CH270741A - Flight control device of an aerodyne. - Google Patents

Flight control device of an aerodyne.

Info

Publication number
CH270741A
CH270741A CH270741DA CH270741A CH 270741 A CH270741 A CH 270741A CH 270741D A CH270741D A CH 270741DA CH 270741 A CH270741 A CH 270741A
Authority
CH
Switzerland
Prior art keywords
aerodyne
control device
flight control
flight
control
Prior art date
Application number
Other languages
French (fr)
Inventor
Corporation Bell Aircraft
Original Assignee
Bell Aircraft 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 Bell Aircraft Corp filed Critical Bell Aircraft Corp
Publication of CH270741A publication Critical patent/CH270741A/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
CH270741D 1943-03-10 1947-08-15 Flight control device of an aerodyne. CH270741A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US270741XA 1943-03-10 1943-03-10

Publications (1)

Publication Number Publication Date
CH270741A true CH270741A (en) 1950-09-15

Family

ID=21835540

Family Applications (1)

Application Number Title Priority Date Filing Date
CH270741D CH270741A (en) 1943-03-10 1947-08-15 Flight control device of an aerodyne.

Country Status (1)

Country Link
CH (1) CH270741A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113247242A (en) * 2021-04-12 2021-08-13 重庆大学 Transmission mechanism of upper rotor system of coaxial double-rotor helicopter

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113247242A (en) * 2021-04-12 2021-08-13 重庆大学 Transmission mechanism of upper rotor system of coaxial double-rotor helicopter

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