GB306155A - Propelling set for high altitude aeroplanes - Google Patents

Propelling set for high altitude aeroplanes

Info

Publication number
GB306155A
GB306155A GB5265/29A GB526529A GB306155A GB 306155 A GB306155 A GB 306155A GB 5265/29 A GB5265/29 A GB 5265/29A GB 526529 A GB526529 A GB 526529A GB 306155 A GB306155 A GB 306155A
Authority
GB
United Kingdom
Prior art keywords
aeroplanes
high altitude
propelling set
propelling
fuscaldo
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
GB5265/29A
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
Publication of GB306155A publication Critical patent/GB306155A/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
    • B64C11/32—Blade pitch-changing mechanisms mechanical
    • B64C11/34—Blade pitch-changing mechanisms mechanical automatic

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Turbines (AREA)

Abstract

306,155. Fuscaldo, O. Feb. 17, 1928, [Convention date]. Void [Published under Sect. 91 of the Acts]. Regulating.-In an aircraft engine having a centrifugal or rotary compressor supplying mixture from the carburettor, the throttle valve is gradually closed, and the propeller pitch is gradually reduced, as the altitude decreases. The throttle lever may be actuated by hand or automatically by a barometric device.
GB5265/29A 1928-02-17 1929-02-16 Propelling set for high altitude aeroplanes Expired GB306155A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT306155X 1928-02-17

Publications (1)

Publication Number Publication Date
GB306155A true GB306155A (en) 1929-12-05

Family

ID=11230176

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5265/29A Expired GB306155A (en) 1928-02-17 1929-02-16 Propelling set for high altitude aeroplanes

Country Status (1)

Country Link
GB (1) GB306155A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE860902C (en) * 1942-02-26 1952-12-29 Daimler Benz Ag Regulation for elevator engines with exhaust gas turbochargers

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE860902C (en) * 1942-02-26 1952-12-29 Daimler Benz Ag Regulation for elevator engines with exhaust gas turbochargers

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