GB302752A - Sustaining propeller and regulator - Google Patents

Sustaining propeller and regulator

Info

Publication number
GB302752A
GB302752A GB26582/27A GB2658227A GB302752A GB 302752 A GB302752 A GB 302752A GB 26582/27 A GB26582/27 A GB 26582/27A GB 2658227 A GB2658227 A GB 2658227A GB 302752 A GB302752 A GB 302752A
Authority
GB
United Kingdom
Prior art keywords
blades
regulator
controlling
addition
control stick
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
GB26582/27A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB26582/27A priority Critical patent/GB302752A/en
Publication of GB302752A publication Critical patent/GB302752A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/54Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement

Abstract

302,752. Oehmichen, E. Oct. 7, 1927. Addition to 272,871. Controlling.-The helicopter according to parent Specification is modified by the addition of means for controlling the incidence of the blades by a transmission gear from the pilot's control stick. According to the arrangement the control stick 67 is linked by wires 62, 63 with a gimbal ring 49 which are supported upon the main lifting blades 41 and the automatic regulating blades 50.
GB26582/27A 1927-10-07 1927-10-07 Sustaining propeller and regulator Expired GB302752A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB26582/27A GB302752A (en) 1927-10-07 1927-10-07 Sustaining propeller and regulator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB26582/27A GB302752A (en) 1927-10-07 1927-10-07 Sustaining propeller and regulator

Publications (1)

Publication Number Publication Date
GB302752A true GB302752A (en) 1928-12-27

Family

ID=10245886

Family Applications (1)

Application Number Title Priority Date Filing Date
GB26582/27A Expired GB302752A (en) 1927-10-07 1927-10-07 Sustaining propeller and regulator

Country Status (1)

Country Link
GB (1) GB302752A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2432441A (en) * 1943-07-17 1947-12-09 Joseph S Pecker Hub for rotary wing aircraft and the like
US2473331A (en) * 1944-10-20 1949-06-14 Vertiflite Inc Helicopter power and control mechanism
US2690811A (en) * 1950-01-24 1954-10-05 Richard Gilbert Rotary blade device for aircraft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2432441A (en) * 1943-07-17 1947-12-09 Joseph S Pecker Hub for rotary wing aircraft and the like
US2473331A (en) * 1944-10-20 1949-06-14 Vertiflite Inc Helicopter power and control mechanism
US2690811A (en) * 1950-01-24 1954-10-05 Richard Gilbert Rotary blade device for aircraft

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