US2494347A - Roller type hinge - Google Patents
Roller type hinge Download PDFInfo
- 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
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- Prior art keywords
- hinge
- roller
- rollers
- elements
- track
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- Expired - Lifetime
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- 230000033001 locomotion Effects 0.000 description 9
- 238000009434 installation Methods 0.000 description 3
- 230000004075 alteration Effects 0.000 description 2
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 125000006850 spacer group Chemical group 0.000 description 2
- 238000007792 addition Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000008933 bodily movement Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/08—Inspection panels for power plants
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D1/00—Pinless hinges; Substitutes for hinges
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D1/00—Pinless hinges; Substitutes for hinges
- E05D1/04—Pinless hinges; Substitutes for hinges with guide members shaped as circular arcs
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D15/00—Suspension arrangements for wings
- E05D15/40—Suspension arrangements for wings supported on arms movable in vertical planes
-
- 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
- E05Y2201/00—Constructional elements; Accessories therefor
- E05Y2201/60—Suspension or transmission members; Accessories therefor
- E05Y2201/622—Suspension or transmission members elements
- E05Y2201/688—Rollers
-
- 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
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.
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- 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
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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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 |
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US2494347A true US2494347A (en) | 1950-01-10 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US590492A Expired - Lifetime US2494347A (en) | 1945-04-26 | 1945-04-26 | Roller type hinge |
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US (1) | US2494347A (en) |
Cited By (19)
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)
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 |
-
1945
- 1945-04-26 US US590492A patent/US2494347A/en not_active Expired - Lifetime
Patent Citations (3)
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)
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 |
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