GB383821A - Improvements in and relating to transverse driven bodies - Google Patents

Improvements in and relating to transverse driven bodies

Info

Publication number
GB383821A
GB383821A GB4630/32A GB463032A GB383821A GB 383821 A GB383821 A GB 383821A GB 4630/32 A GB4630/32 A GB 4630/32A GB 463032 A GB463032 A GB 463032A GB 383821 A GB383821 A GB 383821A
Authority
GB
United Kingdom
Prior art keywords
passage
slots
slot
apical
air
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
Application number
GB4630/32A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of GB383821A publication Critical patent/GB383821A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wind Motors (AREA)

Abstract

383,821. Aerofoils, propellers, and sails. ZIEGLER, J. F., 2, Schwarzenbergplatz, Vienna. Feb. 16, 1932, No. 4630. Convention date, March 27, 1931. [Classes 4, 114, and 115.] Transverse driven bodies such as aerofoils, sails, and turbine blades, which are designed to produce a reaction inclined to the direction of motion and which have a conducting passage extending from the pressure side of the surface to the suction side are formed with means for reversing the direction of fluid flow in the passage between an inflow slot of which both edges lie within the outline of the bottom surface and an outflow slot situated in the apical or main zone of the suction surface, such means taking the form of a C-shaped passage, whereby the suction stream first travels forwardly, then is reversed backwardly and leaves in the apical or main zone. This passage may be formed between a main transverse driven body or surface and a frontal body which forms in combination with the main portion, a body having a streamline contour. As applied to an aerofoil, Fig. 1, a lower inflow slot 1 communicates with an outflow slot 2 in the main zone 4 of the upper surface adjacent to apical zone 3. Between the slots is a direction reversing passage 5 having a nozzle-like constriction 6 opening into a larger space where the passage bends round. The inner wall 9 of the conducting passage is reflexly curved and further intake slots 10 may be provided. The slot opening may also be covered with a pervious material. In a modification several outflow slots are employed between normally closed resilient hinged tongues so that the slots which are most effective at any time will open. In a modification, Fig. 7, lower slots c<1> are controllable by springs or by non-automatic means such as those shown. In a still further modification, the wing surfaces are constructed with overlapping resilient scales between the edges of which the air passes. As applied to a mainsail 11, Fig. 2, the sail is secured to a mast 12 and is provided with an air-gap or with openings 13 for the passage of air. At either side of the mast and tangential to it are auxiliary surfaces 14, 15 which overlap the mainsail and are separated therefrom by leech ropes 16, 17 or struts. The surfaces 14, 15 extend past the passages 13 and thus form intake and outlet slots according to the direction of the wind. The air flow through the gaps 13 may be made smoother by sewing in a curved piece 18 of sailcloth or by the employment of a hollowedout rotatable mast as shown in Fig. 3, which Figure also shows the sail subjected to the action of the wind.
GB4630/32A 1931-03-27 1932-02-16 Improvements in and relating to transverse driven bodies Expired GB383821A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AT383821X 1931-03-27

Publications (1)

Publication Number Publication Date
GB383821A true GB383821A (en) 1932-11-24

Family

ID=3673194

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4630/32A Expired GB383821A (en) 1931-03-27 1932-02-16 Improvements in and relating to transverse driven bodies

Country Status (1)

Country Link
GB (1) GB383821A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2464663A (en) * 1943-08-21 1949-03-15 Zingg Theodor Slotted wing for aircraft
US2514513A (en) * 1942-03-06 1950-07-11 Lockheed Aircraft Corp Jet power plant with boundary layer control for aircraft
GB2186033A (en) * 1986-02-28 1987-08-05 Nei International Research & D Wind turbine
GB2234298A (en) * 1989-07-29 1991-01-30 Anthony Ngornadi Adimora Wind-driven power plants
EP1118747A2 (en) * 2000-01-22 2001-07-25 Rolls-Royce Plc An aerofoil for an axial flow turbomachine
US8764380B2 (en) 2010-07-07 2014-07-01 Rolls-Royce Plc Rotor blade

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2514513A (en) * 1942-03-06 1950-07-11 Lockheed Aircraft Corp Jet power plant with boundary layer control for aircraft
US2464663A (en) * 1943-08-21 1949-03-15 Zingg Theodor Slotted wing for aircraft
GB2186033A (en) * 1986-02-28 1987-08-05 Nei International Research & D Wind turbine
GB2186033B (en) * 1986-02-28 1990-01-04 Northern Eng Ind Wind turbine
GB2234298A (en) * 1989-07-29 1991-01-30 Anthony Ngornadi Adimora Wind-driven power plants
EP1118747A2 (en) * 2000-01-22 2001-07-25 Rolls-Royce Plc An aerofoil for an axial flow turbomachine
US6435815B2 (en) 2000-01-22 2002-08-20 Rolls-Royce Plc Aerofoil for an axial flow turbo machine
EP1118747A3 (en) * 2000-01-22 2003-01-08 Rolls-Royce Plc An aerofoil for an axial flow turbomachine
US8764380B2 (en) 2010-07-07 2014-07-01 Rolls-Royce Plc Rotor blade

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