DE10163585A1 - Wing unit airfoil structure, has raised groove profiles extending from trailing edge towards leading edge in upper and lower skin shells - Google Patents

Wing unit airfoil structure, has raised groove profiles extending from trailing edge towards leading edge in upper and lower skin shells Download PDF

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Publication number
DE10163585A1
DE10163585A1 DE2001163585 DE10163585A DE10163585A1 DE 10163585 A1 DE10163585 A1 DE 10163585A1 DE 2001163585 DE2001163585 DE 2001163585 DE 10163585 A DE10163585 A DE 10163585A DE 10163585 A1 DE10163585 A1 DE 10163585A1
Authority
DE
Germany
Prior art keywords
lower skin
leading edge
trailing edge
wing unit
airfoil structure
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
Application number
DE2001163585
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German (de)
Other versions
DE10163585B4 (en
Inventor
Alexander Burchard
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.)
Airbus Operations GmbH
Original Assignee
Airbus Operations GmbH
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 Airbus Operations GmbH filed Critical Airbus Operations GmbH
Priority to DE2001163585 priority Critical patent/DE10163585B4/en
Publication of DE10163585A1 publication Critical patent/DE10163585A1/en
Application granted granted Critical
Publication of DE10163585B4 publication Critical patent/DE10163585B4/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof
    • 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
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/50—Varying camber by leading or trailing edge flaps

Abstract

Raised groove-shaped profiles (11) spaced apart in the span direction (3) are provided in the upper and lower skin shells (4, 5) forming the airfoil. The profile starts at the trailing edge (2) of the airfoil and its height reduces in height in the direction of the leading edge (1).
DE2001163585 2001-12-21 2001-12-21 Structure profile structure of an airplane Expired - Fee Related DE10163585B4 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE2001163585 DE10163585B4 (en) 2001-12-21 2001-12-21 Structure profile structure of an airplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2001163585 DE10163585B4 (en) 2001-12-21 2001-12-21 Structure profile structure of an airplane

Publications (2)

Publication Number Publication Date
DE10163585A1 true DE10163585A1 (en) 2005-05-04
DE10163585B4 DE10163585B4 (en) 2007-08-09

Family

ID=34398599

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2001163585 Expired - Fee Related DE10163585B4 (en) 2001-12-21 2001-12-21 Structure profile structure of an airplane

Country Status (1)

Country Link
DE (1) DE10163585B4 (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4830315A (en) * 1986-04-30 1989-05-16 United Technologies Corporation Airfoil-shaped body

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4830315A (en) * 1986-04-30 1989-05-16 United Technologies Corporation Airfoil-shaped body

Also Published As

Publication number Publication date
DE10163585B4 (en) 2007-08-09

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Legal Events

Date Code Title Description
OP8 Request for examination as to paragraph 44 patent law
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: AIRBUS OPERATIONS GMBH, 21129 HAMBURG, DE

R119 Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee