GB462411A - Improvements in controlling the output of internal combustion engines of flying machines - Google Patents

Improvements in controlling the output of internal combustion engines of flying machines

Info

Publication number
GB462411A
GB462411A GB1465/36A GB146536A GB462411A GB 462411 A GB462411 A GB 462411A GB 1465/36 A GB1465/36 A GB 1465/36A GB 146536 A GB146536 A GB 146536A GB 462411 A GB462411 A GB 462411A
Authority
GB
United Kingdom
Prior art keywords
parts
controlling
outer part
output
internal combustion
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
GB1465/36A
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.)
Kreditpruefung Ges GmbH
MAX SCHEIDING
Original Assignee
Kreditpruefung Ges GmbH
MAX SCHEIDING
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 Kreditpruefung Ges GmbH, MAX SCHEIDING filed Critical Kreditpruefung Ges GmbH
Publication of GB462411A publication Critical patent/GB462411A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D9/00—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
    • F02D9/08—Throttle valves specially adapted therefor; Arrangements of such valves in conduits
    • F02D9/10—Throttle valves specially adapted therefor; Arrangements of such valves in conduits having pivotally-mounted flaps
    • F02D9/1005—Details of the flap
    • F02D9/102—Details of the flap the flap having movable parts fixed onto it
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D9/00—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
    • F02D9/02—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits concerning induction conduits
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D9/00—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
    • F02D9/02—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits concerning induction conduits
    • F02D2009/0201—Arrangements; Control features; Details thereof
    • F02D2009/0279—Throttle valve control for intake system with two parallel air flow paths, each controlled by a throttle, e.g. a resilient flap disposed on a throttle

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Catching Or Destruction (AREA)

Abstract

462,411. Spray carburetters. GES. FUR KREDITPRUFUNG GES., and SCHEIDING, M. Jan. 16, 1936, No. 1465. Convention date, Jan. 19, 1935. [Class 7 (iii)] A throttle for an aircraft engine is formed in two parts the inner part, such as a flat disc, being opened before the outer part 4, which may be a flat ring, to provide sensitive control for the engine on or near the ground. The outer part 4 may have a combined hand and automatic control abutments which can be disengaged being provided to permit the automatic control to be overridden, during starting for example, and both parts to be opened on the ground. An idling byepass is formed through the thickness of the outer part 4 to the slit between the parts.
GB1465/36A 1935-01-19 1936-01-16 Improvements in controlling the output of internal combustion engines of flying machines Expired GB462411A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE462411X 1935-01-19

Publications (1)

Publication Number Publication Date
GB462411A true GB462411A (en) 1937-03-09

Family

ID=6539979

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1465/36A Expired GB462411A (en) 1935-01-19 1936-01-16 Improvements in controlling the output of internal combustion engines of flying machines

Country Status (1)

Country Link
GB (1) GB462411A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0262883A1 (en) * 1986-09-29 1988-04-06 Mitsubishi Denki Kabushiki Kaisha Throttling apparatus for an automobile
WO1989002981A1 (en) * 1987-10-02 1989-04-06 Siemens Aktiengesellschaft Throttle assembly
EP2977602A3 (en) * 2014-07-04 2016-06-01 Hanking Power Technology Co., Ltd. Intake manifold having variable diameters

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0262883A1 (en) * 1986-09-29 1988-04-06 Mitsubishi Denki Kabushiki Kaisha Throttling apparatus for an automobile
WO1989002981A1 (en) * 1987-10-02 1989-04-06 Siemens Aktiengesellschaft Throttle assembly
EP2977602A3 (en) * 2014-07-04 2016-06-01 Hanking Power Technology Co., Ltd. Intake manifold having variable diameters

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