GB511941A - Improvements in or relating to engines and method of reducing vibrations therein - Google Patents

Improvements in or relating to engines and method of reducing vibrations therein

Info

Publication number
GB511941A
GB511941A GB35483/37A GB3548337A GB511941A GB 511941 A GB511941 A GB 511941A GB 35483/37 A GB35483/37 A GB 35483/37A GB 3548337 A GB3548337 A GB 3548337A GB 511941 A GB511941 A GB 511941A
Authority
GB
United Kingdom
Prior art keywords
rods
master
groups
cranks
engines
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
GB35483/37A
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.)
Raytheon Technologies Corp
Original Assignee
United 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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of GB511941A publication Critical patent/GB511941A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/22Compensation of inertia forces
    • F16F15/24Compensation of inertia forces of crankshaft systems by particular disposition of cranks, pistons, or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B75/22Multi-cylinder engines with cylinders in V, fan, or star arrangement
    • F02B75/222Multi-cylinder engines with cylinders in V, fan, or star arrangement with cylinders in star arrangement

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Abstract

511,941. Fluid-pressure engines. UNITED AIRCRAFT CORPORATION. Dec. 22, 1937, No. 35483. Convention date, Aug. 14. [Class 122 (iii)] [Also in Group XXVII] Engines with groups of radial, multiple cylinders connected to cranks by master-rods and subsidiary link rods have the master rods and/or the cranks so arranged as to reduce vibrations due to harmonics of the torque variation. The groups are arranged so that their vibrations balance out or neutralize. In the arrangement shown in Fig. 3, the cylinders of each group are staggered with respect to the cylinders in the adjacent group. The cranks of the adjacent groups are arranged oppositely, with their master rods 22, 34 respectively as nearly as possible in coincidence. The harmonic components of the torque curves of the respective groups when added together result in a reduction of the exciting vibratory forces. In an arrangement such as shown in Fig. 2, the master rods may remain as shown, and one of the crankpins moved through 180 degrees to bring it into axial alignment with the other crank pin.
GB35483/37A 1937-08-14 1937-12-22 Improvements in or relating to engines and method of reducing vibrations therein Expired GB511941A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US511941XA 1937-08-14 1937-08-14

Publications (1)

Publication Number Publication Date
GB511941A true GB511941A (en) 1939-08-28

Family

ID=21969881

Family Applications (1)

Application Number Title Priority Date Filing Date
GB35483/37A Expired GB511941A (en) 1937-08-14 1937-12-22 Improvements in or relating to engines and method of reducing vibrations therein

Country Status (2)

Country Link
FR (1) FR840744A (en)
GB (1) GB511941A (en)

Also Published As

Publication number Publication date
FR840744A (en) 1939-05-03

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