GB191103334A - A Combined Magneto-ignition Gear for Internal Combustion Engines and Wireless Telegraphy Apparatus, particularly applicable to Aerial Vessels. - Google Patents

A Combined Magneto-ignition Gear for Internal Combustion Engines and Wireless Telegraphy Apparatus, particularly applicable to Aerial Vessels.

Info

Publication number
GB191103334A
GB191103334A GB191103334DA GB191103334A GB 191103334 A GB191103334 A GB 191103334A GB 191103334D A GB191103334D A GB 191103334DA GB 191103334 A GB191103334 A GB 191103334A
Authority
GB
United Kingdom
Prior art keywords
aerial
internal combustion
combustion engines
particularly applicable
condenser
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
Inventor
Murray Fraser Sueter
Frederick Lewis Maitla Boothby
Halliday Gunning Paterson
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
Application granted granted Critical
Publication of GB191103334A publication Critical patent/GB191103334A/en
Expired legal-status Critical Current

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  • Ignition Installations For Internal Combustion Engines (AREA)

Abstract

3334. Sueter, M. F., Boothby, F. L. M., and Paterson, H. G. Feb. 9. Systems, electric.-The ignition apparatus of an internal-combustion engine, particularly those used on aerial vessels, is used to produce electric oscillations for signalling. A magneto a or other generator is connected to the primary of a transformer b, whose secondary is connected to a condenser c. One side of the condenser is connected to an adjustable spark gap g and a distributor h through the primary d of a transformer, whose secondary e is connected to the aerial f. The distributor completes the circuit either through the ignition plugs i or a dummy plug i<1>, an earth return being used to the other side of the condenser. Signalling is effected by a key k arranged to short circuit the secondary e or a part thereof, or to open the aerial circuit.
GB191103334D 1911-02-09 1911-02-09 A Combined Magneto-ignition Gear for Internal Combustion Engines and Wireless Telegraphy Apparatus, particularly applicable to Aerial Vessels. Expired GB191103334A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191103334T 1911-02-09

Publications (1)

Publication Number Publication Date
GB191103334A true GB191103334A (en) 1912-01-11

Family

ID=32365726

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191103334D Expired GB191103334A (en) 1911-02-09 1911-02-09 A Combined Magneto-ignition Gear for Internal Combustion Engines and Wireless Telegraphy Apparatus, particularly applicable to Aerial Vessels.

Country Status (1)

Country Link
GB (1) GB191103334A (en)

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