US10385913B2 - Length-adjustable Samer rod - Google Patents

Length-adjustable Samer rod Download PDF

Info

Publication number
US10385913B2
US10385913B2 US15/366,132 US201615366132A US10385913B2 US 10385913 B2 US10385913 B2 US 10385913B2 US 201615366132 A US201615366132 A US 201615366132A US 10385913 B2 US10385913 B2 US 10385913B2
Authority
US
United States
Prior art keywords
longitudinal axis
teeth
engagement section
receiving hole
circumferential direction
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 - Fee Related, expires
Application number
US15/366,132
Other versions
US20170159700A1 (en
Inventor
Gerd Stahl
Adnan Topal
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.)
Airbus Operations GmbH
Original Assignee
Airbus Operations GmbH
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 Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of US20170159700A1 publication Critical patent/US20170159700A1/en
Assigned to AIRBUS OPERATIONS GMBH reassignment AIRBUS OPERATIONS GMBH ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: STAHL, GERD, Topal, Adnan
Application granted granted Critical
Publication of US10385913B2 publication Critical patent/US10385913B2/en
Expired - Fee Related legal-status Critical Current
Adjusted expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C7/00Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads
    • F16C7/06Adjustable connecting-rods
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061Frames
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/18Floors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B33/00Features common to bolt and nut
    • F16B33/002Means for preventing rotation of screw-threaded elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B7/00Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections
    • F16B7/06Turnbuckles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B7/00Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections
    • F16B7/18Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections using screw-thread elements
    • F16B7/182Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections using screw-thread elements for coaxial connections of two rods or tubes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B7/00Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections
    • F16B7/18Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections using screw-thread elements
    • F16B7/187Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections using screw-thread elements with sliding nuts or other additional connecting members for joining profiles provided with grooves or channels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2226/00Joining parts; Fastening; Assembling or mounting parts
    • F16C2226/50Positive connections
    • F16C2226/60Positive connections with threaded parts, e.g. bolt and nut connections
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2226/00Joining parts; Fastening; Assembling or mounting parts
    • F16C2226/50Positive connections
    • F16C2226/80Positive connections with splines, serrations or similar profiles to prevent movement between joined parts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00Articles relating to transporting
    • F16C2326/43Aeroplanes; Helicopters
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/29Rotarily connected, differentially translatable members, e.g., turn-buckle, etc.
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/29Rotarily connected, differentially translatable members, e.g., turn-buckle, etc.
    • Y10T403/295Rotarily connected, differentially translatable members, e.g., turn-buckle, etc. having locking means

Definitions

  • the present invention relates to a Samer rod, which extends along a longitudinal axis and the length of which is adjustable along the longitudinal axis, having a first element, which extends along the longitudinal axis between a first coupling end and the end of an engagement section, and having a second element, which extends along the longitudinal axis between a second coupling end and a receiving end.
  • Samer rods are well-known from the prior art and are used to keep elements at a specified spacing from one another inside the structure of an aircraft. It is thus known from EP 2 240 364 B1, for example, that Samer rods are used to keep a floor arrangement in a specified position relative to the fuselage frame.
  • this object is achieved by means of a Samer rod
  • the Samer rod according to the invention thus has a first element, which is provided with a coupling end, which can be designed, for example, as an eyelet, wherein the first element extends along a longitudinal axis away from the coupling end and an engagement section with a free end is formed at a distance from the coupling end.
  • the engagement section in turn has an outer row of teeth, in the form of a conventional toothing, for example, wherein the row of teeth extends parallel to the longitudinal axis of the Samer rod and has evenly spaced teeth which extend perpendicular to the longitudinal axis and parallel to the circumferential direction of the engagement section.
  • the Samer rod according to the invention has a second element, which extends from a second coupling end, which can also be formed as an eyelet, along the longitudinal axis to a receiving end.
  • a receiving hole extending parallel to the longitudinal axis is formed on the receiving end, which receiving hole has an inner row of teeth on its inner circumferential wall.
  • This row of teeth can likewise be formed as a toothing, so that it in any case has teeth extending perpendicular to the longitudinal axis and in the circumferential direction along the wall of the receiving hole, which are evenly spaced apart from one another, with the spacing of the teeth of the inner row of teeth corresponding to the spacing of the teeth of the outer row of teeth.
  • the inner and the outer rows of teeth are designed such that the width of the teeth of the inner row of teeth measured in the direction of the longitudinal axis corresponds to the spacing of the teeth of the outer row of teeth.
  • the width of the teeth of the outer rows of teeth measured in the direction of the longitudinal axis corresponds to the spacing of the teeth of the inner row of teeth.
  • the engagement section and the receiving hole are each formed in cross section along their extension such that the engagement section can be inserted into the receiving hole and, regardless of how deeply the engagement section is inserted into the receiving hole, the first element and the second element can be pivoted about the longitudinal axis relative to one another between a locked position and a released position.
  • the locked position the inner and the outer rows of teeth engage with one another, so that the first element cannot then be moved relative to the second element along the longitudinal axis, whereas this can occur in the released position since the rows of teeth are then disengaged.
  • a locking ring is provided, which can be moved along the engagement section, but cannot be twisted relative to the engagement section.
  • a catch device is provided on the receiving end which can be shifted between a first and a second position, with the locking ring being coupled in a non-rotating manner to the second element or the receiving end by means of the catch device when the catch device is in the first position. This prevents the first element and the second element twisting against one another so that, by means of the catch device, the first element and the second element can be held in the locked position.
  • the catch device must firstly be moved into the second position, so that the locking ring and thus also the first element can be twisted relative to the second element, so that the arrangement can be moved into the released position.
  • the first element can subsequently be moved axially relative to the second element and then be moved back into the locked position.
  • the Samer rod according to the invention can thus be easily adjusted in terms of its length and is nevertheless reliably secured when in a specified setting so that this setting cannot be unintentionally released.
  • the locking ring has first engagement elements on its outer circumferential surface, with the catch device having a catch element, which is pivotably held about a pivot axis extending perpendicular to the longitudinal axis in the area of the receiving end on the second element and can be pivoted between the first position and the second position, with the catch element engaging with the engagement elements in the first position and being pivoted away from the locking ring in the second position, so that the catch element is disengaged from the engagement elements.
  • the catch device is constructed in a particularly simple way by being held in a pivotable manner on the receiving end.
  • the first position in which the locking ring is prevented from realizing a rotation relative to the second element or the receiving end, is attained by pivoting of the catch element towards the longitudinal axis. Accordingly, the released position is attained by a pivoting of the catch element away from the longitudinal axis.
  • the engagement elements are formed here as a toothing on the outer circumference of the locking ring, wherein the teeth of the toothing extend parallel to the longitudinal axis.
  • the catch element has a U-shaped form, with two shanks which are connected to one another via a central section, wherein the free ends of the shanks are pivotably connected to the receiving end and wherein, in the first position, the shanks engage with the toothing and the central section extends along the side of the locking ring facing away from the receiving end.
  • the central section which, in the first position, abuts the side of the locking ring facing away from the receiving ends, it is easily ensured that the locking ring in the locked state cannot move in the axial direction away from the receiving end.
  • the catch device can, nevertheless, be easily produced.
  • the inner row of teeth has several inner tooth row sections, which extend linearly parallel to the longitudinal axis and spaced apart from one another in the circumferential direction of the wall of the receiving hole.
  • the outer row of teeth has several outer tooth row sections, which extend linearly parallel to the longitudinal axis and spaced apart from one another in the circumferential direction of the engagement section, wherein the width of the inner tooth row sections in the circumferential direction of the wall of the receiving hole corresponds to the spacing of the outer tooth row sections in the circumferential direction of the engagement section and/or the width of the outer tooth row sections in the circumferential direction of the engagement section corresponds to the spacing of the inner tooth row sections in the circumferential direction of the wall of the receiving hole.
  • each of the spacings between the sections in the circumferential direction being selected such that these spacings correspond to the width of the sections on the respective other element, this ensures, on the one hand, that there are only clearly defined relative positions between the first and the second element in which these elements can be axially moved against one another.
  • the locked position it is furthermore ensured that, due to the large engagement surface between the tooth row sections, a large-surface engagement and thus a high load-bearing capacity in the axial direction are achieved. Nevertheless, a release requires only a relatively small pivoting in the circumferential direction according to the width of the tooth row sections, thus keeping the releasing effort minimal.
  • first coupling end and the engagement section are connected to one another such that they can rotate about the longitudinal axis and/or the second coupling end and a section of the second element, in which the receiving hole extends, are connected to one another such that they can rotate about the longitudinal axis.
  • the length of the Samer rod according to the invention can be adjusted even when the coupling ends are permanently installed.
  • FIG. 1 shows an exemplary embodiment of a Samer rod according to the invention in a longitudinal section
  • FIG. 2 shows an enlarged cross-section view of FIG. 1
  • FIGS. 3A and 3B show sections along the lines III-III and IV-IV of FIG. 1 and
  • FIG. 4 shows different views of the locking ring of the exemplary embodiment of FIG. 1 .
  • the exemplary embodiment of a Samer rod 1 has a first element 3 , which has a first coupling end 5 in the form of an eyelet, away from which a cylindrical engagement section 7 extends along a longitudinal axis 9 of the Samer rod 1 to a free end of the engagement section 7 .
  • the coupling end 5 is rotatably connected to the engagement section 7 about the longitudinal axis 9 , so that the first coupling end 5 can be twisted relative to the engagement section 7 .
  • An outer row of teeth in the form of four outer tooth row sections 11 extending linearly parallel to the longitudinal axis 9 is formed on the linearly extending engagement section 7 , which outer tooth row sections are evenly distributed over the circumference of the engagement section 7 (see FIG. 3B ).
  • the outer tooth row sections 11 have a uniform width in the circumferential direction of the engagement section 7 perpendicular to the longitudinal axis 9 .
  • the outer tooth row sections 11 are formed by teeth which extend in the circumferential direction of the engagement section 7 perpendicular to the longitudinal axis 9 and which are evenly spaced apart from one another.
  • the exemplary embodiment of the Samer rod 1 has a second element 13 , which also extends along the longitudinal axis 9 and has a second coupling end 15 in the form of an eyelet.
  • a section 16 of the second element 13 extends away from the second coupling end 15 linearly along the longitudinal axis 9 to a receiving end 17 , in which a receiving hole 19 is formed extending away from the receiving end 17 linearly along the longitudinal axis 9 .
  • the receiving hole 19 extends in the section 16 .
  • the second coupling end 15 is rotatably connected to the remaining part of the second element 13 about the longitudinal axis 9 , namely, the section 16 .
  • inner tooth row sections 21 are formed in the receiving hole 19 , which extend linearly parallel to the longitudinal axis 9 along the circumferential wall of the receiving hole 19 .
  • the inner tooth row sections 21 are formed by teeth extending perpendicular to the longitudinal axis 9 along the circumferential wall of the receiving hole 19 , which are evenly spaced apart from one another, wherein the spacing of the teeth measured in the direction of the longitudinal direction 9 of the inner tooth row sections 21 corresponds to the width of the teeth of the outer tooth row sections 11 .
  • the width of the teeth of the inner tooth row sections 21 measured parallel to the longitudinal axis 9 is identical to the spacing of the teeth of the outer tooth row section 11 .
  • the tooth row sections 11 , 21 can thus engage with one another when they are brought into alignment.
  • the spacing of the inner tooth row sections 21 from one another measured in the circumferential direction corresponds to the width of the outer tooth row sections 11 on the engagement section 7 .
  • the previously described arrangement of the inner and outer tooth row sections 11 , 21 allows the engagement section to be inserted into the receiving hole 19 and moved axially when the outer tooth row sections 11 are offset in the circumferential direction to the inner tooth row sections 21 .
  • the teeth of the outer tooth row sections 11 can engage with the teeth of the inner tooth row sections 21 , so that the axial position of the first element 3 relative to the second element 13 is fixed.
  • the locked position is attained, while the released position exists when the first and the second elements 3 , 13 are pivoted relative to one another in such a way that the tooth row sections 11 , 21 are disengaged.
  • the spacing between the inner tooth row sections 21 corresponds to the width of the outer tooth row sections 11 , the latter can be positioned between the inner tooth row sections 21 , and an axial translational movement is permitted.
  • FIG. 2 is an enlarged depiction of the engagement of the inner tooth row sections 21 with the outer tooth row sections 11 .
  • the engagement section 7 or the first element 3 can thus be pivoted relative to the second element 13 between a locked position, in which the tooth row sections 11 , 21 or the tooth rows are engaged with one another, and a released position, in which the tooth row sections 11 , 21 are disengaged, and, in the released position, the engagement section 7 can be moved axially relative to the receiving hole 19 .
  • a locking ring 23 is provided on the engagement section 7 of the first element 3 , with the inner circumferential wall of the locking ring having projections 25 , the width of which in the circumferential direction corresponds to the width of the spacing between adjacent outer tooth row sections 11 .
  • the projections 25 are distributed in such a way over the circumference of the locking ring 23 that the projections 25 fit exactly in the spaces between the outer tooth row sections 11 . This results in the locking ring 23 being mounted in a non-twisting manner but axially movable on the engagement section 7 .
  • a toothing 27 is provided on the outer circumference of the locking ring 3 .
  • a catch element 29 is held on the second element 13 , about a pivot axis 31 , which extends perpendicular to the longitudinal axis 9 .
  • the catch element 29 is formed U-shaped and has shanks 33 and a central section 35 connecting them, with the free ends of the shanks 33 being linked pivotable about the pivot axis 31 to the second element 23 .
  • the catch element 29 can be pivoted between a first position, in which the shanks 33 can engage in the region of the central section 35 with the toothing 27 of the locking ring 23 , when the locking ring abuts directly on the receiving end 17 , and a second position, in which the locking ring 23 is disengaged from the catch element 29 .
  • the catch element 29 is in the first position, on the one hand the shanks 33 engage with the toothing 27 , and on the other hand, the central section 35 abuts the radial end surface of the locking element 23 facing away from the receiving end 17 , so that the locking ring 23 is prevented from making an axial movement away from the receiving end 17 .
  • the engagement of the shanks 33 and the toothing 27 prevents twisting of the locking ring 23 , and also of the first element 3 , due to the non-rotating coupling thereof with the engagement section 7 , relative to the second element 13 .
  • the catch element 29 can thus prevent a twisting of the first element 3 out of the locked position into the released position when the catch element is in its first position, in which the shanks 33 engage with the toothing 27 .
  • the catch element 29 thus makes it possible, once the axial length of the Samer rod 1 has been set as described previously, to lock the Samer rod in such a way that it cannot move itself back into the released position of the two elements 3 , 13 .
  • the length of the Samer rod 1 can be adjusted in the manner already described, without needing to release the possibly already permanently mounted coupling ends 5 , 15 .
  • the length of the Samer rod 1 can thus also be adapted in the installed state. It is in principle sufficient that only one of the two coupling ends 5 , 15 is rotatably mounted.
  • the previously described Samer rod 1 can thus be easily adjusted in terms of its length and it can also be reliably locked in this position once the setting has been realized.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Dental Prosthetics (AREA)
  • Steering Controls (AREA)

Abstract

A Samer rod has length adjustable along a longitudinal axis. A first element extends along the axis between a first coupling end and an engagement section end, and a second element extends along the axis between a second coupling end and a receiving end. A receiving hole extends along the axis, inside the first element, away from the receiving end to the second coupling end. The engagement section has an outer row of teeth extending parallel to the axis with evenly spaced teeth extending perpendicular to the axis in the circumferential direction of the engagement section. The receiving hole has an inner row of teeth extending parallel to the axis with evenly spaced teeth extending perpendicular to the axis in the circumferential direction of the receiving hole wall. The spacing of the teeth of the two rows in the direction of the axis corresponds to one another.

Description

CROSS-REFERENCES TO RELATED APPLICATIONS
This application claims the benefit of the German patent application No. 10 2015 121 018.5 filed on Dec. 3, 2015, the entire disclosures of which are incorporated herein by way of reference.
BACKGROUND OF THE INVENTION
The present invention relates to a Samer rod, which extends along a longitudinal axis and the length of which is adjustable along the longitudinal axis, having a first element, which extends along the longitudinal axis between a first coupling end and the end of an engagement section, and having a second element, which extends along the longitudinal axis between a second coupling end and a receiving end.
Samer rods are well-known from the prior art and are used to keep elements at a specified spacing from one another inside the structure of an aircraft. It is thus known from EP 2 240 364 B1, for example, that Samer rods are used to keep a floor arrangement in a specified position relative to the fuselage frame.
It is, however, often desirable to be able to adjust the length of the Samer rods in a simple way in order to adapt the Samer rods to the specified installation position so as to avoid having to produce a plurality of Samer rods with different lengths. It is also desirable that the length setting is reliably maintained and that there is no risk of the adjustment mechanism being released, which would then compromise the stability of the Samer rod.
SUMMARY OF THE INVENTION
Based on the prior art, it is therefore an object of the present invention to provide a length-adjustable Samer rod, the adjustment mechanism of which can be reliably secured and which has adequate stability in the longitudinal direction in spite of the adjustability.
According to the invention, this object is achieved by means of a Samer rod
    • having a first element, which extends along the longitudinal axis between a first coupling end and the end of an engagement section,
    • having a second element, which extends along the longitudinal axis between a second coupling end and a receiving end, wherein a receiving hole extends away from the receiving end to the second coupling end, which receiving hole extends along the longitudinal axis inside the first element,
    • wherein the engagement section is provided with an outer row of teeth, which extends parallel to the longitudinal axis and has evenly spaced teeth extending perpendicular to the longitudinal axis in the circumferential direction of the engagement section,
    • wherein the receiving hole is provided with an inner row of teeth, which extends parallel to the longitudinal axis and has evenly spaced teeth extending perpendicular to the longitudinal axis in the circumferential direction of the wall of the receiving hole, the spacing of which in the direction of the longitudinal axis corresponds to the spacing of the teeth of the outer row of teeth in the direction of the longitudinal axis,
    • wherein the engagement section is received in the receiving hole in such a way that the first element can be pivoted about the longitudinal axis between a released position and a locked position relative to the second element,
    • wherein the inner and the outer rows of teeth are disengaged in the released position, so that the engagement section can be moved parallel to the longitudinal axis in the receiving hole, and wherein the rows of teeth engage with one another in the locked position and a movement of the engagement section relative to the receiving hole along the longitudinal axis is prevented,
    • having a locking ring, which can be moved along the longitudinal axis and is held in a non-twisting manner on the engagement section, and
    • having a catch device, which is mounted on the receiving end adjustable between a first position and a second position, wherein the catch device is designed such that, in the first position, the locking ring is coupled to the receiving end in a non-rotating manner and unmovable along the longitudinal axis, and that, in the second position, a rotation of the locking ring relative to the receiving end is permitted.
The Samer rod according to the invention thus has a first element, which is provided with a coupling end, which can be designed, for example, as an eyelet, wherein the first element extends along a longitudinal axis away from the coupling end and an engagement section with a free end is formed at a distance from the coupling end. The engagement section in turn has an outer row of teeth, in the form of a conventional toothing, for example, wherein the row of teeth extends parallel to the longitudinal axis of the Samer rod and has evenly spaced teeth which extend perpendicular to the longitudinal axis and parallel to the circumferential direction of the engagement section.
In addition, the Samer rod according to the invention has a second element, which extends from a second coupling end, which can also be formed as an eyelet, along the longitudinal axis to a receiving end. A receiving hole extending parallel to the longitudinal axis is formed on the receiving end, which receiving hole has an inner row of teeth on its inner circumferential wall. This row of teeth can likewise be formed as a toothing, so that it in any case has teeth extending perpendicular to the longitudinal axis and in the circumferential direction along the wall of the receiving hole, which are evenly spaced apart from one another, with the spacing of the teeth of the inner row of teeth corresponding to the spacing of the teeth of the outer row of teeth. In addition, the inner and the outer rows of teeth are designed such that the width of the teeth of the inner row of teeth measured in the direction of the longitudinal axis corresponds to the spacing of the teeth of the outer row of teeth. In a reciprocal manner, the width of the teeth of the outer rows of teeth measured in the direction of the longitudinal axis corresponds to the spacing of the teeth of the inner row of teeth.
Finally, the engagement section and the receiving hole are each formed in cross section along their extension such that the engagement section can be inserted into the receiving hole and, regardless of how deeply the engagement section is inserted into the receiving hole, the first element and the second element can be pivoted about the longitudinal axis relative to one another between a locked position and a released position. In the locked position, the inner and the outer rows of teeth engage with one another, so that the first element cannot then be moved relative to the second element along the longitudinal axis, whereas this can occur in the released position since the rows of teeth are then disengaged.
Finally, a locking ring is provided, which can be moved along the engagement section, but cannot be twisted relative to the engagement section. A catch device is provided on the receiving end which can be shifted between a first and a second position, with the locking ring being coupled in a non-rotating manner to the second element or the receiving end by means of the catch device when the catch device is in the first position. This prevents the first element and the second element twisting against one another so that, by means of the catch device, the first element and the second element can be held in the locked position.
If, however, it is desirable to adjust the length of the Samer rod, the catch device must firstly be moved into the second position, so that the locking ring and thus also the first element can be twisted relative to the second element, so that the arrangement can be moved into the released position. The first element can subsequently be moved axially relative to the second element and then be moved back into the locked position.
The Samer rod according to the invention can thus be easily adjusted in terms of its length and is nevertheless reliably secured when in a specified setting so that this setting cannot be unintentionally released.
In a preferred embodiment, the locking ring has first engagement elements on its outer circumferential surface, with the catch device having a catch element, which is pivotably held about a pivot axis extending perpendicular to the longitudinal axis in the area of the receiving end on the second element and can be pivoted between the first position and the second position, with the catch element engaging with the engagement elements in the first position and being pivoted away from the locking ring in the second position, so that the catch element is disengaged from the engagement elements.
In this preferred embodiment, the catch device is constructed in a particularly simple way by being held in a pivotable manner on the receiving end. The first position, in which the locking ring is prevented from realizing a rotation relative to the second element or the receiving end, is attained by pivoting of the catch element towards the longitudinal axis. Accordingly, the released position is attained by a pivoting of the catch element away from the longitudinal axis.
In a particularly preferred manner, the engagement elements are formed here as a toothing on the outer circumference of the locking ring, wherein the teeth of the toothing extend parallel to the longitudinal axis. Such a construction can be produced particularly easily.
In another preferred manner, the catch element has a U-shaped form, with two shanks which are connected to one another via a central section, wherein the free ends of the shanks are pivotably connected to the receiving end and wherein, in the first position, the shanks engage with the toothing and the central section extends along the side of the locking ring facing away from the receiving end.
Thanks to the central section which, in the first position, abuts the side of the locking ring facing away from the receiving ends, it is easily ensured that the locking ring in the locked state cannot move in the axial direction away from the receiving end. The catch device can, nevertheless, be easily produced.
In another preferred embodiment, the inner row of teeth has several inner tooth row sections, which extend linearly parallel to the longitudinal axis and spaced apart from one another in the circumferential direction of the wall of the receiving hole. The outer row of teeth has several outer tooth row sections, which extend linearly parallel to the longitudinal axis and spaced apart from one another in the circumferential direction of the engagement section, wherein the width of the inner tooth row sections in the circumferential direction of the wall of the receiving hole corresponds to the spacing of the outer tooth row sections in the circumferential direction of the engagement section and/or the width of the outer tooth row sections in the circumferential direction of the engagement section corresponds to the spacing of the inner tooth row sections in the circumferential direction of the wall of the receiving hole.
If the rows of teeth in the receiving hole and on the engagement section have several sections extending parallel to one another, with each of the spacings between the sections in the circumferential direction being selected such that these spacings correspond to the width of the sections on the respective other element, this ensures, on the one hand, that there are only clearly defined relative positions between the first and the second element in which these elements can be axially moved against one another. In the locked position, it is furthermore ensured that, due to the large engagement surface between the tooth row sections, a large-surface engagement and thus a high load-bearing capacity in the axial direction are achieved. Nevertheless, a release requires only a relatively small pivoting in the circumferential direction according to the width of the tooth row sections, thus keeping the releasing effort minimal.
Finally, it is preferred that the first coupling end and the engagement section are connected to one another such that they can rotate about the longitudinal axis and/or the second coupling end and a section of the second element, in which the receiving hole extends, are connected to one another such that they can rotate about the longitudinal axis. In this case, the length of the Samer rod according to the invention can be adjusted even when the coupling ends are permanently installed.
BRIEF DESCRIPTION OF THE DRAWINGS
The present invention is explained below with reference to drawings showing a preferred exemplary embodiment of the present invention, in which
FIG. 1 shows an exemplary embodiment of a Samer rod according to the invention in a longitudinal section,
FIG. 2 shows an enlarged cross-section view of FIG. 1,
FIGS. 3A and 3B show sections along the lines III-III and IV-IV of FIG. 1 and
FIG. 4 shows different views of the locking ring of the exemplary embodiment of FIG. 1.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
It is seen from FIG. 1 that the exemplary embodiment of a Samer rod 1 according to the invention has a first element 3, which has a first coupling end 5 in the form of an eyelet, away from which a cylindrical engagement section 7 extends along a longitudinal axis 9 of the Samer rod 1 to a free end of the engagement section 7. The coupling end 5 is rotatably connected to the engagement section 7 about the longitudinal axis 9, so that the first coupling end 5 can be twisted relative to the engagement section 7.
An outer row of teeth in the form of four outer tooth row sections 11 extending linearly parallel to the longitudinal axis 9 is formed on the linearly extending engagement section 7, which outer tooth row sections are evenly distributed over the circumference of the engagement section 7 (see FIG. 3B). In particular, the outer tooth row sections 11 have a uniform width in the circumferential direction of the engagement section 7 perpendicular to the longitudinal axis 9. The outer tooth row sections 11 are formed by teeth which extend in the circumferential direction of the engagement section 7 perpendicular to the longitudinal axis 9 and which are evenly spaced apart from one another.
As is also seen from FIG. 1, the exemplary embodiment of the Samer rod 1 has a second element 13, which also extends along the longitudinal axis 9 and has a second coupling end 15 in the form of an eyelet. A section 16 of the second element 13 extends away from the second coupling end 15 linearly along the longitudinal axis 9 to a receiving end 17, in which a receiving hole 19 is formed extending away from the receiving end 17 linearly along the longitudinal axis 9. The receiving hole 19 extends in the section 16. In the case of the second element 13 too, the second coupling end 15 is rotatably connected to the remaining part of the second element 13 about the longitudinal axis 9, namely, the section 16.
As can also be seen in FIG. 3A, inner tooth row sections 21 are formed in the receiving hole 19, which extend linearly parallel to the longitudinal axis 9 along the circumferential wall of the receiving hole 19. The inner tooth row sections 21 are formed by teeth extending perpendicular to the longitudinal axis 9 along the circumferential wall of the receiving hole 19, which are evenly spaced apart from one another, wherein the spacing of the teeth measured in the direction of the longitudinal direction 9 of the inner tooth row sections 21 corresponds to the width of the teeth of the outer tooth row sections 11. In a reciprocal manner, the width of the teeth of the inner tooth row sections 21 measured parallel to the longitudinal axis 9 is identical to the spacing of the teeth of the outer tooth row section 11. The tooth row sections 11, 21 can thus engage with one another when they are brought into alignment.
The spacing of the inner tooth row sections 21 from one another measured in the circumferential direction corresponds to the width of the outer tooth row sections 11 on the engagement section 7.
The previously described arrangement of the inner and outer tooth row sections 11, 21 allows the engagement section to be inserted into the receiving hole 19 and moved axially when the outer tooth row sections 11 are offset in the circumferential direction to the inner tooth row sections 21. When the engagement section 7 or the first element 3 is, however, pivoted relative to the second element 13 about the longitudinal axis 9, the teeth of the outer tooth row sections 11 can engage with the teeth of the inner tooth row sections 21, so that the axial position of the first element 3 relative to the second element 13 is fixed. When the tooth row sections 11, 21 are engaged with one another, the locked position is attained, while the released position exists when the first and the second elements 3, 13 are pivoted relative to one another in such a way that the tooth row sections 11, 21 are disengaged.
Because the spacing between the inner tooth row sections 21 corresponds to the width of the outer tooth row sections 11, the latter can be positioned between the inner tooth row sections 21, and an axial translational movement is permitted.
FIG. 2 is an enlarged depiction of the engagement of the inner tooth row sections 21 with the outer tooth row sections 11.
The engagement section 7 or the first element 3 can thus be pivoted relative to the second element 13 between a locked position, in which the tooth row sections 11, 21 or the tooth rows are engaged with one another, and a released position, in which the tooth row sections 11, 21 are disengaged, and, in the released position, the engagement section 7 can be moved axially relative to the receiving hole 19.
Finally, it can be seen in FIGS. 1 and 4 that a locking ring 23 is provided on the engagement section 7 of the first element 3, with the inner circumferential wall of the locking ring having projections 25, the width of which in the circumferential direction corresponds to the width of the spacing between adjacent outer tooth row sections 11. The projections 25 are distributed in such a way over the circumference of the locking ring 23 that the projections 25 fit exactly in the spaces between the outer tooth row sections 11. This results in the locking ring 23 being mounted in a non-twisting manner but axially movable on the engagement section 7. Finally, a toothing 27 is provided on the outer circumference of the locking ring 3.
It can also be seen from FIG. 1 that, adjacent to the receiving end 17, a catch element 29 is held on the second element 13, about a pivot axis 31, which extends perpendicular to the longitudinal axis 9. The catch element 29 is formed U-shaped and has shanks 33 and a central section 35 connecting them, with the free ends of the shanks 33 being linked pivotable about the pivot axis 31 to the second element 23.
The catch element 29 can be pivoted between a first position, in which the shanks 33 can engage in the region of the central section 35 with the toothing 27 of the locking ring 23, when the locking ring abuts directly on the receiving end 17, and a second position, in which the locking ring 23 is disengaged from the catch element 29. However, when the catch element 29 is in the first position, on the one hand the shanks 33 engage with the toothing 27, and on the other hand, the central section 35 abuts the radial end surface of the locking element 23 facing away from the receiving end 17, so that the locking ring 23 is prevented from making an axial movement away from the receiving end 17. In addition, the engagement of the shanks 33 and the toothing 27 prevents twisting of the locking ring 23, and also of the first element 3, due to the non-rotating coupling thereof with the engagement section 7, relative to the second element 13.
The catch element 29 can thus prevent a twisting of the first element 3 out of the locked position into the released position when the catch element is in its first position, in which the shanks 33 engage with the toothing 27.
The catch element 29 thus makes it possible, once the axial length of the Samer rod 1 has been set as described previously, to lock the Samer rod in such a way that it cannot move itself back into the released position of the two elements 3, 13.
Because the coupling ends 5, 15 are connected rotatably about the longitudinal axis 9 to the other part of the first and second element 3, 13, the length of the Samer rod 1 can be adjusted in the manner already described, without needing to release the possibly already permanently mounted coupling ends 5, 15. The length of the Samer rod 1 can thus also be adapted in the installed state. It is in principle sufficient that only one of the two coupling ends 5, 15 is rotatably mounted.
The previously described Samer rod 1 can thus be easily adjusted in terms of its length and it can also be reliably locked in this position once the setting has been realized.
While at least one exemplary embodiment of the present invention(s) is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. This disclosure is intended to cover any adaptations or variations of the exemplary embodiment(s). In addition, in this disclosure, the terms “comprise” or “comprising” do not exclude other elements or steps, the terms “a” or “one” do not exclude a plural number, and the term “or” means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority.

Claims (6)

The invention claimed is:
1. A Samer rod extending along a longitudinal axis having a length adjustable along the longitudinal axis, comprising:
a first element, extending along the longitudinal axis between a first coupling end and an end of an engagement section,
a second element, extending along the longitudinal axis between a second coupling end and a receiving end,
a receiving hole extending away from the receiving end to the second coupling end, which receiving hole extends along the longitudinal axis inside the first element,
the engagement section being provided with an outer row of teeth extending parallel to the longitudinal axis and having evenly spaced teeth extending perpendicular to the longitudinal axis in the circumferential direction of the engagement section,
the receiving hole being provided with an inner row of teeth extending parallel to the longitudinal axis and having evenly spaced teeth extending perpendicular to the longitudinal axis in the circumferential direction of the wall of the receiving hole, the spacing of which, in the direction of the longitudinal axis, corresponds to the spacing of the teeth of the outer row of teeth in the direction of the longitudinal axis,
the engagement section being received in the receiving hole in such a way that the first element is pivotable about the longitudinal axis between a released position and a locked position relative to the second element,
the inner and the outer rows of teeth being disengaged in the released position, so that the engagement section is movable parallel to the longitudinal axis in the receiving hole, and wherein the rows of teeth engage with one another in the locked position, and a movement of the engagement section relative to the receiving hole along the longitudinal axis is prevented,
a locking ring movable along the longitudinal axis and being held in a non-twisting manner on the engagement section, and
a catch device being mounted on the receiving end adjustable between a first position and a second position, wherein the catch device is configured such that, in the first position, the locking ring is coupled to the receiving end in a non-rotating manner and unmovable along the longitudinal axis, and wherein, in the second position, a rotation of the locking ring relative to the receiving end is permitted.
2. The Samer rod according to claim 1,
wherein the locking ring has first engagement elements on its outer circumferential surface and
wherein the catch device has a catch element pivotably held on the second element about a pivot axis extending perpendicular to the longitudinal axis, the catch element being pivotable between the first position and the second position,
wherein the catch element engages with the engagement elements in the first position and is pivoted away from the locking ring in the second position, so that the lock element is disengaged from the engagement elements.
3. The Samer rod according to claim 2, wherein the engagement elements are formed as a toothing on the outer circumference of the locking ring, and wherein the teeth of the toothing extend parallel to the longitudinal axis.
4. The Samer rod according to claim 3,
wherein the catch element has a U-shaped form, with two shanks connected to one another by means of a central section,
wherein the free ends of the shanks are pivotably connected to the receiving end, and
wherein the shanks engage with the toothing and the central section extends along the side of the locking ring facing away from the receiving end in the first position.
5. The Samer rod according to claim 1,
wherein the inner row of teeth has several inner tooth row sections extending linearly parallel to the longitudinal axis and being spaced apart from one another in the circumferential direction of the wall of the receiving hole,
wherein the outer row of teeth has several outer tooth row sections extending linearly parallel to the longitudinal axis and being spaced apart from one another in the circumferential direction of the engagement section, and
wherein at least one of
the width of the inner tooth row sections in the circumferential direction of the wall of the receiving hole corresponds to the spacing of the outer tooth row sections in the circumferential direction of the engagement section, or
the width of the outer tooth row sections in the circumferential direction of the engagement section corresponds to the spacing of the inner tooth row sections in the circumferential direction of the wall of the receiving hole.
6. The Samer rod according to claim 1, wherein at least one of
the first coupling end and the engagement section are rotatably connected to one another about the longitudinal axis, or
the second coupling end and a section of the second element, in which the receiving hole extends, are rotatably connected to one another about the longitudinal axis.
US15/366,132 2015-12-03 2016-12-01 Length-adjustable Samer rod Expired - Fee Related US10385913B2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102015121018.5 2015-12-03
DE102015121018.5A DE102015121018B4 (en) 2015-12-03 2015-12-03 Length adjustable Samer bar
DE102015121018 2015-12-03

Publications (2)

Publication Number Publication Date
US20170159700A1 US20170159700A1 (en) 2017-06-08
US10385913B2 true US10385913B2 (en) 2019-08-20

Family

ID=58722425

Family Applications (1)

Application Number Title Priority Date Filing Date
US15/366,132 Expired - Fee Related US10385913B2 (en) 2015-12-03 2016-12-01 Length-adjustable Samer rod

Country Status (3)

Country Link
US (1) US10385913B2 (en)
CN (1) CN106985996B (en)
DE (1) DE102015121018B4 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20220290737A1 (en) * 2019-08-07 2022-09-15 Latchways Plc Turnbuckle Device

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3480107A1 (en) * 2017-10-27 2019-05-08 Airbus Operations GmbH Aircraft framework assembly, aircraft structural framework and aircraft with an aircraft structural framework
EP3480110A1 (en) * 2017-11-03 2019-05-08 Airbus Operations GmbH Fastening arrangement for attaching a vehicle floor
GB201821307D0 (en) 2018-12-31 2019-02-13 Airbus Operations Gmbh Connection rod
IT201900004613A1 (en) * 2019-03-27 2020-09-27 Denso Thermal Systems Spa Variable length plastic tie rod
DE202020100426U1 (en) * 2020-01-27 2020-02-13 S-Fasteners Gmbh Train-push rod

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3837753A (en) * 1972-03-30 1974-09-24 F Schumacher Longitudinally adjustable guide rod
US6324940B1 (en) 1997-08-13 2001-12-04 Maclean-Fogg Company Composite link
DE102006058377A1 (en) 2006-12-08 2008-06-26 Airbus Deutschland Gmbh Samer rod for structural reinforcement of fuselage structure of airplane, has shaft and double sided eyes that are arranged at shaft ends for connection of samer rod
US20080175685A1 (en) 2007-01-22 2008-07-24 Herrmann Benthien Fastening arrangement for lashing brackets in the floor of a cargo hold of an aircraft
EP2240364A2 (en) 2008-02-07 2010-10-20 Airbus Operations GmbH Floor system for a fuselage section of an aircraft
US9221313B2 (en) * 2011-08-19 2015-12-29 Deere & Company Stabilizer for a lower link of a three-point hitch of a tractor

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2049079A (en) * 1979-04-20 1980-12-17 Decoto Aircraft Inc Snubber assembly
GB2204292A (en) * 1987-05-01 1988-11-09 Lewis Fredrick Yeatman Hang glider components
DE102006019123B4 (en) * 2006-04-25 2012-08-02 Airbus Operations Gmbh Soil structure for a hull
CN201786838U (en) * 2010-08-16 2011-04-06 慈溪新皇冠金属制品厂有限公司 Sleeve capable of preventing rotation
EP2607229B1 (en) * 2011-12-22 2016-05-11 Airbus Operations, S.L. Composite rod and manufacturing method
CN103600832B (en) * 2013-08-23 2016-01-13 中国航空工业集团公司西安飞机设计研究所 A kind of strut
CN103708022B (en) * 2013-12-30 2015-12-23 陕西中航气弹簧有限责任公司 End self-locking type cabin door stay bar
CN203770328U (en) * 2014-01-04 2014-08-13 周帅 Novel controllable telescopic rod
CN204452916U (en) * 2014-12-10 2015-07-08 中国航空工业集团公司金城南京机电液压工程研究中心 A kind of length-adjustable hatch door connecting rod mechanism

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3837753A (en) * 1972-03-30 1974-09-24 F Schumacher Longitudinally adjustable guide rod
US6324940B1 (en) 1997-08-13 2001-12-04 Maclean-Fogg Company Composite link
DE102006058377A1 (en) 2006-12-08 2008-06-26 Airbus Deutschland Gmbh Samer rod for structural reinforcement of fuselage structure of airplane, has shaft and double sided eyes that are arranged at shaft ends for connection of samer rod
US20100096506A1 (en) 2006-12-08 2010-04-22 Hermann Benthien Connecting rod for the structural reinforcement of a fuselage structure of an aircraft
US20080175685A1 (en) 2007-01-22 2008-07-24 Herrmann Benthien Fastening arrangement for lashing brackets in the floor of a cargo hold of an aircraft
DE102007011621A1 (en) 2007-01-22 2008-07-31 Airbus Deutschland Gmbh Device, in particular Samerstange, for stiffening a fuselage cell structure of an aircraft and / or for fastening a component
EP2240364A2 (en) 2008-02-07 2010-10-20 Airbus Operations GmbH Floor system for a fuselage section of an aircraft
US20110011978A1 (en) 2008-02-07 2011-01-20 Cord Haack Floor system for a fuselage airframe of an aircraft
US9221313B2 (en) * 2011-08-19 2015-12-29 Deere & Company Stabilizer for a lower link of a three-point hitch of a tractor

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
German Search Report, dated Apr. 5, 2016, priority document.

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20220290737A1 (en) * 2019-08-07 2022-09-15 Latchways Plc Turnbuckle Device

Also Published As

Publication number Publication date
DE102015121018A1 (en) 2017-06-08
US20170159700A1 (en) 2017-06-08
CN106985996A (en) 2017-07-28
CN106985996B (en) 2019-05-17
DE102015121018B4 (en) 2018-11-29

Similar Documents

Publication Publication Date Title
US10385913B2 (en) Length-adjustable Samer rod
US10428580B2 (en) Spring operated roller blind system with tension spring adjusting mechanism and locking element for said system
US10690190B2 (en) Torque transfer coupler with anti-slip feature for roller blind drive mechanism
US9416698B2 (en) Fastening method, assembly and structure of engine oil fill extension tube
US10364602B2 (en) Spring pre-tensioning device for roll blind
CA2799150C (en) Handle assembly for double-walled door
US20150297936A1 (en) Freestanding Selectable Free Weight Assembly
AU2020218005B2 (en) Roller blind actuation mechanism, spool housing assembly and cable-covering tube system for a roller blind actuation assembly
BR102016019233B1 (en) COVERING FOR AN ARCHITECTURAL OPENING, BRAKE ASSEMBLY FOR A COVERING AND METHOD OF ASSEMBLY OF A COVERING FOR AN ARCHITECTURAL OPENING
EP2056020A1 (en) Articulated support, particularly for lamps
ES2987837T3 (en) A connector assembly for connecting a rope to a tubular frame
US20160324703A1 (en) System for coupling an auxiliary element to a wheelchair
US20170122463A1 (en) Hanger for mounting cables
EP4403739A2 (en) Roller blind limiter assembly, roller blind mechanism, roller blind system and method for adjusting an end position of a roller blind
DE102018215165A1 (en) Wheel holder
TWI645131B (en) Mounting arrangement for mounting a device, and methods for mounting the mounting arrangement
US11346425B2 (en) Anti-rotational locking device
DE102015219175B4 (en) Connection pipe socket for a sanitary fitting
CN107636237B (en) Spatial structure
DE102009038160B4 (en) Arrangement for releasably fixing a server insert to a server rack
US20190077296A1 (en) Load securing bar
US20130092333A1 (en) Tubular gearmotor with fixing support
WO1997044593A1 (en) Device for the longitudinal correction or setting of cable pulls, cords or the like
US1258940A (en) Shade-roller.
KR200468610Y1 (en) Farming clamp

Legal Events

Date Code Title Description
STPP Information on status: patent application and granting procedure in general

Free format text: DOCKETED NEW CASE - READY FOR EXAMINATION

AS Assignment

Owner name: AIRBUS OPERATIONS GMBH, GERMANY

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:TOPAL, ADNAN;STAHL, GERD;SIGNING DATES FROM 20170516 TO 20170527;REEL/FRAME:045387/0037

STPP Information on status: patent application and granting procedure in general

Free format text: NOTICE OF ALLOWANCE MAILED -- APPLICATION RECEIVED IN OFFICE OF PUBLICATIONS

STPP Information on status: patent application and granting procedure in general

Free format text: PUBLICATIONS -- ISSUE FEE PAYMENT VERIFIED

STCF Information on status: patent grant

Free format text: PATENTED CASE

FEPP Fee payment procedure

Free format text: MAINTENANCE FEE REMINDER MAILED (ORIGINAL EVENT CODE: REM.); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

LAPS Lapse for failure to pay maintenance fees

Free format text: PATENT EXPIRED FOR FAILURE TO PAY MAINTENANCE FEES (ORIGINAL EVENT CODE: EXP.); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

STCH Information on status: patent discontinuation

Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362

FP Lapsed due to failure to pay maintenance fee

Effective date: 20230820