[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

US2494347A - Roller type hinge - Google Patents

Roller type hinge Download PDF

Info

Publication number
US2494347A
US2494347A US590492A US59049245A US2494347A US 2494347 A US2494347 A US 2494347A US 590492 A US590492 A US 590492A US 59049245 A US59049245 A US 59049245A US 2494347 A US2494347 A US 2494347A
Authority
US
United States
Prior art keywords
hinge
roller
rollers
elements
track
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 - Lifetime
Application number
US590492A
Inventor
Arthur F Matthews
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.)
Curtiss Wright Corp
Original Assignee
Curtiss Wright Corp
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 Curtiss Wright Corp filed Critical Curtiss Wright Corp
Priority to US590492A priority Critical patent/US2494347A/en
Application granted granted Critical
Publication of US2494347A publication Critical patent/US2494347A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/08Inspection panels for power plants
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D1/00Pinless hinges; Substitutes for hinges
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D1/00Pinless hinges; Substitutes for hinges
    • E05D1/04Pinless hinges; Substitutes for hinges with guide members shaped as circular arcs
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00Suspension arrangements for wings
    • E05D15/40Suspension arrangements for wings supported on arms movable in vertical planes
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING 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
    • E05Y2201/00Constructional elements; Accessories therefor
    • E05Y2201/60Suspension or transmission members; Accessories therefor
    • E05Y2201/622Suspension or transmission members elements
    • E05Y2201/688Rollers
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING 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
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/50Application of doors, windows, wings or fittings thereof for vehicles
    • E05Y2900/502Application of doors, windows, wings or fittings thereof for vehicles for aircraft or spacecraft

Definitions

  • This invention relates generally to hinges, and is particularly directed to improvements in roller hinges which will render them of greater utility.
  • hinged closures or doors In airplane fuselages, engine nacelles and other curved surfaces, it is often desired to provide hinged closures or doors for various purposes. In the design of hinges for such purposes, it is desired to prevent interference of adjacent edges along the hinged joint, and at the same time provide a smooth uninterrupted surface offering little aerodynamic resistance.
  • the common type of individual hinge or continuous piano hinge is limited in its application to a condition in which the hinge line is rectilinear and also lies within or on the surface of the panel or skin. A curved surface obviously does not lend itself readily to the installation of such a hinge.
  • Another object is to provide a hinge in which the hinge axis may be located at some advantageous point outside the physical limits of the hinge structure, so that the utility thereof may be greatly enhanced.
  • Still another object is to provide a hinge which is remarkably well adapted for general use where a door or movable panel is desired to be provided in a body having a curved contour.
  • a further object is to provide a hinge capable of use in an installation in which the parting line is required to be other than rectilinear and in which edge interference must be eliminated for free hinging movement.
  • a still further object is to provide a hinge which is useful as a structural member for resisting tension and bending loads which may be imposed thereon. Another object is to provide a hinge which will permit the ready detachment of the door or other hinged part without first necessitating the disassembly or removal of any securing elements, such as bolts, screws or the like. An additional object is to provide a hinge structure which is particularly well adapted for use in aircraft, wherein flush joints and otherwise aerodynamically clean, smooth contours are greatly to be desired. Other objects will appear hereinafter.
  • one of the cooperating hinge elements comprises a set of guide rollers and the other cooperating hinge element is a curved track element cooperating with and guided by the guide rollers, in a manner to be described more particularly hereinafter.
  • Figure 1 is a perspective view of an aircraft engine nacelle with an access door hinged thereto employing the novel type of hinge structure according to the present invention
  • Figure 2 is a cross section on a greatly enlarged scale of a portion of Figure 1
  • Figures 3 and 4 are views taken along the lines 3-3 and 44, respectively, of Figure 2
  • Figure 5 is a perspective view, on the same scale as Figure 2, with parts removed for clarity in illustration.
  • each hinge assembly includes a guide portion l3 and a track portion I4.
  • Each track portion is curved as shown, preferably in a plane and preferably having a constant radius of curvature (i. e. each operative edge of the track defining the arc of a circle, as shown in greater detail hereafter).
  • the three assemblies l2 need not have the same radii of curvature, but the center of curvature for all the track elements should lie on a single straight line, which is the hinge axis and is an imaginary line in space indicated at A-A, exterior to the door 10 and the nacelle H.
  • the guide portion l3 includes two spaced bracket members 16 disposed parallel to each other and affixed to the nacelle I i such as by riveting, welding or the like.
  • the brackets it are suitably apertured for l the reception of thru-shafts.
  • three such shafts MA, MB and NC are indicated as being arranged in a triangular pattern, the purpose of which will appear presently.
  • a pair of roller elements l8 separated by a spacer element or collar l9 are operatively carried on each shaft, and the assembly thereof is maintained by the provision of a head 2!! at one end and a nut or collar 2! at the opposite end thereof.
  • the roller elements are circumferentially grooved, so that they may serve as guides in addition to their function as friction reducing elements.
  • bracket members I 6 there is arranged a spaced pair of hinge track members 22, and as illustrated these members 22 are formed as arcuate elements having substantially parallel bounding faces. These tracks 22 are attached to the movable panel or door In by means of suitable flanges 23. Spacing of the stopping such travel is made.
  • tracks is maintained by one or more shouldered elements 24 spaced along the arcuate portion thereof such that parallelism therebetween is assured.
  • the spacer elements 24 have projecting end portions as indicated in Figures 4 and 5, which are up-set into a countersunk depression so as to lie flush with the outer surface of the tracks.
  • the tracks22 are arranged to lie between and be embracedby the hinge bracket members It.
  • the spacing of each pair of roller elements IB is exactly equal to the track spacing such that, at the time the tracks and brackets are placed in operative assembly, the tracks will ride down in the grooved portions of the roller elements 3 and be guided and supported thereby.
  • FIG. 1 and 2 illustrate to advantage the latter named condition and shows how the present type of roller hinge will obviate door edge clearance difliculties and yet maintain a clean outer contour when the same is closed.
  • the true hinge axis A is exteriorly located with respect to the nacelle body shown.
  • the edge portions of the tracks or moving hinge elements 22 may correspond to some other curve, so that the effective hinge axis A may move in space as the door is opened or closed.
  • the curvilinear trend thereof may be that of an ellipse, a spiral or a sine curve.
  • the possible combinations are many so that the hinged door or panel may be given a bodily movement which will permit it to clear most adjacent obstacles.
  • hinge member which forms the subject matter of the present description is illustrated as applicable to the installation condition in which the hinge axis is generall horizontal in extent, it should be understood that the structural revisions required to permit the use of this type hinge with its hinge axis set in a vertical position are not such as will depart in any great materiality from the broad principle involved.
  • a device to provide for relative hinging movement of two elements comprising roller means for one element and curved track means for the other element, said roller means comprising spaced sets of three rollers each, with each roller having a groove in the circumferential face thereof, said track means comprising a circularly curved rail for each set of rollers with one curved edge of each rail engaging in the grooves of two rollers of one set and with the opposite curved edge of said rail engaging in the groove of the third roller of said set, said rails being spaced at one end from said other element to provide for their disengagement from said rollers upon continuation of hinging movement in one direction, and said track means further comprising a part connecting said rails intermediate the ends thereof and adapted to pass between said two rollers and said third roller of each set during hinging movement.
  • a device to provide for relative hinging movement of two elements comprising roller means for one element and curved track means for the other element, said roller means comprising spaced sets of three rollers each, with the corresponding rollers of the several sets in coaxial relation, said track means comprising a circularly curved rail for each set of rollers with one curved edge of each rail engaging circumferential portions of two rollers of one set and with the opposite curved edge of the rail engaging a circumferential portion of the third roller of said set, said curved rail edge and said circumferential portions of the rollers having cooperating groove and groove engaging surfaces, and said track means further comprising a part connecting said rails intermediate the ends thereof and adapted to pass between said two rollers and said third roller of each set during hinging movement.
  • a device to provide for relative hinging movement of two elements comprising roller means for one element and curved track means for the other element, said roller means comprising spaced sets of three rollers each, with the corresponding rollers of the several sets in coaxial relation, said track means comprising a circularly curved rail for each set of rollers with one curved edge of each rail engaging circumferential portions of two rollers of one set and with the opposite curved edge of the rail engaging a circumferential portion of the third roller of said set, said curved rail edges and said circumferential portions of the rollers having cooperating groove and groove engaging surfaces, and said rails being spaced at one end from said other element to provide for their disengagement from said rollers upon continuation of hinging movement in one direction.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Support Devices For Sliding Doors (AREA)

Description

,1 A. F. MATTHEWS 2,494,347
ROLLER TYPE HINGE Filed April 26, 1945 2 Shets-Sheet 1 v INVENTOR. ARTHUR s MATTHEWS.
BY? F ATTOR BY 7 Jan. 10, 1950 A. F. MATTHEWS 2,494,347
ROLLER TYPE HINGE Filed April 26, 1945 2 SheetsSheet '2 INVENTOR.
ARTHUR F. MATTHEWS Patented Jan. 10, 1950 ROLLER TYPE HINGE Arthur F. Matthews, Ferguson, Mo., assignor to Curtiss-Wright Corporation, a corporation of Delaware Application April 26, 1945, Serial No. 590,492
3 Claims.
This invention relates generally to hinges, and is particularly directed to improvements in roller hinges which will render them of greater utility.
In airplane fuselages, engine nacelles and other curved surfaces, it is often desired to provide hinged closures or doors for various purposes. In the design of hinges for such purposes, it is desired to prevent interference of adjacent edges along the hinged joint, and at the same time provide a smooth uninterrupted surface offering little aerodynamic resistance. The common type of individual hinge or continuous piano hinge is limited in its application to a condition in which the hinge line is rectilinear and also lies within or on the surface of the panel or skin. A curved surface obviously does not lend itself readily to the installation of such a hinge.
It is therefore an object of this invention to provide a hinge embodying novel features which will permit the use thereof in a wide variety of applications where the standard type of leaf hinge will not serve in a satisfactory manner. Another object is to provide a hinge in which the hinge axis may be located at some advantageous point outside the physical limits of the hinge structure, so that the utility thereof may be greatly enhanced. Still another object is to provide a hinge which is remarkably well adapted for general use where a door or movable panel is desired to be provided in a body having a curved contour. A further object is to provide a hinge capable of use in an installation in which the parting line is required to be other than rectilinear and in which edge interference must be eliminated for free hinging movement. A still further object is to provide a hinge which is useful as a structural member for resisting tension and bending loads which may be imposed thereon. Another object is to provide a hinge which will permit the ready detachment of the door or other hinged part without first necessitating the disassembly or removal of any securing elements, such as bolts, screws or the like. An additional object is to provide a hinge structure which is particularly well adapted for use in aircraft, wherein flush joints and otherwise aerodynamically clean, smooth contours are greatly to be desired. Other objects will appear hereinafter.
These objects are accomplished by means of a hinge construction in Which one of the cooperating hinge elements comprises a set of guide rollers and the other cooperating hinge element is a curved track element cooperating with and guided by the guide rollers, in a manner to be described more particularly hereinafter.
The invention may be more readily understood by reference to the accompanying drawings, in which: Figure 1 is a perspective view of an aircraft engine nacelle with an access door hinged thereto employing the novel type of hinge structure according to the present invention; Figure 2 is a cross section on a greatly enlarged scale of a portion of Figure 1; Figures 3 and 4 are views taken along the lines 3-3 and 44, respectively, of Figure 2; Figure 5 is a perspective view, on the same scale as Figure 2, with parts removed for clarity in illustration.
Referring now to Figure 1, the hinge construction according to the present invention is shown as installed on a door It providing access to the interior of an aircraft engine nacelle I I. In the present instance three hinge assemblies IZ-ai-e shown, although a greater number could be provided. Each assembly includes a guide portion l3 and a track portion I4. Each track portion is curved as shown, preferably in a plane and preferably having a constant radius of curvature (i. e. each operative edge of the track defining the arc of a circle, as shown in greater detail hereafter). The three assemblies l2 need not have the same radii of curvature, but the center of curvature for all the track elements should lie on a single straight line, which is the hinge axis and is an imaginary line in space indicated at A-A, exterior to the door 10 and the nacelle H.
The details of the hinge assembly are indicated more clearly in Figures 2, 3 and 4. The guide portion l3 includes two spaced bracket members 16 disposed parallel to each other and affixed to the nacelle I i such as by riveting, welding or the like. The brackets it are suitably apertured for l the reception of thru-shafts. In the form shown, three such shafts MA, MB and NC are indicated as being arranged in a triangular pattern, the purpose of which will appear presently. A pair of roller elements l8 separated by a spacer element or collar l9 are operatively carried on each shaft, and the assembly thereof is maintained by the provision of a head 2!! at one end and a nut or collar 2! at the opposite end thereof. The roller elements are circumferentially grooved, so that they may serve as guides in addition to their function as friction reducing elements.
In conjunction with the bracket members I 6, there is arranged a spaced pair of hinge track members 22, and as illustrated these members 22 are formed as arcuate elements having substantially parallel bounding faces. These tracks 22 are attached to the movable panel or door In by means of suitable flanges 23. Spacing of the stopping such travel is made.
tracks is maintained by one or more shouldered elements 24 spaced along the arcuate portion thereof such that parallelism therebetween is assured. The spacer elements 24 have projecting end portions as indicated in Figures 4 and 5, which are up-set into a countersunk depression so as to lie flush with the outer surface of the tracks. As shown, the tracks22 are arranged to lie between and be embracedby the hinge bracket members It. Furthermore, the spacing of each pair of roller elements IB is exactly equal to the track spacing such that, at the time the tracks and brackets are placed in operative assembly, the tracks will ride down in the grooved portions of the roller elements 3 and be guided and supported thereby.
It may now be seen that the throw or hinging travel of the present device is determined by the amount of curvature given the track elements 22 while the smooth, substantially frictionless and interference free movement will be governed by the location of the grooved roller elements I8 with respect thereto. Further, on examination of Figure 2, it can be seen how the present hinge functions such that a smooth exterior surface is preserved between nacelle II and door It when the same is in closed position (full line), and such that the adjacent edges of the latter parts, when opened (dot-dash line), are separated to obviate interference or binding. It is also clearly shown that the true hinge axis, indicated at A in Figure 2 and at A-A in Figure 1, may be located in space. This latter feature is particularly advantageous in the case of hinge mounting a door or panel having a pronounced curvature in two directions. Figures 1 and 2 illustrate to advantage the latter named condition and shows how the present type of roller hinge will obviate door edge clearance difliculties and yet maintain a clean outer contour when the same is closed. The true hinge axis A is exteriorly located with respect to the nacelle body shown.
A further examination of Figures 2 and 5 will reveal an important advantage found only in a hinge of the present type. It will be noted that the track members 22 roll along on the grooved rollers l3 and that no means for limiting or Thus, if the door I0 is opened sufficiently far, the tracks 22 will become disengaged from the rollers l8 and complete removal thereof is obviously possible. Quick detachability is therefore a feature giving this present hinge a marked superiority over the pin type leaf or plate hinges.
An additional advantage to be gained from this hinge resides in the structural characteristics of the arrangement. Obviously a considerable tension load may be imposed on the hinge since such loading will be distributed substantially equally between the two roller shafts HA and NB. The major portions of any compressive loads will be absorbed along the abutting edges of the structure ll and door H3. Proper selection of proportions and sizes of the several parts and elements of this present hinge is facilitated by its inherent structural arrangement.
While a hinge track having its edge portions corresponding to the arc of a circle has been indicated in the drawings, it is contemplated that the edge portions of the tracks or moving hinge elements 22 may correspond to some other curve, so that the effective hinge axis A may move in space as the door is opened or closed. Thus, the curvilinear trend thereof may be that of an ellipse, a spiral or a sine curve. The possible combinations are many so that the hinged door or panel may be given a bodily movement which will permit it to clear most adjacent obstacles. When other than substantially circular track elements 22 are employed, there must be an alteration made in the geometrical relationship of the roller elements !8, and in some cases additional or movable rollers may be required. Consequently, the circularly curved track elements are preferred.
While the hinge member which forms the subject matter of the present description is illustrated as applicable to the installation condition in which the hinge axis is generall horizontal in extent, it should be understood that the structural revisions required to permit the use of this type hinge with its hinge axis set in a vertical position are not such as will depart in any great materiality from the broad principle involved.
The foregoing description of the invention is intended merely to point out a simple preferred arrangement of parts and elements in a hinge of roller type, but it is to be understood that additions and alterations may be made or become obvious after a study of the same without departing from the spirit and full intended scope of the invention as will be defined by the claims hereinafter appended.
I claim:
l. A device to provide for relative hinging movement of two elements, comprising roller means for one element and curved track means for the other element, said roller means comprising spaced sets of three rollers each, with each roller having a groove in the circumferential face thereof, said track means comprising a circularly curved rail for each set of rollers with one curved edge of each rail engaging in the grooves of two rollers of one set and with the opposite curved edge of said rail engaging in the groove of the third roller of said set, said rails being spaced at one end from said other element to provide for their disengagement from said rollers upon continuation of hinging movement in one direction, and said track means further comprising a part connecting said rails intermediate the ends thereof and adapted to pass between said two rollers and said third roller of each set during hinging movement.
2. A device to provide for relative hinging movement of two elements, comprising roller means for one element and curved track means for the other element, said roller means comprising spaced sets of three rollers each, with the corresponding rollers of the several sets in coaxial relation, said track means comprising a circularly curved rail for each set of rollers with one curved edge of each rail engaging circumferential portions of two rollers of one set and with the opposite curved edge of the rail engaging a circumferential portion of the third roller of said set, said curved rail edge and said circumferential portions of the rollers having cooperating groove and groove engaging surfaces, and said track means further comprising a part connecting said rails intermediate the ends thereof and adapted to pass between said two rollers and said third roller of each set during hinging movement.
3. A device to provide for relative hinging movement of two elements, comprising roller means for one element and curved track means for the other element, said roller means comprising spaced sets of three rollers each, with the corresponding rollers of the several sets in coaxial relation, said track means comprising a circularly curved rail for each set of rollers with one curved edge of each rail engaging circumferential portions of two rollers of one set and with the opposite curved edge of the rail engaging a circumferential portion of the third roller of said set, said curved rail edges and said circumferential portions of the rollers having cooperating groove and groove engaging surfaces, and said rails being spaced at one end from said other element to provide for their disengagement from said rollers upon continuation of hinging movement in one direction.
ARTHUR F. MATTHEWS.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,648,781 Pepin Nov. 8, 1927 2,233,882 Bobek Mar. 4, 1941 FOREIGN PATENTS Number Country Date 654,618 France Nov. 29, 1928
US590492A 1945-04-26 1945-04-26 Roller type hinge Expired - Lifetime US2494347A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US590492A US2494347A (en) 1945-04-26 1945-04-26 Roller type hinge

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US590492A US2494347A (en) 1945-04-26 1945-04-26 Roller type hinge

Publications (1)

Publication Number Publication Date
US2494347A true US2494347A (en) 1950-01-10

Family

ID=24362485

Family Applications (1)

Application Number Title Priority Date Filing Date
US590492A Expired - Lifetime US2494347A (en) 1945-04-26 1945-04-26 Roller type hinge

Country Status (1)

Country Link
US (1) US2494347A (en)

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2666872A (en) * 1950-08-19 1954-01-19 Westinghouse Electric Corp Electric power system for aircraft
US2802478A (en) * 1954-04-21 1957-08-13 Carl B Fritsche Shelter construction
US4530412A (en) * 1984-04-12 1985-07-23 General Motors Corporation Vehicle hood support and secondary latch
US4554700A (en) * 1984-08-16 1985-11-26 Whirlpool Corporation Invisible hinge means for lid and hood of a canister vacuum cleaner
EP0744339A1 (en) * 1995-05-24 1996-11-27 AEROSPATIALE Société Nationale Industrielle Aircraft engine nacelle with a nacelle cowling
FR2768489A1 (en) * 1997-09-12 1999-03-19 Eurocopter France Aerodynamic hinged panel for helicopter engine unit hood
DE10053632A1 (en) * 2000-10-28 2002-05-02 Bayerische Motoren Werke Ag Car boot flap hinge rides curved guide between flap end positions with three-roller slide ensuring guide movement despite unevenness.
US20050023411A1 (en) * 2001-12-13 2005-02-03 Minoru Matsuda Lubricating oil filling structure for an engine
US20110133489A1 (en) * 2009-12-09 2011-06-09 Airbus Operations Sas Aircraft nacelle incorporating a hood closure device that is independent of the locking mechanism
WO2012104561A3 (en) * 2011-02-04 2012-10-26 Aircelle Nacelle with articulated fan casing covers
US20140294581A1 (en) * 2013-03-07 2014-10-02 Rolls-Royce Corporation Gas turbine engine access panel
US20160214729A1 (en) * 2013-09-04 2016-07-28 Snecma Casing structure interposed between the engine and the nacelle having pivoting shroud sectors
FR3040044A1 (en) * 2015-08-12 2017-02-17 Snecma PLATFORM HOOD COMPRISING A HOLDING MEMBER IN SOLIDARIZED POSITION ON THE INSIDE OF THE HOOD
US20180057183A1 (en) * 2016-08-23 2018-03-01 Airbus Helicopters Deutschland GmbH Rotorcraft with cowling able to rotate and translate relative to the fuselage
FR3055313A1 (en) * 2016-08-30 2018-03-02 Safran Nacelles PLATFORM FOR AIRCRAFT TURBOJET ENGINE, AIR INLET AND HYBRID BLOWER HOOD
EP3461744A1 (en) * 2017-09-29 2019-04-03 Airbus Operations S.A.S. Thrust reverser turbofan engine for an aircraft with improved opening
US10494112B2 (en) * 2015-12-22 2019-12-03 Rolls-Royce Deutschland Ltd & Co Kg Engine cowling with three-dimensionally adjustable hinge
US10738521B2 (en) 2017-03-29 2020-08-11 Interlock Usa, Inc. Sliding door roller system
US11274480B2 (en) 2019-10-30 2022-03-15 Interlock Usa, Inc. Sliding door roller and method of installation

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1648781A (en) * 1924-01-24 1927-11-08 Joseph N Pepin Hinge
FR654618A (en) * 1928-05-19 1929-04-09 Articulation system
US2233882A (en) * 1938-01-24 1941-03-04 Bobek William Self-locking concealed hinge

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1648781A (en) * 1924-01-24 1927-11-08 Joseph N Pepin Hinge
FR654618A (en) * 1928-05-19 1929-04-09 Articulation system
US2233882A (en) * 1938-01-24 1941-03-04 Bobek William Self-locking concealed hinge

Cited By (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2666872A (en) * 1950-08-19 1954-01-19 Westinghouse Electric Corp Electric power system for aircraft
US2802478A (en) * 1954-04-21 1957-08-13 Carl B Fritsche Shelter construction
US4530412A (en) * 1984-04-12 1985-07-23 General Motors Corporation Vehicle hood support and secondary latch
US4554700A (en) * 1984-08-16 1985-11-26 Whirlpool Corporation Invisible hinge means for lid and hood of a canister vacuum cleaner
EP0744339A1 (en) * 1995-05-24 1996-11-27 AEROSPATIALE Société Nationale Industrielle Aircraft engine nacelle with a nacelle cowling
FR2734540A1 (en) * 1995-05-24 1996-11-29 Aerospatiale AIRCRAFT ENGINE NACELLE HAVING A NACELLE HOOD
US5755403A (en) * 1995-05-24 1998-05-26 Societe Nationale Industrielle Et Aerospitiale Aircraft motor pod including a pivotable pod cowling
US6155520A (en) * 1997-09-12 2000-12-05 Eurocopter Bracket hinged panel
FR2768489A1 (en) * 1997-09-12 1999-03-19 Eurocopter France Aerodynamic hinged panel for helicopter engine unit hood
DE10053632A1 (en) * 2000-10-28 2002-05-02 Bayerische Motoren Werke Ag Car boot flap hinge rides curved guide between flap end positions with three-roller slide ensuring guide movement despite unevenness.
DE10053632B4 (en) * 2000-10-28 2008-02-28 Bayerische Motoren Werke Ag Hinge for a flap or the like of a vehicle
US20050023411A1 (en) * 2001-12-13 2005-02-03 Minoru Matsuda Lubricating oil filling structure for an engine
US7070147B2 (en) * 2001-12-13 2006-07-04 Honda Giken Kogyo Kabushiki Kaisha Lubricating oil filling structure for an engine
US20110133489A1 (en) * 2009-12-09 2011-06-09 Airbus Operations Sas Aircraft nacelle incorporating a hood closure device that is independent of the locking mechanism
FR2953492A1 (en) * 2009-12-09 2011-06-10 Airbus Operations Sas AIRCRAFT NACELLE INCORPORATING A CLOSURE RECONCILIATION DEVICE INDEPENDENT OF THE LATCHING MECHANISM
US8894012B2 (en) 2009-12-09 2014-11-25 Airbus Operations Sas Aircraft nacelle incorporating a hood closure device that is independent of the locking mechanism
WO2012104561A3 (en) * 2011-02-04 2012-10-26 Aircelle Nacelle with articulated fan casing covers
US9759095B2 (en) * 2013-03-07 2017-09-12 Rolls-Royce Corporation Gas turbine engine access panel
US20140294581A1 (en) * 2013-03-07 2014-10-02 Rolls-Royce Corporation Gas turbine engine access panel
US20160214729A1 (en) * 2013-09-04 2016-07-28 Snecma Casing structure interposed between the engine and the nacelle having pivoting shroud sectors
US10322813B2 (en) * 2013-09-04 2019-06-18 Safran Aircraft Engines Casing structure interposed between the engine and the nacelle having pivoting shroud sectors
FR3040044A1 (en) * 2015-08-12 2017-02-17 Snecma PLATFORM HOOD COMPRISING A HOLDING MEMBER IN SOLIDARIZED POSITION ON THE INSIDE OF THE HOOD
US10494112B2 (en) * 2015-12-22 2019-12-03 Rolls-Royce Deutschland Ltd & Co Kg Engine cowling with three-dimensionally adjustable hinge
US10173783B2 (en) * 2016-08-23 2019-01-08 Airbus Helicopters Rotorcraft with cowling able to rotate and translate relative to the fuselage
US20180057183A1 (en) * 2016-08-23 2018-03-01 Airbus Helicopters Deutschland GmbH Rotorcraft with cowling able to rotate and translate relative to the fuselage
WO2018042117A1 (en) * 2016-08-30 2018-03-08 Safran Nacelles Aircraft turbojet engine nacelle, with hybrid air inlet and fan cowling
FR3055313A1 (en) * 2016-08-30 2018-03-02 Safran Nacelles PLATFORM FOR AIRCRAFT TURBOJET ENGINE, AIR INLET AND HYBRID BLOWER HOOD
US10689125B2 (en) 2016-08-30 2020-06-23 Safran Nacelles Nacelle for an aircraft turbojet engine with hybrid air inlet and fan cowl
US10738521B2 (en) 2017-03-29 2020-08-11 Interlock Usa, Inc. Sliding door roller system
EP3461744A1 (en) * 2017-09-29 2019-04-03 Airbus Operations S.A.S. Thrust reverser turbofan engine for an aircraft with improved opening
FR3071821A1 (en) * 2017-09-29 2019-04-05 Airbus Operations DOUBLE FLOW TURBOREACTOR FOR AN AIRCRAFT WITH IMPROVED OPENING
CN109573065A (en) * 2017-09-29 2019-04-05 空中客车运营简化股份公司 Double-current method jet engine and aircraft
US10882630B2 (en) * 2017-09-29 2021-01-05 Airbus Operations Sas Dual-flow jet engine for an aircraft with an improved aperture
CN109573065B (en) * 2017-09-29 2022-03-08 空中客车运营简化股份公司 Double-flow jet engine and aircraft
US11274480B2 (en) 2019-10-30 2022-03-15 Interlock Usa, Inc. Sliding door roller and method of installation
US11629538B2 (en) 2019-10-30 2023-04-18 Interlock Usa, Inc. Sliding door roller and method of installation

Similar Documents

Publication Publication Date Title
US2494347A (en) Roller type hinge
US11046446B2 (en) Tiltrotor aircraft rotating proprotor assembly
US2564988A (en) Door hinge linkage
US2290331A (en) Door check for automobiles
US2445131A (en) Door mounting
US11492131B2 (en) Tiltrotor aircraft rotating proprotor assembly
US4185415A (en) Articulated hinge cooperating with an energy storage device capable of automatically opening and holding open an unlatched compartment door
US5915653A (en) Spherical mating fairings for hingeline applications
US2862256A (en) Weather seals for slidable closure assemblies
US10538303B2 (en) Systems and methods for linkage controlling access panel on commercial aircraft
EP3378767B1 (en) Roller track assembly for a tiltrotor proprotor door
US4697763A (en) Hinge system for thrust reverser cowl
US3837040A (en) Mechanism for limiting deflection of a door
US3280562A (en) Thrust reversing device for fan type jet engines
US2333482A (en) Airplane wing, aileron, and airplane rudder
US2621359A (en) Hinge construction
US2494001A (en) Hinge construction
US2476268A (en) Flush latch assembly
US2355456A (en) Resilient mounting
CN109760703B (en) Inter-vehicle through channel top guard plate device
US2440817A (en) Hinge structure
US1772559A (en) Concealed hinge for refrigerators and the like
US5072898A (en) Engine cowling roller attachment
GB443887A (en) Hinge device particularly for panels and frames
US2423636A (en) Gun carriage for turret gun slot closures