GB524143A - The operation of hinged structures by direct action upon the hinge - Google Patents

The operation of hinged structures by direct action upon the hinge

Info

Publication number
GB524143A
GB524143A GB37677/38A GB3767738A GB524143A GB 524143 A GB524143 A GB 524143A GB 37677/38 A GB37677/38 A GB 37677/38A GB 3767738 A GB3767738 A GB 3767738A GB 524143 A GB524143 A GB 524143A
Authority
GB
United Kingdom
Prior art keywords
hinge
hinges
operated
hinged
limb
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
GB37677/38A
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 GB37677/38A priority Critical patent/GB524143A/en
Publication of GB524143A publication Critical patent/GB524143A/en
Expired legal-status Critical Current

Links

Classifications

    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D3/00—Hinges with pins
    • E05D3/06—Hinges with pins with two or more pins
    • E05D3/10—Hinges with pins with two or more pins with non-parallel pins
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/16—Fairings movable in conjunction with undercarriage elements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00—Application of doors, windows, wings or fittings thereof
    • E05Y2900/50—Application of doors, windows, wings or fittings thereof for vehicles
    • E05Y2900/502—Application of doors, windows, wings or fittings thereof for vehicles for aircraft or spacecraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Hinges (AREA)

Abstract

524,143. Hinges. HUDSON, R. J. H. Dec. 28, 1938, No. 37677. [Class 65 (ii)] A hinge for doors &c. which swing in a curved path about a vertical axis, such as the hinged parts of aircraft, comprises two butt parts 1, 4 fixed to the relatively movable parts and two flaps 2, 3 hinged to the butts and to each other, an axis of the hinge pins a, b, c meeting at a point P on the vertical axis v. The hinge may be operated by power applied to the pin b, as by the telescopic jack 6, Fig. 3A, connecting a pair of hinges. The hinge is concealed in a recess between frame and door, as shown in Fig. 5B. In another form, two or more hinges are operated by screw and nut mechanism connecting them, and one flap 2 may form one limb of a bell-crank lever, the other limb of which engages the operating means. In another form, the hinges are operated through gearing from the retractable undercarriage of aircraft.
GB37677/38A 1938-12-28 1938-12-28 The operation of hinged structures by direct action upon the hinge Expired GB524143A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB37677/38A GB524143A (en) 1938-12-28 1938-12-28 The operation of hinged structures by direct action upon the hinge

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB37677/38A GB524143A (en) 1938-12-28 1938-12-28 The operation of hinged structures by direct action upon the hinge

Publications (1)

Publication Number Publication Date
GB524143A true GB524143A (en) 1940-07-31

Family

ID=10398189

Family Applications (1)

Application Number Title Priority Date Filing Date
GB37677/38A Expired GB524143A (en) 1938-12-28 1938-12-28 The operation of hinged structures by direct action upon the hinge

Country Status (1)

Country Link
GB (1) GB524143A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3791073A (en) * 1972-04-28 1974-02-12 Boeing Co Aircraft door with moving hinge line
EP0267876A2 (en) * 1986-11-13 1988-05-18 Ateliers de Constructions Mecaniques de Vevey S.A. Door hinge
US4854010A (en) * 1987-11-20 1989-08-08 The Boeing Company Hinge mechanism for aircraft door
WO1999016658A1 (en) * 1997-09-30 1999-04-08 M & C Corporation Vehicle closure hinge
US6314615B1 (en) 1997-09-30 2001-11-13 Tiete O. Wolda Closure hinge
US6447043B1 (en) 2001-01-09 2002-09-10 M & C Corporation Vehicle closure assembly with hinge
CN102787772A (en) * 2011-08-05 2012-11-21 薛广振 Space hinge
CN108533106A (en) * 2018-05-22 2018-09-14 大连金蝴蝶科技有限公司 A kind of latent hinged flap of the V-shaped arrangement of shaft

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3791073A (en) * 1972-04-28 1974-02-12 Boeing Co Aircraft door with moving hinge line
EP0267876A2 (en) * 1986-11-13 1988-05-18 Ateliers de Constructions Mecaniques de Vevey S.A. Door hinge
EP0267876A3 (en) * 1986-11-13 1988-09-21 Ateliers de Constructions Mecaniques de Vevey S.A. Door hinge
US4854010A (en) * 1987-11-20 1989-08-08 The Boeing Company Hinge mechanism for aircraft door
WO1999016658A1 (en) * 1997-09-30 1999-04-08 M & C Corporation Vehicle closure hinge
US6314615B1 (en) 1997-09-30 2001-11-13 Tiete O. Wolda Closure hinge
US6447043B1 (en) 2001-01-09 2002-09-10 M & C Corporation Vehicle closure assembly with hinge
CN102787772A (en) * 2011-08-05 2012-11-21 薛广振 Space hinge
CN108533106A (en) * 2018-05-22 2018-09-14 大连金蝴蝶科技有限公司 A kind of latent hinged flap of the V-shaped arrangement of shaft

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