![]() The cambering apparatus comprises an upper surface flexible skin panel which is supported along its inner edge by a wing spar assembly and along its outermost edge, by an airfoil edge forming structure. Y02T50/00- Aeronautics or air transportĪ variable camber apparatus for the leading and/or trailing edge of an airfoil that is operable for lift variation at high airspeeds of a jet aircraft such as for maneuvering of fighter aircraft.Y02T- CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION.Y02- TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE.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 AND DIGESTS.B64C3/48- Varying camber by relatively-movable parts of wing structures.B64C3/38- Adjustment of complete wings or parts thereof.238000006011 modification reaction Methods 0.000 description 8.Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.) Filing date Publication date Priority claimed from US05/607,004 external-priority patent/US3994452A/en Application filed by Boeing Co filed Critical Boeing Co Priority to US05/708,671 priority Critical patent/US4053124A/en Application granted granted Critical Publication of US4053124A publication Critical patent/US4053124A/en Anticipated expiration legal-status Critical Status Expired - Lifetime legal-status Critical Current Links Original Assignee Boeing Co 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 or warranty as to the accuracy of the list.) Cole Current Assignee (The listed assignees may be inaccurate. ![]() Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.) Expired - Lifetime Application number US05/708,671 Inventor James B. Google Patents US4053124A - Variable camber airfoilÄownload PDF Info Publication number US4053124A US4053124A US05/708,671 US70867176A US4053124A US 4053124 A US4053124 A US 4053124A US 70867176 A US70867176 A US 70867176A US 4053124 A US4053124 A US 4053124A Authority US United States Prior art keywords airfoil trailing edge chordwise rib camber Prior art date Legal status (The legal status is an assumption and is not a legal conclusion.
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