ES160651A1 - ADJUSTABLE DEVICE FOR SUCCESSIVELY ARRANGED COUNTER-DRIVE AIR PROPELLERS - Google Patents

ADJUSTABLE DEVICE FOR SUCCESSIVELY ARRANGED COUNTER-DRIVE AIR PROPELLERS

Info

Publication number
ES160651A1
ES160651A1 ES0160651A ES160651A ES160651A1 ES 160651 A1 ES160651 A1 ES 160651A1 ES 0160651 A ES0160651 A ES 0160651A ES 160651 A ES160651 A ES 160651A ES 160651 A1 ES160651 A1 ES 160651A1
Authority
ES
Spain
Prior art keywords
successively arranged
adjustable device
drive air
arranged counter
air propellers
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
ES0160651A
Other languages
Spanish (es)
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.)
Messerschmidt A G
Original Assignee
Messerschmidt A G
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 Messerschmidt A G filed Critical Messerschmidt A G
Publication of ES160651A1 publication Critical patent/ES160651A1/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/306—Blade pitch-changing mechanisms specially adapted for contrarotating propellers

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Dispostivo regulable para hélices aéreas de contramarcha sucesivamente dispuestas caracterizado por dos accionamientos regulables separados que al menos parcialmente giran con la hélice del lado del motor y por un manguito intermedio de deslizamiento dispuesto entre ambas hélices aéreas que contenga dos partes relativamente giratorias entre sí por medio del cual se transmite el movimiento de uno de ambos accionamientos regulables a las aspas de la hélice aérea distante del motor.Adjustable device for successively arranged counter-gear aerial propellers characterized by two separate adjustable drives that at least partially rotate with the propeller on the engine side and by an intermediate sliding sleeve arranged between both aerial propellers containing two parts that are relatively rotatable relative to each other by means of the which the movement of one of the two adjustable drives is transmitted to the blades of the air propeller distant from the engine.

ES0160651A 1942-03-13 1943-03-10 ADJUSTABLE DEVICE FOR SUCCESSIVELY ARRANGED COUNTER-DRIVE AIR PROPELLERS Expired ES160651A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE233498X 1942-03-13

Publications (1)

Publication Number Publication Date
ES160651A1 true ES160651A1 (en) 1943-07-01

Family

ID=5886434

Family Applications (1)

Application Number Title Priority Date Filing Date
ES0160651A Expired ES160651A1 (en) 1942-03-13 1943-03-10 ADJUSTABLE DEVICE FOR SUCCESSIVELY ARRANGED COUNTER-DRIVE AIR PROPELLERS

Country Status (2)

Country Link
CH (1) CH233498A (en)
ES (1) ES160651A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL285118A (en) * 1961-11-09
US4657484A (en) * 1984-09-04 1987-04-14 General Electric Company Blade pitch varying means
GB201408103D0 (en) * 2014-05-08 2014-06-25 Rolls Royce Plc A system

Also Published As

Publication number Publication date
CH233498A (en) 1944-07-31

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