CA731007A - Helicopter rotor system having elastomeric bearings - Google Patents

Helicopter rotor system having elastomeric bearings

Info

Publication number
CA731007A
CA731007A CA731007A CA731007DA CA731007A CA 731007 A CA731007 A CA 731007A CA 731007 A CA731007 A CA 731007A CA 731007D A CA731007D A CA 731007DA CA 731007 A CA731007 A CA 731007A
Authority
CA
Canada
Prior art keywords
rotor system
helicopter rotor
elastomeric bearings
elastomeric
bearings
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.)
Expired
Application number
CA731007A
Inventor
C. Ballauer Alb
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.)
RJ Enstrom Corp
Original Assignee
RJ Enstrom Corp
Publication date
Application granted granted Critical
Publication of CA731007A publication Critical patent/CA731007A/en
Expired legal-status Critical Current

Links

CA731007A Helicopter rotor system having elastomeric bearings Expired CA731007A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA731007T

Publications (1)

Publication Number Publication Date
CA731007A true CA731007A (en) 1966-03-29

Family

ID=36069933

Family Applications (1)

Application Number Title Priority Date Filing Date
CA731007A Expired CA731007A (en) Helicopter rotor system having elastomeric bearings

Country Status (1)

Country Link
CA (1) CA731007A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN120103886A (en) * 2025-05-12 2025-06-06 大连理工大学 A closed-loop control method for helicopter vibration based on cone constraints

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN120103886A (en) * 2025-05-12 2025-06-06 大连理工大学 A closed-loop control method for helicopter vibration based on cone constraints

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