be reduced by creating a classical peardrop aerofoil shape around the existing construction.
Particularly in the use of class one flex wings (hang gliders), microlights and pedal cycle frames and accessories. Solid aerofoil sections however, are heavier than spherical tube sections have low lateral strength capabilities but are excessively strong in frontal loads which can cause unnecessary injury or discomfort e.g., when a pilot collides with the structure under heavy landing conditions in the case of the hang glider and when a rider is forced to carry the cycle manually in the case of a cyclocross competition.
According to the present invention there is provided a flexible aerofoil section comprising of two separate hollow sections which may be formed by way of extrusion, moulding, or other suitable profiling technique which when mounted on an existing tubular construction creates classical peardrop aerofoil shape which can be removed or added as required.
A specific embodiment of the invention will now be described by way of example with reference to the accompanying drawing in which: - Figure 1 - shows in perspective, the sections in position on an existing tubular construction.
Figure 2 - shows the separation of the sections from the construction.
Figure 3 - shows the mounting of the sections on the exposed tubing on a hang glider.
Figure 4 - shows the mounting of the sections on the exposed tubing on a pedal cycle.
Referring to the drawing the sections comprise of a flexible extruded or moulded material secured to the existing construction by, for example, glue, ties or similar means (not shown).
In order to attach the section(s) to. the existing tubing it is placed at a predetermined angle in order that the greatest efficiency is gained when exposed to the primary airflow in which reduction in drag is required. It is then fixed by the means previously explained.
In order to remove in the case of breakage of the main structure to which the section(s) have been attached the ties or bonding methods are released.
Claims (5)
1. - An aerofoil section comprising of two separate sections which can be added in part or in whole to an existing tubular construction in order to reduce parasitic drag.
2. A removable aerofoil section as claimed in 1 where the material of construction is flexible. which allows it to recover from severe bending or compression moments without damage.
3. A removable flexible aerofoil section as claimed in 1 and 2 when attached to the exposed tubing on a hang glider.
4. A removable flexible aerofoil section as claimed in 1 and 2 when attached to the exposed tubing on a microlight.
5. A removable flexible aerofoil section as claimed in 1 and 2 when attached to the frame or accessories on a pedal cycle.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8825569A GB2224253A (en) | 1988-11-01 | 1988-11-01 | Removable flexible aerofoil section |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8825569A GB2224253A (en) | 1988-11-01 | 1988-11-01 | Removable flexible aerofoil section |
Publications (2)
Publication Number | Publication Date |
---|---|
GB8825569D0 GB8825569D0 (en) | 1988-12-07 |
GB2224253A true GB2224253A (en) | 1990-05-02 |
Family
ID=10646139
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8825569A Withdrawn GB2224253A (en) | 1988-11-01 | 1988-11-01 | Removable flexible aerofoil section |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2224253A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2231316A (en) * | 1989-05-03 | 1990-11-14 | Christopher John Gladish | Flexible lightweight aerofoil sheath for hang-glider and micro-light "uprights" and king posts |
GB2278814A (en) * | 1993-06-04 | 1994-12-14 | Moore Large & Co Ltd | A bicycle frame |
EP0686551A1 (en) * | 1994-06-11 | 1995-12-13 | Honda Giken Kogyo Kabushiki Kaisha | Body cover structure in motor-assisted bicycle |
US5538285A (en) * | 1994-01-18 | 1996-07-23 | Goode; David P. | Ski pole shaft with rotating wing foil |
US5782139A (en) * | 1995-09-06 | 1998-07-21 | Fraiman; Peter G. | Bicycle handlebar centerpiece |
US7147238B2 (en) * | 2003-08-05 | 2006-12-12 | Shimano, Inc. | Bicycle part with a partitioned chamber |
WO2009115806A1 (en) * | 2008-03-20 | 2009-09-24 | The United Kingdom Sports Council | Component for a bicycle to reduce aerodynamic drag |
EP2241497A1 (en) * | 2009-04-14 | 2010-10-20 | Vroomen/White Design Inc. | Aerodynamic handlebar storage container |
EP1886911A3 (en) * | 2006-08-10 | 2011-02-23 | Philip White | Aerodynamic fork mast structure |
DE102009054398C5 (en) * | 2009-11-24 | 2018-05-03 | Scott Sports S.A. | Component for bicycle frame |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB365300A (en) * | 1931-01-05 | 1932-01-21 | Albert Eustace Short | Improvements in fairings for streamlining struts of aircraft |
-
1988
- 1988-11-01 GB GB8825569A patent/GB2224253A/en not_active Withdrawn
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB365300A (en) * | 1931-01-05 | 1932-01-21 | Albert Eustace Short | Improvements in fairings for streamlining struts of aircraft |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2231316A (en) * | 1989-05-03 | 1990-11-14 | Christopher John Gladish | Flexible lightweight aerofoil sheath for hang-glider and micro-light "uprights" and king posts |
GB2231316B (en) * | 1989-05-03 | 1993-03-31 | Christopher John Gladish | Flexible lightweight aerofoil sheath for hang-glider and micro-light uprights and king-posts |
GB2278814B (en) * | 1993-06-04 | 1996-10-09 | Moore Large & Co Ltd | Bicycle |
WO1994029162A1 (en) * | 1993-06-04 | 1994-12-22 | Moore Large & Co. Limited | Bicycle frame with outer casing |
GB2278814A (en) * | 1993-06-04 | 1994-12-14 | Moore Large & Co Ltd | A bicycle frame |
US5538285A (en) * | 1994-01-18 | 1996-07-23 | Goode; David P. | Ski pole shaft with rotating wing foil |
EP0686551A1 (en) * | 1994-06-11 | 1995-12-13 | Honda Giken Kogyo Kabushiki Kaisha | Body cover structure in motor-assisted bicycle |
US5782139A (en) * | 1995-09-06 | 1998-07-21 | Fraiman; Peter G. | Bicycle handlebar centerpiece |
US7147238B2 (en) * | 2003-08-05 | 2006-12-12 | Shimano, Inc. | Bicycle part with a partitioned chamber |
EP1886911A3 (en) * | 2006-08-10 | 2011-02-23 | Philip White | Aerodynamic fork mast structure |
WO2009115806A1 (en) * | 2008-03-20 | 2009-09-24 | The United Kingdom Sports Council | Component for a bicycle to reduce aerodynamic drag |
EP2241497A1 (en) * | 2009-04-14 | 2010-10-20 | Vroomen/White Design Inc. | Aerodynamic handlebar storage container |
US9051023B2 (en) | 2009-04-14 | 2015-06-09 | Vroomen/White Design Inc. | Aerodynamic handlebar storage container |
DE102009054398C5 (en) * | 2009-11-24 | 2018-05-03 | Scott Sports S.A. | Component for bicycle frame |
Also Published As
Publication number | Publication date |
---|---|
GB8825569D0 (en) | 1988-12-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |