GB9825876D0 - New wing design - Google Patents

New wing design

Info

Publication number
GB9825876D0
GB9825876D0 GBGB9825876.7A GB9825876A GB9825876D0 GB 9825876 D0 GB9825876 D0 GB 9825876D0 GB 9825876 A GB9825876 A GB 9825876A GB 9825876 D0 GB9825876 D0 GB 9825876D0
Authority
GB
United Kingdom
Prior art keywords
wing design
passage
new wing
wing
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.)
Withdrawn
Application number
GBGB9825876.7A
Other versions
GB2344092A (en
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.)
SMYTH DAVID A
Original Assignee
SMYTH DAVID A
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 SMYTH DAVID A filed Critical SMYTH DAVID A
Priority to GB9825876A priority Critical patent/GB2344092A/en
Publication of GB9825876D0 publication Critical patent/GB9825876D0/en
Publication of GB2344092A publication Critical patent/GB2344092A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/04—Boundary layer controls by actively generating fluid flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/20—Boundary layer controls by passively inducing fluid flow, e.g. by means of a pressure difference between both ends of a slot or duct
    • 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

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Cleaning Of Streets, Tracks, Or Beaches (AREA)

Abstract

The wing comprises a passage 5, intended to conduct air from the upper surface of the leading edge of the wing to a lower surface of the wing thereby increasing lift. The passage may have multiple exits (4, fig.3) and the air could be sucked through the passage by means of jet engine or other propulsion device.
GB9825876A 1998-11-27 1998-11-27 Wing with airflow passage therethrough Withdrawn GB2344092A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9825876A GB2344092A (en) 1998-11-27 1998-11-27 Wing with airflow passage therethrough

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9825876A GB2344092A (en) 1998-11-27 1998-11-27 Wing with airflow passage therethrough

Publications (2)

Publication Number Publication Date
GB9825876D0 true GB9825876D0 (en) 1999-01-20
GB2344092A GB2344092A (en) 2000-05-31

Family

ID=10843057

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9825876A Withdrawn GB2344092A (en) 1998-11-27 1998-11-27 Wing with airflow passage therethrough

Country Status (1)

Country Link
GB (1) GB2344092A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0001399D0 (en) 2000-01-22 2000-03-08 Rolls Royce Plc An aerofoil for an axial flow turbomachine
GB0313456D0 (en) * 2003-06-11 2003-07-16 Rolls Royce Plc Propulsion arrangement
CN107344612A (en) * 2017-06-16 2017-11-14 青岛华创风能有限公司 A kind of gas control equipment for wings/blades

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB484405A (en) * 1936-11-02 1938-05-02 Bristol Aeroplane Co Ltd Improvements in aircraft
GB532892A (en) * 1938-08-04 1941-02-03 Edgar Roy Brewster A method of, and means for, increasing or varying the lift coefficient of the wing of an aeroplane
GB596580A (en) * 1943-08-21 1948-01-07 Theodor Zingg Reaction-propelled aeroplane
GB918325A (en) * 1960-07-02 1963-02-13 Dornier Werke Gmbh Aircraft which take-off and land on a cushion of air
GB1220055A (en) * 1967-02-10 1971-01-20 Lawrence Arthur Senhenn Fixed wing aeroplanes
US3512414A (en) * 1968-05-23 1970-05-19 Rosemount Eng Co Ltd Slotted airfoil sensor housing

Also Published As

Publication number Publication date
GB2344092A (en) 2000-05-31

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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)