GB326757A - Improvements in amphibian aircraft - Google Patents

Improvements in amphibian aircraft

Info

Publication number
GB326757A
GB326757A GB3249329A GB3249329A GB326757A GB 326757 A GB326757 A GB 326757A GB 3249329 A GB3249329 A GB 3249329A GB 3249329 A GB3249329 A GB 3249329A GB 326757 A GB326757 A GB 326757A
Authority
GB
United Kingdom
Prior art keywords
tube
bearing
rudder
secured
spring
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
GB3249329A
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 GB3249329A priority Critical patent/GB326757A/en
Publication of GB326757A publication Critical patent/GB326757A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C35/00Flying-boats; Seaplanes
    • B64C35/005Flying-boats; Seaplanes with propellers, rudders or brakes acting in the water

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Axle Suspensions And Sidecars For Cycles (AREA)
  • Vibration Dampers (AREA)

Abstract

326,757. Short, A. E., and Short, H. O. June 5, 1929. Divided on 327,060. Steering; skid; shock-absorbers, applications of. -The water rudder of an amphibian extends below the buoyant body and is spring mounted to act as a skid and is connected by a telescopic member to the means for actuating the air rudder. A light casting 1 having a, shoe 30 is provided with lugs 35, 36 to which a vertical tube 37 is secured, this tube being capable of turning and sliding in bearings 38, 39 on a member 40 secured to the stem of the buoyant body. A spring 41 surrounds the tube 37 between the bearing 38 and the lug 35 to take landing shocks, and a lighter spring 42, arranged inside the tube between an abutment therein and the closed end of a sleeve in the bearing 39, takes the rebound. The upper end of the tube 37 is connected by a universal joint 50 to a member 51 adapted to telescope in a member 52 of oval section which is connected by a second universal joint 53 to a tubular member 56 mounted in a bearing 57 on the fuselage. The member 56 has arms connected by wires 62 to the air rudder. Instead of being within the fuselage, as shown, the arms may be connected to the member 56 below the bearing 57. The rudder, instead of being cast, may be built up with two side plates riveted to spacing members to which the lugs 35, 36 are secured, and to a lower broadened member to which an additional shoe is. fixed.
GB3249329A 1929-06-05 1929-06-05 Improvements in amphibian aircraft Expired GB326757A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3249329A GB326757A (en) 1929-06-05 1929-06-05 Improvements in amphibian aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3249329A GB326757A (en) 1929-06-05 1929-06-05 Improvements in amphibian aircraft

Publications (1)

Publication Number Publication Date
GB326757A true GB326757A (en) 1930-03-20

Family

ID=10339436

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3249329A Expired GB326757A (en) 1929-06-05 1929-06-05 Improvements in amphibian aircraft

Country Status (1)

Country Link
GB (1) GB326757A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112829924A (en) * 2020-12-31 2021-05-25 上海机电工程研究所 Retractable duck steering mechanism
CN113306717A (en) * 2021-07-09 2021-08-27 湖北航特航空飞行器有限公司 Fast advancing rudder of large amphibious aircraft

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112829924A (en) * 2020-12-31 2021-05-25 上海机电工程研究所 Retractable duck steering mechanism
CN112829924B (en) * 2020-12-31 2022-12-13 上海机电工程研究所 Retractable duck steering mechanism
CN113306717A (en) * 2021-07-09 2021-08-27 湖北航特航空飞行器有限公司 Fast advancing rudder of large amphibious aircraft
CN113306717B (en) * 2021-07-09 2022-11-22 安徽维统航空装备有限公司 Fast advancing rudder of large amphibious aircraft

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