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GB1085649A - Improvements in and relating to reduction gear construction - Google Patents

Improvements in and relating to reduction gear construction

Info

Publication number
GB1085649A
GB1085649A GB18331/66A GB1833166A GB1085649A GB 1085649 A GB1085649 A GB 1085649A GB 18331/66 A GB18331/66 A GB 18331/66A GB 1833166 A GB1833166 A GB 1833166A GB 1085649 A GB1085649 A GB 1085649A
Authority
GB
United Kingdom
Prior art keywords
engine
reduction gear
gear unit
propeller
relating
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
GB18331/66A
Inventor
Leonard Louis Gaubis
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.)
RTX 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
Priority to GB18331/66A priority Critical patent/GB1085649A/en
Publication of GB1085649A publication Critical patent/GB1085649A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H37/00—Combinations of mechanical gearings, not provided for in groups F16H1/00 - F16H35/00
    • F16H37/02—Combinations of mechanical gearings, not provided for in groups F16H1/00 - F16H35/00 comprising essentially only toothed or friction gearings
    • F16H37/04—Combinations of toothed gearings only
    • F16H37/041—Combinations of toothed gearings only for conveying rotary motion with constant gear ratio
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H1/00—Toothed gearings for conveying rotary motion
    • F16H1/02—Toothed gearings for conveying rotary motion without gears having orbital motion
    • F16H1/04—Toothed gearings for conveying rotary motion without gears having orbital motion involving only two intermeshing members
    • F16H1/06—Toothed gearings for conveying rotary motion without gears having orbital motion involving only two intermeshing members with parallel axes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H1/00—Toothed gearings for conveying rotary motion
    • F16H1/28—Toothed gearings for conveying rotary motion with gears having orbital motion

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Retarders (AREA)

Abstract

1,085,649. Driving aircraft propellers. UNITED AIRCRAFT CORPORATION. April 27, 1966, No. 18331/66. Heading B7G. [Also in Division F2] In an aircraft power plant, Fig. 1, a gas turbine or piston engine 12 drives a variable pitch propeller 18 through a clutch and a reduction gear unit 16 including an epicyclic reduction stage 92, Fig. 2, a cross-shaft 26 from the gear unit 16 allowing the engine 12 to drive a second propeller similar to 18 or a second engine to drive the propeller 18 through the reduction gear unit 16 on failure of the engine 12.
GB18331/66A 1966-04-27 1966-04-27 Improvements in and relating to reduction gear construction Expired GB1085649A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB18331/66A GB1085649A (en) 1966-04-27 1966-04-27 Improvements in and relating to reduction gear construction

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB18331/66A GB1085649A (en) 1966-04-27 1966-04-27 Improvements in and relating to reduction gear construction

Publications (1)

Publication Number Publication Date
GB1085649A true GB1085649A (en) 1967-10-04

Family

ID=10110646

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18331/66A Expired GB1085649A (en) 1966-04-27 1966-04-27 Improvements in and relating to reduction gear construction

Country Status (1)

Country Link
GB (1) GB1085649A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1951427A1 (en) * 1968-10-28 1970-05-14 North American Rockwell Reduction gear

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1951427A1 (en) * 1968-10-28 1970-05-14 North American Rockwell Reduction gear

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