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WO2002020350A3 - Method of providing an aircraft wing with an airfoil for low speed flight - Google Patents

Method of providing an aircraft wing with an airfoil for low speed flight Download PDF

Info

Publication number
WO2002020350A3
WO2002020350A3 PCT/US2001/028224 US0128224W WO0220350A3 WO 2002020350 A3 WO2002020350 A3 WO 2002020350A3 US 0128224 W US0128224 W US 0128224W WO 0220350 A3 WO0220350 A3 WO 0220350A3
Authority
WO
WIPO (PCT)
Prior art keywords
speed flight
low speed
airfoil
providing
aircraft wing
Prior art date
Application number
PCT/US2001/028224
Other languages
French (fr)
Other versions
WO2002020350A2 (en
Inventor
Norbert A Weisend Jr
Original Assignee
Goodrich Corp
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 Goodrich Corp filed Critical Goodrich Corp
Priority to AU2001290702A priority Critical patent/AU2001290702A1/en
Publication of WO2002020350A2 publication Critical patent/WO2002020350A2/en
Publication of WO2002020350A3 publication Critical patent/WO2002020350A3/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/16—De-icing or preventing icing on exterior surfaces of aircraft by mechanical means, e.g. pulsating mats or shoes attached to, or built into, surface
    • B64D15/166—De-icing or preventing icing on exterior surfaces of aircraft by mechanical means, e.g. pulsating mats or shoes attached to, or built into, surface using pneumatic boots
    • 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
    • B64C3/46—Varying camber by inflatable elements
    • 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)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

A method of altering the aerodynamic characteristics of the wings (14) of an aircraft (12). For low speed flight, a first wall portion (46) is expanded to provide an airfoil geometry for low speed flight (e.g., high camber, blunt leading edge) and a second wall portion (48) is maintained (e.g., suction is applied to a corresponding chamber) so that it follows a concave path. For high speed flight, the wall portions (46, 48) are retracted to provide the airfoil geometry for high speed flight (e.g., low camber, sharp leading edge).
PCT/US2001/028224 2000-09-07 2001-09-07 Method of providing an aircraft wing with an airfoil for low speed flight WO2002020350A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2001290702A AU2001290702A1 (en) 2000-09-07 2001-09-07 Method of providing an aircraft wing with an airfoil for low speed flight

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US65680000A 2000-09-07 2000-09-07
US09/656,800 2000-09-07

Publications (2)

Publication Number Publication Date
WO2002020350A2 WO2002020350A2 (en) 2002-03-14
WO2002020350A3 true WO2002020350A3 (en) 2002-09-26

Family

ID=24634620

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2001/028224 WO2002020350A2 (en) 2000-09-07 2001-09-07 Method of providing an aircraft wing with an airfoil for low speed flight

Country Status (1)

Country Link
WO (1) WO2002020350A2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2734680T3 (en) * 2015-10-15 2019-12-11 Airbus Operations Sl Leading edge for an aerodynamic profile
CN105626396A (en) * 2015-12-29 2016-06-01 北京金风科创风电设备有限公司 Blade deicing device, wind generating set and blade deicing method
CN112977836B (en) * 2021-05-11 2021-08-10 中国空气动力研究与发展中心低速空气动力研究所 Anti-icing device

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2378528A (en) * 1939-05-17 1945-06-19 Arsandaux Louis Supporting element for aircraft
US2934288A (en) * 1954-12-15 1960-04-26 Bendix Aviat Corp Control system for varying airfoil surfaces and the air inlet to the engine of an aircraft under prevailing operating conditions
US2937826A (en) * 1955-11-18 1960-05-24 Goodrich Co B F Means for altering the leading edge shape of an airfoil

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2378528A (en) * 1939-05-17 1945-06-19 Arsandaux Louis Supporting element for aircraft
US2934288A (en) * 1954-12-15 1960-04-26 Bendix Aviat Corp Control system for varying airfoil surfaces and the air inlet to the engine of an aircraft under prevailing operating conditions
US2937826A (en) * 1955-11-18 1960-05-24 Goodrich Co B F Means for altering the leading edge shape of an airfoil

Also Published As

Publication number Publication date
WO2002020350A2 (en) 2002-03-14

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