GB1041353A - Aircraft propellor - Google Patents

Aircraft propellor

Info

Publication number
GB1041353A
GB1041353A GB208362A GB208362A GB1041353A GB 1041353 A GB1041353 A GB 1041353A GB 208362 A GB208362 A GB 208362A GB 208362 A GB208362 A GB 208362A GB 1041353 A GB1041353 A GB 1041353A
Authority
GB
United Kingdom
Prior art keywords
pitch
feathering
automatic
manual
propeller
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
GB208362A
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.)
ALEXANDER GRIGORIEVICH TOMILIN
BRONISLAV LUDVIGOVICH IAKUTS
IVAN LUKICH ALEXEEV
KONSTANTIN IVANOVICH ZHDANOV
NICKOLAI PROKHOROVICH KUZMICHO
NICKOLAI PROKHOROVICH KUZMICHOV
PAVEL IVANOVICH SOMOV
Original Assignee
ALEXANDER GRIGORIEVICH TOMILIN
BRONISLAV LUDVIGOVICH IAKUTS
IVAN LUKICH ALEXEEV
KONSTANTIN IVANOVICH ZHDANOV
NICKOLAI PROKHOROVICH KUZMICHO
NICKOLAI PROKHOROVICH KUZMICHOV
PAVEL IVANOVICH SOMOV
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 ALEXANDER GRIGORIEVICH TOMILIN, BRONISLAV LUDVIGOVICH IAKUTS, IVAN LUKICH ALEXEEV, KONSTANTIN IVANOVICH ZHDANOV, NICKOLAI PROKHOROVICH KUZMICHO, NICKOLAI PROKHOROVICH KUZMICHOV, PAVEL IVANOVICH SOMOV filed Critical ALEXANDER GRIGORIEVICH TOMILIN
Priority to GB208362A priority Critical patent/GB1041353A/en
Publication of GB1041353A publication Critical patent/GB1041353A/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
    • B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
    • B64C11/40—Blade pitch-changing mechanisms fluid, e.g. hydraulic automatic

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)

Abstract

1,041,353. Variable pitch propeller controls. K. I. ZHDANOV, L. M. NOGTJEV, P. I. SOMOV, N. P. KUZMICHOV, A. G. TOMILIN, I. L. ALEXEEV, and B. L. IAKUTS. March 6, 1953 [Jan. 19, 1962], No. 2083/62. Heading B7V. An hydraulic control system for a variable pitch propeller provides for (1) automatic constant speed operation, (2) automatic locking of blades against decrease in pitch if the oil pressure should fail, (3) automatic locking of the blades against decrease in pitch if the propeller speed becomes excessive, (4) arrest of the blades at an intermediate stop position during decreasing in pitch, (5) automatic feathering when thrust becomes negative, (6) automatic feathering to prevent excessive turbine speed, (7) normal manual feathering, (8) emergency manual feathering, (9) manual feathering, and (10) manual decreasing of pitch.
GB208362A 1962-01-19 1962-01-19 Aircraft propellor Expired GB1041353A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB208362A GB1041353A (en) 1962-01-19 1962-01-19 Aircraft propellor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB208362A GB1041353A (en) 1962-01-19 1962-01-19 Aircraft propellor

Publications (1)

Publication Number Publication Date
GB1041353A true GB1041353A (en) 1966-09-07

Family

ID=9733287

Family Applications (1)

Application Number Title Priority Date Filing Date
GB208362A Expired GB1041353A (en) 1962-01-19 1962-01-19 Aircraft propellor

Country Status (1)

Country Link
GB (1) GB1041353A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4533296A (en) * 1983-11-07 1985-08-06 United Technologies Corporation Pitch control system for variable pitch propeller
DE102012207447A1 (en) * 2012-05-04 2013-11-07 Rolls-Royce Deutschland Ltd & Co Kg Oil supply system for a propeller turbine engine
US8753084B2 (en) 2010-05-06 2014-06-17 Rolls-Royce Plc Back-up featherer
US8757976B2 (en) 2010-05-06 2014-06-24 Rolls-Royce Plc Pitch control mechanism
US8757975B2 (en) 2010-05-06 2014-06-24 Rolls-Royce Plc Pitch control mechanism
US8757977B2 (en) 2010-05-06 2014-06-24 Rolls-Royce Plc Back-up featherer

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4533296A (en) * 1983-11-07 1985-08-06 United Technologies Corporation Pitch control system for variable pitch propeller
US8753084B2 (en) 2010-05-06 2014-06-17 Rolls-Royce Plc Back-up featherer
US8757976B2 (en) 2010-05-06 2014-06-24 Rolls-Royce Plc Pitch control mechanism
US8757975B2 (en) 2010-05-06 2014-06-24 Rolls-Royce Plc Pitch control mechanism
US8757977B2 (en) 2010-05-06 2014-06-24 Rolls-Royce Plc Back-up featherer
DE102012207447A1 (en) * 2012-05-04 2013-11-07 Rolls-Royce Deutschland Ltd & Co Kg Oil supply system for a propeller turbine engine
US9416680B2 (en) 2012-05-04 2016-08-16 Rolls-Royce Deutschland Ltd & Co Kg Oil supply system for a propeller turbine engine

Similar Documents

Publication Publication Date Title
GB1520173A (en) Method of controlling the flight path of a lowflying aircraft
ES406110A1 (en) Variable pitch propeller with emergency control
GB1041353A (en) Aircraft propellor
GB1133739A (en) Improvements in or relating to control apparatus for aircraft propulsion units
GB1346563A (en) Rotary wing overload protection
GB1074873A (en) An adjustable pitch propeller
GB1174345A (en) Combined Propeller Pitch Lock and Low Pitch Stop System.
GB1267371A (en) Variable-pitch bladed rotors
GB467103A (en) Improved method of controlling variable pitch propellers
GB972080A (en) Improvements in or relating to a hydraulic servo-motor system,comprising a double-acting servo-motor
GB600603A (en) Improvements in or relating to propeller controls
GB947690A (en) Turbine control
GB816870A (en) Improvements in variable pitch propeller control systems
GB706338A (en) Improvements in or relating to hydraulic pitch control mechanism for propellers
GB1314195A (en) Variable pitch propellers
GB568531A (en) Improved operating gear for adjustable propeller blades
GB1527836A (en) Auxiliary device for controlling and manoeuvring an aircraft
GB1237189A (en) Emergency landing system, particularly for aircraft with high aspect ratio wings
CORBIN et al. The design of automatic flight control systems to reduce the effects of atmospheric disturbances(flight tests of experimental automatic pilots on BAC-111 aircraft)
Kamber An airframe manufacturer's requirements for future propulsion controls
JPS54162355A (en) Hydraulic elevator
GB577911A (en) Improvements in apparatus for controlling the speed of aero engines
GB534523A (en) Improvements in or relating to aircraft cabins
GB603089A (en) Improvements in automatic pilots for aircraft
GB1192179A (en) Improvements in or relating to Sealing Devices