GB116364A - Improvements in Balancing Arrangements for Aircraft. - Google Patents

Improvements in Balancing Arrangements for Aircraft.

Info

Publication number
GB116364A
GB116364A GB8398/17A GB839817A GB116364A GB 116364 A GB116364 A GB 116364A GB 8398/17 A GB8398/17 A GB 8398/17A GB 839817 A GB839817 A GB 839817A GB 116364 A GB116364 A GB 116364A
Authority
GB
United Kingdom
Prior art keywords
balancing
aircraft
rudder
tail
rings
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
GB8398/17A
Inventor
Hugh Robertson Ritchie
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
Priority to GB8398/17A priority Critical patent/GB116364A/en
Publication of GB116364A publication Critical patent/GB116364A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders

Abstract

116,364. Ritchie, H. R. June 12, 1917. Steering and balancing.-In aeroplanes in which the tail-surfaces are rotated about a longitudinal axis for lateral balancing, the tail-plane and elevator b are carried by rings a rotatable on rings c fixed to the body, the rotation being effected by connexions to the rudder-bar, which for this purpose is mounted to oscillate in a vertical plane, in addition to the usual fore-and-aft oscillation for controlling the rudder. According to the Provisional Specification, the elevator alone may be rotatably mounted.
GB8398/17A 1917-06-12 1917-06-12 Improvements in Balancing Arrangements for Aircraft. Expired GB116364A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8398/17A GB116364A (en) 1917-06-12 1917-06-12 Improvements in Balancing Arrangements for Aircraft.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8398/17A GB116364A (en) 1917-06-12 1917-06-12 Improvements in Balancing Arrangements for Aircraft.

Publications (1)

Publication Number Publication Date
GB116364A true GB116364A (en) 1918-06-12

Family

ID=32670664

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8398/17A Expired GB116364A (en) 1917-06-12 1917-06-12 Improvements in Balancing Arrangements for Aircraft.

Country Status (1)

Country Link
GB (1) GB116364A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112249298A (en) * 2020-10-10 2021-01-22 郑州海王实业有限公司 Efficient ground effect wing ship elevator counterweight device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112249298A (en) * 2020-10-10 2021-01-22 郑州海王实业有限公司 Efficient ground effect wing ship elevator counterweight device

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