GB721530A - Improvements in boats - Google Patents

Improvements in boats

Info

Publication number
GB721530A
GB721530A GB562851A GB562851A GB721530A GB 721530 A GB721530 A GB 721530A GB 562851 A GB562851 A GB 562851A GB 562851 A GB562851 A GB 562851A GB 721530 A GB721530 A GB 721530A
Authority
GB
United Kingdom
Prior art keywords
wings
pins
tail
glider
boat
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
GB562851A
Inventor
Arthur Gouge
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.)
SAUNDERS ROE Ltd
Original Assignee
SAUNDERS ROE Ltd
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 SAUNDERS ROE Ltd filed Critical SAUNDERS ROE Ltd
Priority to GB562851A priority Critical patent/GB721530A/en
Publication of GB721530A publication Critical patent/GB721530A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C35/00—Flying-boats; Seaplanes
    • B64C35/005—Flying-boats; Seaplanes with propellers, rudders or brakes acting in the water

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Earth Drilling (AREA)

Abstract

721,530. Glider-boats. SAUNDERS-ROE, Ltd. March 5, 1952, [March 8, 1951], No. 5628/51. Class 4. A glider, Fig. 1, has for its body a boat 10 furnished with a motor driven propeller 15, and is provided with detachable wings 18 and tail boom 19, and has a towing loop 100 at the nose. The tail boom is attached as shown in Fig. 5, by upper and lower fittings 22 and 24 engaging pins 23 and 25 respectively. The hooks 26 which normally lock the pins, may be racked by movement of toggles 28, which is effected by pushing the rod 35. A similar arrangement is used to detachably secure the wings to the body, torque tubes connecting the mechanisms so that one rod serves to control the release of all the pins. The control pin connections for the control surfaces of the wings and tail end in forked links which readily pull away. Another means of detaching the wings and tail is by explosives. In the Provisional Specification the boat may form part of an autogiro.
GB562851A 1951-03-08 1951-03-08 Improvements in boats Expired GB721530A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB562851A GB721530A (en) 1951-03-08 1951-03-08 Improvements in boats

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB562851A GB721530A (en) 1951-03-08 1951-03-08 Improvements in boats

Publications (1)

Publication Number Publication Date
GB721530A true GB721530A (en) 1955-01-05

Family

ID=9799652

Family Applications (1)

Application Number Title Priority Date Filing Date
GB562851A Expired GB721530A (en) 1951-03-08 1951-03-08 Improvements in boats

Country Status (1)

Country Link
GB (1) GB721530A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2942814A (en) * 1956-01-09 1960-06-28 Hans U Schuerch Attachment apparatus
US5150858A (en) * 1989-03-11 1992-09-29 British Aerospace Public Limited Company Jettisonable aerodynamic control surfaces

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2942814A (en) * 1956-01-09 1960-06-28 Hans U Schuerch Attachment apparatus
US5150858A (en) * 1989-03-11 1992-09-29 British Aerospace Public Limited Company Jettisonable aerodynamic control surfaces

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