CN214112847U

CN214112847U - A cabin door lock mechanism for intelligent low-altitude manned aircraft

Info

Publication number: CN214112847U
Application number: CN202022792286.5U
Authority: CN
Inventors: 王新林; 蔡建东; 谢安桓; 张丹
Original assignee: Zhejiang Lab
Current assignee: Zhejiang Lab
Priority date: 2020-11-27
Filing date: 2020-11-27
Publication date: 2021-09-03
Anticipated expiration: 2030-11-27

Abstract

The utility model discloses a cabin door lock mechanism for an intelligent low-altitude manned aircraft, which relates to the field of intelligent low-altitude manned aircraft cabin door structure design. Two components; the first component includes a first component support, a lock pin, a pull ring, and a first return spring, the lock pin is arranged in the guide hole of the first component support, and the end of the lock pin is connected to the The pull ring is fixedly connected, the first return spring is arranged on the lock pin; the second component includes a second component support, a lock hook, a hand plate, an index shaft and a second return spring, and the lock hook is indexed through the The shaft is connected with the second component support, the second return spring is arranged on the indexing shaft, and the hand plate is arranged on the lock hook. The utility model can open and close the cabin door urgently in and out of the cabin, has strong environmental adaptability, does not need external power sources such as electricity, gas, liquid, etc., and the operation of opening and closing the cabin door is convenient and reliable.

Description

Cabin door lock mechanism for intelligent low-no-load manned aircraft

Technical Field

The utility model belongs to low no-load man aircraft hatch door structural design field, more specifically relates to a low no-load man aircraft's of intelligence hatch door latch mechanism.

Background

In the low empty load people aircraft field of tradition, the person of taking has higher flight operation control authority, and the aircraft is higher to the person of taking controls the degree of dependence at the flight phase moreover, so flight phase controls the level requirement to the person of taking and higher to can use comparatively complicated and control loaded down with trivial details hatch door latch mechanism.

The field of intelligent low-no-load manned aircrafts aims to simplify the operation process of aircraft passengers and reduce the control level requirements of the passengers by means of the ground station function, and realizes unmanned driving in the whole process. This requires that the aircraft cabin door lock, in addition to ensuring structural strength and light weight, also take into account the safety, reliability and convenience of the crew in any situation in which the cabin door lock is operated. The utility model aims at providing a simple structure is reliable, need not the outside energy and easily emergency escape operation's cabin lock, solves this problem to a certain extent.

SUMMERY OF THE UTILITY MODEL

Problem to exist among the prior art, the utility model provides a low no-load man-made aircraft's of intelligence hatch door latch mechanism, this hatch door latch mechanism simple structure is convenient for open, close the hatch door.

The purpose of the utility model is realized through the following technical scheme: a cabin door lock mechanism for an intelligent low-no-load manned aircraft comprises a first assembly arranged on the outer side of a cabin body and a second assembly arranged on the inner side of a cabin door; the first assembly comprises a first assembly support, a lock pin, a pull ring and a first return spring, the lock pin is arranged in a guide hole of the first assembly support, the end part of the lock pin is fixedly connected with the pull ring, and the first return spring is arranged on the lock pin; the second assembly comprises a second assembly support, a lock hook, a hand plate, a shifting shaft and a second reset spring, the lock hook is connected with the second assembly support through the shifting shaft, the second reset spring is arranged on the shifting shaft, and the hand plate is arranged on the lock hook.

Further, the first assembly support is installed on the outer side of the cabin body in an embedded mode, and the pull ring extends into the cabin body through the opening of the cabin body.

Further, the second assembly support is arranged on the inner side edge of the cabin door, and the hand plate extends out of the outer side of the cabin door.

Further, the sliding stroke of the lock pin is larger than or equal to the width of the lock hook.

Furthermore, the second assembly support is further provided with a limiting pin, and the limiting pin is located behind the locking hook.

Compared with the prior art, the beneficial effects of the utility model are as follows: the first assembly is provided with a lock pin which can slide up and down and is reset by using a first reset spring, and an operator pulls the lock pin upwards by pulling a pull ring in the cabin, so that the cabin door is unlocked in the cabin; the second component is provided with a lock hook which can swing left and right and is reset by a spring, and an operator can release the lock hook by pressing the hand plate outside the cabin, so that the cabin door can be unlocked outside the cabin. When the door is closed, the lock hook can realize automatic rebound locking by impacting the lock pin. The utility model discloses a hatch door latch mechanism does not rely on external power sources such as electricity, gas, liquid, makes the operator all can the manual operation open, close the hatch door in the under-deck and the cabin outside, and simple structure is reliable, convenient operation.

Drawings

Fig. 1 is a schematic structural view of a hatch lock mechanism of the present invention;

fig. 2 is a detail view of the door lock mechanism of the present invention: FIG. 2a is a block diagram of a first assembly; FIG. 2b is a block diagram of a second assembly;

fig. 3 is the utility model discloses hatch door lock mechanism's in-service behavior diagram: FIG. 3a is a structural diagram illustrating a locked state; FIG. 3b is a schematic view of the unlocking structure inside the cabin; fig. 3c is a schematic view of the outboard unlocking structure.

Wherein: 1-a first component; 2-a second component; 101-a first component holder; 102-a locking pin; 103-a pull ring; 104-a first return spring; 201-second component support; 202-a latch hook; 203-hand plate; 204-an indexing shaft; 205-a spacing pin; 206-second return spring.

Detailed Description

In order to make the objects and technical solutions of the embodiments of the present invention clearer, the technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings. It is to be understood that the embodiments described are only some of the embodiments of the present invention, and not all of them. In general, the components of the embodiments of the invention described and illustrated in the drawings can be realized in other different details as well as variations in size. In the drawings of the embodiments of the present invention, in order to describe the operation principle of each element in the door lock mechanism more clearly, the size, dimension and shape of each component inside the structure cannot be limited.

As shown in fig. 1, the present invention provides a schematic structural diagram of a cabin door lock mechanism for an intelligent low-idling human aircraft, which includes a first component 1 disposed outside a cabin body and a second component 2 disposed inside a cabin door; the detail view of the first assembly 1 is shown in fig. 2a, the first assembly 1 includes a first assembly holder 101, a lock pin 102, a pull ring 103, and a first return spring 104, the lock pin 102 is disposed in a guide hole of the first assembly holder 101 and can slide linearly along the guide hole of the first assembly holder 101; the end of the lock pin 102 is fixedly connected with a pull ring 103, the pull ring 103 can drive the lock pin 102 to linearly slide back and forth by pushing or pulling, and the first return spring 104 is arranged on the lock pin 102 and used for returning the lock pin 102; the first assembly support 101 is installed on the outer side of the cabin body in an embedded mode, and the pull ring 103 extends into the cabin body through an opening of the cabin body; an operator can unlock the cabin door in the cabin body by pulling the pull ring 103 upwards so as to leave the cabin body, the lock pin 102 is reset under the action of the first return spring 104 after unlocking, and the reset pressure of the lock pin 102 at the maximum stroke position is not more than 20N after the next locking operation.

The second assembly 2 is shown in a detail view in fig. 2b, the second assembly 2 includes a second assembly support 201, a latch hook 202, a hand plate 203, a shift shaft 204 and a second return spring 206, the latch hook 202 is connected to the second assembly support 201 through the shift shaft 204, the shift shaft 204 is used for fixing the latch hook 202, the second assembly support 201 is further provided with a limit pin 205, and the limit pin 205 is located behind the latch hook 202. The stopper pin 205 limits the lock hook 202 to rotate around the rotation shaft 204 by a limited angle and hooks the lock pin 102 during the locking operation, and the second return spring 206 is disposed on the rotation shaft 204 to automatically return the lock hook 202 during the rotation. The hand plate 203 is arranged on the locking hook 202, the hand plate 203 is used for manually pressing to enable the locking hook 202 to rotate, and the torque of the second return spring 206 when the hand plate 203 is pressed to the limit position is not more than 1.8 Nm. The second component support 201 is disposed on the inner edge of the cabin door, the hand plate 203 extends out of the cabin door, an operator can press the hand plate 203 to rotate the locking hook 202 along the indexing shaft 204 in the direction away from the locking pin 102 outside the cabin body, so as to unlock the cabin door, and after unlocking, the locking hook 202 is reset to the position of the limit pin 205 under the action of the second return spring 206 and waits for the next locking operation. The sliding travel of the latch 102 is greater than or equal to the width of the latch hook 202.

The structure of the locked state is schematically shown in fig. 3a, when the door is closed inside or outside the cabin, the second assembly 2 moves to approach the first assembly 1 following the door, and the locking hook 202 strikes the locking pin 102 and rotates along the indexing shaft 204 in the direction away from the locking pin 102; the second assembly continues to move closer to the cabin, the locking hook 202 returns to the original position under the action of the second return spring 206 and catches the locking pin 102, and the locking operation is finished.

The cabin unlocking structure is schematically shown in fig. 3b, an operator can pull the pull ring 103 upwards in the cabin to enable the lock pin 102 to slide along the guide hole of the first component support 101, the lock pin 102 is separated from the lock hook 202, the cabin door is unlocked and opened, the lock pin 102 is reset under the action of the first return spring 104 after unlocking, and the next locking operation is waited.

The fig. 3c illustrates an outboard unlocking structure, where an operator can press the hand plate 203 to rotate the locking hook 202 along the rotation axis 204 in a direction away from the locking pin 102 outside the cabin body, so as to unlock the cabin door, and after unlocking, the locking hook 202 is returned to the position of the limit pin 205 by the second return spring 206 and waits for the next locking operation.

To sum up, the utility model provides a hatch door latch mechanism through installing first subassembly 1 and the second subassembly 2 on the cabin body and hatch door, has realized all manually locking and unblock hatch door in the under-deck and extravehicular, and does not need external power source, and the structure is ingenious, and the simple operation, and simple and reliable is the less preferred choice of idle man aircraft of intelligence at development and trial flight stage hatch door latch mechanism.

The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. A cabin door lock mechanism for an intelligent low-no-load manned aircraft is characterized by comprising a first assembly (1) arranged on the outer side of a cabin body and a second assembly (2) arranged on the inner side of the cabin door; the first assembly (1) comprises a first assembly support (101), a lock pin (102), a pull ring (103) and a first return spring (104), wherein the lock pin (102) is arranged in a guide hole of the first assembly support (101), the end part of the lock pin (102) is fixedly connected with the pull ring (103), and the first return spring (104) is arranged on the lock pin (102); the second assembly (2) comprises a second assembly support (201), a lock hook (202), a hand plate (203), a transposition shaft (204) and a second return spring (206), the lock hook (202) is connected with the second assembly support (201) through the transposition shaft (204), the second return spring is arranged on the transposition shaft (204), and the hand plate (203) is arranged on the lock hook (202).

2. The door lock mechanism for an intelligent low-empty-load passenger aircraft according to claim 1, wherein the first component support (101) is embedded outside the cabin, and the pull ring (103) extends into the cabin through the cabin opening.

3. The door lock mechanism for intelligent low-altitude manned aircraft according to claim 1, wherein the second component mount (201) is provided on an inboard edge of the door, the hand plate (203) protruding outside the door.

4. The door lock mechanism for intelligent low empty manned aircraft according to claim 1 wherein the sliding travel of the locking pin (102) is greater than or equal to the width of the locking hook (202).

5. The door lock mechanism for intelligent low-empty manned aircraft according to claim 1, characterized in that the second component support (201) is further provided with a check pin (205), the check pin (205) being located behind the locking hook (202).