SECURING MECHANISM FOR SECURING A VEHICLE DOOR
20220381070 · 2022-12-01
Inventors
Cpc classification
E05B83/42
FIXED CONSTRUCTIONS
E05C9/02
FIXED CONSTRUCTIONS
E05B63/0052
FIXED CONSTRUCTIONS
International classification
Abstract
A securing mechanism for a vehicle door. The securing mechanism includes: a locking system which includes a locking element configured, in a locking position of the locking element, to lock the vehicle door in a closed position and, in an unlocking position of the locking element, to unlock the vehicle door; a securing element configured, in a securing position, to block a locking element movement from the locking position into the unlocking position in a first direction and, in a release position, to release the movement of the locking element from the locking position into the unlocking position in the first direction; and an actuator configured to move the securing element from the release position into the securing position and/or from the securing position into the release position. The securing element is configured, in the securing position, to release a movement of the locking element in a second direction.
Claims
1. A securing mechanism for securing a vehicle door, wherein the securing mechanism comprises: a locking system which comprises a locking element and which is configured, in a locking position of the locking element, to lock the vehicle door in a closed position and, in an unlocking position of the locking element, to unlock the vehicle door; a securing element which is configured, in a securing position, to block a movement of the locking element from the locking position into the unlocking position in a first direction and, in a release position, to release the movement of the locking element from the locking position into the unlocking position in the first direction; and an actuator which is configured to move the securing element from at least one of the release position into the securing position or the securing position into the release position, wherein the securing element is further configured, in the securing position, to release a movement of the locking element in a second direction.
2. The securing mechanism according to claim 1, wherein the securing element is configured, in the securing position, when the locking element is moved from the locking position into the unlocking position, to come into contact with the locking element and, by means of the contact between the securing element and the locking element, to block the movement of the locking element from the locking position into the unlocking position.
3. The securing mechanism according to claim 2, configured in such a manner that, upon the contact between the securing element and the locking element, a connection, which is positive-locking only in the first direction, is formed between the securing element and the locking element.
4. The securing mechanism according to claim 2, configured in such a manner that the securing element in the securing position, in the event of contact with the locking element, provides a support for the locking element, wherein the support brings about the blocking of the movement of the locking element from the locking position into the unlocking position.
5. The securing mechanism according to claim 4, wherein the support is a floating bearing.
6. The securing mechanism according to claim 4, wherein the support is substantially linear or point-like.
7. The securing mechanism according to claim 1, configured in such a manner that the securing element is spaced apart from the locking element in the securing position when the locking element is in the locking position.
8. The securing mechanism according to claim 1, configured in such a manner that the movement of the locking element from the locking position into the unlocking position involves or is a translation of the locking element along a first axis.
9. The securing mechanism according to claim 1, configured in such a manner that a movement of the securing element from the release position into the securing position involves or is a rotation of the securing element about a second axis.
10. The securing mechanism according to claim 8, configured in such a manner that a movement of the securing element from the release position into the securing position involves or is a rotation of the securing element about a second axis, and wherein the first axis extends obliquely with respect to the second axis.
11. The securing mechanism according to claim 10, configured in such a manner that the securing element in the securing position, in the event of contact with the locking element, provides a support for the locking element, wherein the support brings about the blocking of the movement of the locking element from the locking position into the unlocking position, configured in such a manner that the support is spaced apart with respect to the second axis in a third direction, wherein the third direction extends obliquely with respect to at least one of the first axis or the second axis.
12. The securing mechanism according to claim 11, configured in such a manner that the first direction extends at an angle with respect to the first axis and wherein the securing element during rotation about the second axis rotates substantially through the angle.
13. A vehicle door comprising the securing mechanism according to claim 1.
14. A door system comprising: a vehicle door; a door frame; and the securing mechanism according to claim 1, wherein the locking system is arranged on the door, and wherein the actuator and the securing element are arranged on the door frame.
15. A vehicle comprising the securing mechanism according to claim 1.
16. A vehicle comprising the vehicle door according to claim 13.
17. A vehicle comprising the door system according to claim 14.
18. The vehicle according to claim 15, wherein the vehicle comprises an airplane.
19. The vehicle according to claim 16, wherein the vehicle comprises an airplane.
20. The vehicle according to claim 17, wherein the vehicle comprises an airplane.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0021] Preferred embodiments of the invention will now be explained with reference to the appended schematic drawings, in which:
[0022]
[0023]
[0024]
[0025]
[0026]
[0027]
[0028] In the following, the same reference numerals refer to the same functional or structural features.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0029]
[0030] In
[0031] The translational movement of the locking element 4 between the locking position and the unlocking position is carried out along a first axis 14. The securing element 2 is rotatably arranged about a second axis 16 and formed in a rotationally asymmetrical manner with respect to the second axis 16. The securing element 2 is rotated about the second axis 16 in order to move it from the securing position into a release position, which will be further explained in greater detail with respect to
[0032] In the example shown, the locking element 4 is spaced apart from the securing element 2. The two elements 2, 4 are thus not in contact. If an attempt is made to move the locking element 4 along the first axis 14 into the unlocking position, however, there is contact between the two elements 2 and 4. This direct contact blocks a further displacement of the locking element 4 in the direction of the unlocking position.
[0033] The elements 2 and 4 are constructed in such a manner that, in the event of contact between the securing element 2 and the locking element 4, no complete or multi-dimensionally positive-locking connection is formed. It may be said that, in the event of contact, a connection which is positive-locking only in the first direction is formed between the securing element 2 and the locking element 4 so that the movement of the locking element 4 is blocked only in the first direction. In other words, the securing element 2 provides, in this instance, a support for the locking element 4, wherein the support brings about the blocking of the movement of the locking element 4 from the locking position into the unlocking position. This support is, in the case shown, a linear or point-like floating bearing. It may also be a laminar floating bearing. It can also thereby be ensured that the locking element 4 cannot be moved into the unlocking position as long as the securing element 2 is in the securing position. At the same time, it can be ensured that the locking element 4 can move in directions different from the first direction (for example, in the opposite direction).
[0034] As indicated in
[0035]
[0036]
[0037] The securing mechanism comprises an actuator 30 which is configured to move the securing element 2 from the release position into the securing position and/or from the securing position into the release position. The actuator 30 is, for example, wired, and is operated electrically or hydraulically. To this end, a connection cable 32 may be connected to the actuator. The actuator 30 is arranged on the door frame 28, as is the securing element 2. In this configuration, the cable 32 does not have to be guided from the fuselage side to the door 26 since the actuator 30 is secured to the door frame 28. In particular, the actuator 30 and the securing element may be arranged in the region of a door lintel of the door frame 28. In the state shown in
[0038]
[0039]
[0040] Of course, the entire securing mechanism 100 may also be arranged on or in the door 26. In this instance, in particular the actuator 30 and the securing element 2 would be arranged on or secured to the door 26, in the same manner as the locking system 6.
[0041]
[0042] According to the present disclosure the securing element 2 can be mechanically uncoupled from the locking element 4, both in the securing position and in the release position of the securing element 2. The small contact of the two elements 2 and 4 acting as floating bearings can also minimize wear. Furthermore, as a result of the described configuration, a very reliable securing mechanism 100 in the manner of an FLA can be provided. The securing mechanism 100 enables a separate arrangement of the actuator 30 and locking system 6, for example, a positioning of the actuator 30 on the fuselage of the aircraft 300. Assembly complexity and cable wear can thus be minimized. In this instance, no cable guiding from the fuselage side of the vehicle 300 to an actuator 30 which is arranged on the door 26 is also required. Additional assembly costs and also weight can thus be saved.
[0043] Of course, yet other advantages of the invention described herein are possible. Of course, the aspects, embodiments and examples described herein can be combined with each other, wherein individual features may be omitted.
[0044] 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.