#AIRFOIL BLADE PDF#

238000000926 separation method Methods 0.000 description 2.238000005755 formation reaction Methods 0.000 description 2.230000015572 biosynthetic process Effects 0.000 description 2.

238000006073 displacement reaction Methods 0.000 claims description 13.

Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.) Filing date Publication date Priority to US903169 priority Critical Priority to US06/903,169 priority patent/US4744728A/en Application filed by United Technologies Corp filed Critical United Technologies Corp Publication of EP0262071A1 publication Critical patent/EP0262071A1/en Application granted granted Critical Publication of EP0262071B1 publication Critical patent/EP0262071B1/en Status Expired legal-status Critical Current Links Original Assignee United Technologies 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 or warranty as to the accuracy of the list.) ( en Inventor David Alan Lednicer Stephen John Owen 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 Application number EP87630148A Other languages German ( de)

#AIRFOIL BLADE PDF#

Google Patents Helicopter blade airfoilĭownload PDF Info Publication number EP0262071B1 EP0262071B1 EP87630148A EP87630148A EP0262071B1 EP 0262071 B1 EP0262071 B1 EP 0262071B1 EP 87630148 A EP87630148 A EP 87630148A EP 87630148 A EP87630148 A EP 87630148A EP 0262071 B1 EP0262071 B1 EP 0262071B1 Authority EP European Patent Office Prior art keywords airfoil blade section lift max Prior art date Legal status (The legal status is an assumption and is not a legal conclusion. Google Patents EP0262071B1 - Helicopter blade airfoil

Airfoil blade