CN217695999U

CN217695999U - Cooking utensil

Info

Publication number: CN217695999U
Application number: CN202221609596.1U
Authority: CN
Inventors: 朱泽春; 邱雄杰; 马艳龙
Original assignee: Joyoung Co Ltd
Current assignee: Joyoung Co Ltd
Priority date: 2022-06-24
Filing date: 2022-06-24
Publication date: 2022-11-01
Anticipated expiration: 2032-06-24

Abstract

The utility model discloses a cooking appliance, which comprises a pot body and a pot cover, wherein the pot body comprises a body and a machine head, the machine head is rotationally connected with the body so as to have a first state of pressing the pot cover when the pot cover covers the body and a second state of rotating towards one side far away from the body so as to lead the pot cover to be taken down from the body; the fuselage is provided with and is used for rotating the articulated seat of being connected with the aircraft nose, and the surface of articulated seat is provided with first backstop portion, and the aircraft nose is provided with second backstop portion, and first backstop portion can be with the cooperation of second backstop portion backstop to restriction aircraft nose is by second state free rotation to first state. Fuselage and aircraft nose set up backstop structure respectively, and the aircraft nose makes the aircraft nose stop in a certain position for the pivoted in-process of fuselage because the backstop effect of first backstop portion and second backstop portion, and can not continue upset downwards to play the effect of only changeing and the anticollision of aircraft nose, both prevented that aircraft nose and pot cover collision from sending the abnormal sound, alleviateed the loss that the collision brought again, improve life.

Description

Cooking utensil

Technical Field

The utility model belongs to the technical field of domestic appliance, concretely relates to cooking utensil.

Background

With the social development and the improvement of the economic level, kitchen electric products such as a rice cooker pressure cooker and the like are very popular in the market and are very common in families. Moreover, with the advancement of science and technology and the pursuit of beauty, the style of the rice cooker is more and more abundant.

There is a rice cooker in the market, including fuselage, aircraft nose and pot cover, in order to satisfy demands such as visual, this rice cooker sets up display panel subassembly on the aircraft nose to the aircraft nose can overturn for the fuselage. When the cooker cover is used specifically, the machine head is rotated upwards to open the area above the machine body, then the cooker cover is covered on the machine body, and then the machine head is turned downwards to enable the machine head to tightly press the cooker cover.

However, when the rice cooker is used, the machine head always turns downwards under the action of gravity and violently impacts the cooker cover or the cooker body, so that a large abnormal sound is emitted, and the cooker cover is generally made of glass, is easy to break under long-time impact, and is poor in user experience.

The common way of using torsion spring or damping block to counteract the gravity of the cover in the flip-type rice cooker is not suitable for the rice cooker with lighter head because of the complex structure, higher cost and the like.

SUMMERY OF THE UTILITY MODEL

The utility model provides a cooking utensil to solve at least one among the above-mentioned technical problem.

The utility model discloses the technical scheme who adopts does:

a cooking appliance comprises a pot body and a pot cover, wherein the pot body comprises a body and a machine head, the machine head is provided with a display panel, and the machine head is rotatably connected with the body so as to have a first state of pressing the pot cover when the pot cover covers the body and a second state of rotating towards one side far away from the body so that the pot cover can be taken down from the body; the fuselage be provided with be used for with the aircraft nose rotates the articulated seat of being connected, the surface of articulated seat is provided with first backstop portion, the aircraft nose is provided with second backstop portion, first backstop portion can with the cooperation of second backstop portion backstop, in order to restrict the aircraft nose by the second state free rotation extremely first state.

One of the first blocking portion and the second blocking portion is a blocking protrusion, and the other of the first blocking portion and the second blocking portion is a blocking groove matched with the blocking protrusion.

The first stopping portion is the stopping protrusion, the second stopping portion is the stopping groove, the stopping protrusions are multiple, and the stopping protrusions are arranged on the surface of the hinged seat at intervals along the rotating path of the machine head.

The stop bulge is provided with a guide arc surface along the moving direction of the machine head.

The surface of articulated seat is provided with the joint bar position, first backstop portion set up in the joint bar position, the one end of joint bar position with articulated seat links firmly, just the subregion of joint bar position periphery with articulated seat has seted up the spread groove between.

One side of the hinged seat facing the machine head is provided with a transition arc surface, and the connecting rib position forms a partial area of the transition arc surface.

The aircraft nose orientation one side of articulated seat has still linked firmly the base station, second backstop portion set up in the base station, the base station still be provided with link firmly in the strengthening rib of aircraft nose.

The aircraft nose is equipped with two orientation articulated arm that articulated seat extends, the articulated arm is located respectively the both sides of articulated seat, cooperation space has between the articulated arm, first backstop portion with second backstop portion all is located in the cooperation space.

The aircraft nose includes base and lid, second backstop portion set up in the base, the lid orientation the projection of base covers second backstop portion with articulated seat, just the edge of lid has downwardly extending's shelters from muscle position.

Still be provided with steam generator in the fuselage, the fuselage has the culinary art chamber, the pot cover is provided with steam channel and stretches into the steam drainage spare in the culinary art intracavity, so that steam generator to the culinary art intracavity steam of carrying.

Since the technical scheme is used, the utility model discloses the beneficial effect who gains does:

1. cooking utensil is in respectively the fuselage with set up backstop structure on the aircraft nose, the aircraft nose for fuselage pivoted in-process, because first backstop portion with the backstop effect of second backstop portion, thereby the restriction the rotation of aircraft nose makes the aircraft nose stops in a certain position, and can not continue upset downwards, thereby plays the effect of the splining and the anticollision of aircraft nose has both prevented the aircraft nose with the abnormal sound is sent in the pot cover collision, has alleviateed the loss that the collision brought again, improves life. Meanwhile, the machine head is light in weight, so that the rotation of the machine head can be easily limited by the stop matching, and the machine head is more suitable for the machine head with light weight.

Furthermore, the utility model discloses still can be through further design first backstop portion with the position of second backstop portion makes the two backstop after, the aircraft nose stops in a designed position to make things convenient for the user to add food in the fuselage or open and shut the lid operation, improve and use experience.

2. In a preferred embodiment of the present invention, one of the first stopper and the second stopper is a stopper protrusion, and the other of the first stopper and the second stopper is a stopper groove engaged with the stopper protrusion. After the stop protrusion is matched with the stop groove, the stop protrusion can be limited in two directions under the stop action of the groove wall of the stop groove, and the machine head is limited to rotate in the two directions, so that the machine head is stably kept at a preset position without swinging, and the positioning stability of the machine head is improved.

3. As an embodiment of the present invention, the surface of the hinge seat is provided with the connecting rib position, the first stopping portion is disposed in the connecting rib position, one end of the connecting rib position is fixedly connected with the hinge seat, and the partial region of the periphery of the connecting rib position is disposed with the connecting groove disposed between the hinge seats. The one end of joint bar position with the fuselage links firmly, other regions of joint bar position periphery with surely go out the mode of recess (the clout forms thin muscle behind the excision recess) with the fuselage links to each other, makes with this the joint bar position form one can for fuselage elastic deformation's elastic base body makes it with certain deformation can take place when receiving the extrusion after the aircraft nose contacts, thereby reduces the joint bar position is right the resistance of aircraft nose makes opening and shutting of aircraft nose is more smooth and easy and make user's more laborsaving during the operation.

4. As a preferred embodiment of the utility model, the aircraft nose orientation one side of articulated seat has still linked firmly the base station, second backstop portion set up in the base station, the base station still be provided with link firmly in the strengthening rib of aircraft nose. The base station orientation articulated seat is protruding, makes the distance between the two more nearly, and is convenient first backstop portion with second backstop portion contact and cooperation, the setting of strengthening rib has increased first backstop portion with the intensity of aircraft nose junction, and through the base station sets up second backstop portion, compare in with second backstop portion directly set up in the mode of aircraft nose, can alleviate second backstop portion with when first backstop portion collides, transmit extremely the vibrations of aircraft nose improve user's operation and feel.

5. As a preferred embodiment of the present invention, the machine head includes a base and a cover, the second stopping portion is disposed on the base, the cover faces the projection of the base to cover the second stopping portion and the hinged seat, and the edge of the cover has a shielding rib position extending downward. The lid can be right the base with articulated structure between the fuselage forms and shelters from, improves pleasing to the eye. Simultaneously the lid is still right the top and the lateral part of base form the parcel, improve the wholeness of aircraft nose improves user's operation and feels.

Drawings

The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the invention and do not constitute a limitation on the invention. In the drawings:

fig. 1 is a schematic structural diagram of the cooking appliance according to an embodiment of the present invention;

FIG. 2 is a cross-sectional view of a portion of the cooking appliance of FIG. 1;

FIG. 3 is an enlarged view of area A of FIG. 2;

FIG. 4 is a schematic structural view of a partial region of the pot body according to an embodiment of the present invention;

FIG. 5 is an enlarged view of area B of FIG. 4;

fig. 6 is a schematic structural diagram of the base according to an embodiment of the present invention.

Wherein:

1, a pan body; 11, a machine head; a 111 base; 1111 an articulated arm; 1112 fitting a space; 1113 base station; 1114 reinforcing ribs; 112 a cover body; 1121 blocking the tendon; 113 a stopper groove; 12 a fuselage; 121 a housing; 122 a hinged seat; 123 stop boss; 1231 to the cambered surface; 124 connecting rib positions; 125 connecting grooves; 126 transition arc surface;

and 2, covering the pot.

Detailed Description

In order to more clearly explain the overall concept of the present invention, the following detailed description is given by way of example in conjunction with the accompanying drawings.

In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, however, the present invention may be practiced in other ways than those specifically described herein, and therefore the scope of the present invention is not limited by the specific embodiments disclosed below.

In addition, in the description of the present invention, it should be understood that the terms "top", "bottom", "inner", "outer", "circumferential" and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present invention.

In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; the connection can be mechanical connection, electrical connection or communication; they may be directly connected or indirectly connected through intervening media, or may be connected through the use of two elements or the interaction of two elements. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

In the present application, unless expressly stated or limited otherwise, a first feature "on" or "under" a second feature may be directly contacting the second feature or the first and second features may be indirectly contacting the second feature through intervening media. In the description of the present specification, reference to the terms "implementation," "embodiment," "one embodiment," "example" or "specific example" or the like, means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above are not necessarily intended to refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.

As shown in fig. 1 to 6, a cooking appliance comprises a pot body 1 and a pot cover 2, wherein the pot body 1 comprises a body 12 and a head 11, the head 11 is provided with a display panel, the head 11 is rotatably connected with the body 12 to have a first state of pressing the pot cover 2 when the pot cover 2 covers the body 12 and a second state of rotating towards one side far away from the body 12 to enable the pot cover 2 to be taken down from the body 12; the fuselage 12 be provided with be used for with articulated seat 122 that aircraft nose 11 rotated to be connected, the surface of articulated seat 122 is provided with first backstop portion, aircraft nose 11 is provided with the second backstop portion, first backstop portion can with the cooperation of second backstop portion backstop, in order to restrict aircraft nose 11 by second state free rotation extremely first state.

The utility model discloses it is right cooking utensil's heating method does not do specifically and restricts, as the utility model discloses a preferred embodiment, cooking utensil is steam cooking utensil, particularly, still be provided with steam generator in the fuselage 12, fuselage 12 has the culinary art chamber, pot cover 2 is provided with the steam passageway and stretches into the steam drainage spare in the culinary art intracavity, so that steam generator to carry steam in the culinary art intracavity. The food is heated by the high-temperature steam, so that the heating uniformity is improved, and the taste of the food is improved.

Of course, the cooking appliance may also adopt a heating plate heating manner, which is not particularly limited.

Further, as shown in fig. 1, the main body 12 has a cover 121, the cover 121 surrounds at least a partial region of the cooking cavity of the main body 12, the cover 121 is made of a transparent material, so that the cooking cavity of the cooking appliance is visible, and during cooking, a user can observe food cooking conditions in the cooking cavity from the outside of the cooking appliance, thereby improving the use experience.

Cooking utensil, with display panel set up in aircraft nose 11, thereby guaranteed the pot cover 2 with the integrality of fuselage 12 structure, and make pot cover 2 with fuselage 12 has large tracts of land and complete visual area, has guaranteed by a wide margin cooking utensil's visual effect.

Meanwhile, the weight of the machine head 11 is light, so that the rotation of the machine head 11 can be easily limited by the stop matching, and the machine head is more suitable for the machine head 11 with light weight. Therefore, cooking utensil is in respectively fuselage 12 with set up backstop structure on the aircraft nose 11, aircraft nose 11 for fuselage 12 pivoted in-process, because first backstop portion with the backstop effect of second backstop portion, thereby the restriction the rotation of aircraft nose 11 makes aircraft nose 11 stops in a certain position, and can not continue upset downwards, thereby plays the effect of the splining of aircraft nose 11 and anticollision has both prevented aircraft nose 11 with the abnormal sound is sent in the 2 collisions of pot cover, has alleviateed the loss that the collision brought again, improves life.

Furthermore, the utility model discloses still can be through further design first backstop portion with the position of second backstop portion makes the two backstop after, aircraft nose 11 stops in a designed position to make things convenient for the user to add food in the fuselage 12 or open and shut the lid operation, improve and use experience.

It should be noted that the present invention is not limited to the structure of the first stopping portion and the second stopping portion, and includes, but is not limited to, the following embodiments:

the first implementation mode comprises the following steps: in this embodiment, the first stopping portion and the second stopping portion are both protruding structures, and when the handpiece 11 is turned over and opened, the first stopping portion and the second stopping portion stop, and at this time, a prompt is provided for a user, and the user can continue to rotate the handpiece 11 upward, so that the first stopping portion goes over the second stopping portion. When the user stops rotating the handpiece 11, the handpiece 11 is turned downwards under the action of gravity, but due to the existence of the first stop, the second stop is stopped on the downward movement path, so that the handpiece 11 is limited to rotate downwards.

The second embodiment: as a preferred embodiment, as shown in fig. 2 and 3, one of the first and second stopping portions is a stopping protrusion 123, and the other one of the first and second stopping portions is a stopping groove 113 matched with the stopping protrusion 123.

After the stop protrusion 123 is matched with the stop groove 113, under the stop action of the groove walls on two sides of the stop groove 113, the stop protrusion 123 can be limited in two directions to limit the rotation of the machine head 11 in two directions, at the moment, the machine head 11 cannot rotate downwards or upwards, so that the machine head 11 is stably kept at a preset position and cannot swing, and the positioning stability of the machine head 11 is improved.

Further, the number and arrangement of the stopping protrusions 123 and the stopping grooves 113 are not limited in this embodiment, and in a preferred embodiment, as shown in fig. 2 to 5, the first stopping portion is the stopping protrusion 123, the second stopping portion is the stopping groove 113, the stopping protrusions 123 are multiple and are arranged on the surface of the hinge seat 122 at intervals along the rotation path of the handpiece 11.

Through on the motion path of aircraft nose 11 the interval set up a plurality ofly backstop arch 123 makes aircraft nose 11 has a plurality of "gears" at the rotation in-process, for aircraft nose 11 reserves a plurality of angle positions of predetermineeing, makes it stop on a certain position as required, has improved suitability and use experience. For example, the position of the stopping protrusion 123 may be set to keep the handpiece 11 at a position of 30 °, 45 °, 60 °, 90 ° or the like, so as to meet different requirements of users, and is not particularly limited herein.

Moreover, when the user rotates during aircraft nose 11, backstop groove 113 passes through each in proper order backstop arch 123 can also give the feedback of user's power, makes the user more clear the dwell position of aircraft nose 11 improves and uses experience.

Of course, the first stopping portion may also be a stopping groove, and a plurality of stopping portions are arranged at intervals along the moving path of the handpiece 11, and the second stopping portion is a stopping protrusion, which is not specifically limited herein.

Further, as shown in fig. 3, the stopper protrusion 123 is provided with a guide arc 1231 in the moving direction of the head 11.

The protruding 123 of backstop gets into the backstop groove 113 and follow during the roll-off in the backstop groove 113, receive the guide of direction cambered surface 1231 reduces the 113 openings in backstop groove are right the hindrance of the protruding 123 of backstop makes aircraft nose 11 is more smooth and easy in the motion process, prevents aircraft nose 11 is in certain position department card die, makes the operation more laborsaving.

As a preferred embodiment of the present invention, as shown in fig. 4 and 5, the surface of the hinged seat 122 is provided with a connecting rib position 124, the first stopping portion is disposed on the connecting rib position 124, one end of the connecting rib position 124 is fixedly connected with the hinged seat 122, and the connecting groove 125 has been opened between the partial region of the periphery of the connecting rib position 124 and the hinged seat 122.

One end of the connecting rib position 124 is fixedly connected with the hinge seat 122, and other areas on the periphery of the connecting rib position 124 are connected with the hinge seat 122 in a groove cutting mode (the residual material after the groove is cut off is formed into a thin rib), so that the connecting rib position 124 forms an elastic base body which can elastically deform relative to the machine body 12, and the elastic base body is enabled to deform to a certain extent when being extruded after being contacted with the machine head 11, thereby reducing the resistance of the connecting rib position 124 to the machine head 11, and enabling the machine head 11 to be opened and closed more smoothly and enabling a user to operate more easily.

In addition, the connecting rib position 124 has certain elasticity, and can also play the cushioning effect to its vibrations that produce when with aircraft nose 11 contacts, reduce the transmission to the vibrations of aircraft nose 11 improve user's operation and feel.

Specifically, as shown in fig. 5, the lower end of the connecting rib portion 124 is fixedly connected to the hinge base 122 or integrally formed therewith, and the connecting grooves 125 are formed between the upper end, the left end, and the right end of the connecting rib portion 124 and the hinge base 122, so that the connecting rib portion 124 can swing with the lower end as a fulcrum.

Further, as shown in fig. 5, a side of the hinge seat 122 facing the handpiece 11 has a transition arc surface 126, and the connecting rib 124 forms a partial area of the transition arc surface 126.

The aircraft nose 11 is followed transition cambered surface 126 removes, transition cambered surface 126 can be right aircraft nose 11 plays the guide effect, reduces aircraft nose 11 with the frictional resistance between articulated seat 122 makes aircraft nose 11 motion is more smooth, simultaneously connecting rib position 124 constitutes transition cambered surface 126 partly, works as aircraft nose 11 is followed transition cambered surface 126 removes to when connecting rib position 124 department, the extrusion connecting rib position 124 takes place to be out of shape to further reduce the resistance between the two, improve the smoothness nature of aircraft nose 11 motion.

In a preferred embodiment of the present invention, as shown in fig. 1 and fig. 6, the machine head 11 faces towards one side of the hinged seat 122 is further fixedly connected with a base 1113, the second stopping portion is disposed on the base 1113, and the base 1113 is further provided with a reinforcing rib 1114 fixedly connected to the machine head 11.

Base station 1113 orientation articulated seat 122 is protruding, makes the distance between the two closer, makes things convenient for first backstop portion with the contact of second backstop portion and cooperation, the setting of strengthening rib 1114 has increased first backstop portion with the intensity of aircraft nose 11 junction to through base station 1113 sets up second backstop portion, compare in with second backstop portion directly set up in the mode of aircraft nose 11, can alleviate second backstop portion with when first backstop portion collides, transmit to the vibrations of aircraft nose 11, improve user's operation and feel.

Preferably, as shown in fig. 6, the handpiece 11 is provided with two hinge arms 1111 extending towards the hinge base 122, the hinge arms 111 are respectively located at two sides of the hinge base 122, a matching space 1112 is provided between the hinge arms 1111, and the first stopper and the second stopper are both located in the matching space 1112.

The two hinged arms 1111 of the hand piece 11 are matched with the hinged seat 122 at two sides of the hinged seat 122, and the first stopping portion and the second stopping portion are matched between the two hinged arms 1111, so that the matching positions of the first stopping portion and the second stopping portion are closer to the central area of the hinged structure, thereby optimizing the stress of the hand piece 11, and preventing the damage of the single-side hinged structure caused by the uneven stress at the hinged matching positions at two sides or the inclination of the hand piece 11 caused by the uneven stress at two sides in the rotating process.

As a preferred embodiment of the present invention, as shown in fig. 1 and fig. 6, the handpiece 11 includes a base 111 and a cover 112, the second stopping portion is disposed on the base 111, the projection of the cover 112 toward the base 111 covers the second stopping portion and the hinge seat 122, and the edge of the cover 112 has a shielding rib 1121 extending downward.

The cover 112 can shield the hinge structure between the base 111 and the body 12, thereby improving the appearance. Meanwhile, the cover body 112 also wraps the top and the side of the base 111, so that the integrity of the machine head 11 is improved, and the operation hand feeling of a user is improved.

The utility model can be realized by adopting or using the prior art for reference in places which are not mentioned in the specification.

The embodiments in the present specification are described in a progressive manner, and the same and similar parts among the embodiments are referred to each other, and each embodiment focuses on the differences from the other embodiments.

The above description is only an example of the present invention, and is not intended to limit the present invention. Various modifications and variations of the present invention will be apparent to those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the scope of the claims of the present invention.

Claims

1. A cooking appliance comprises a pot body and a pot cover, wherein the pot body comprises a body and a machine head, the machine head is provided with a display panel, and the machine head is rotatably connected with the body so as to have a first state of pressing the pot cover when the pot cover covers the body and a second state of rotating towards one side far away from the body so that the pot cover can be taken down from the body; it is characterized in that the preparation method is characterized in that,

the fuselage be provided with be used for with the articulated seat that the aircraft nose rotated to be connected, the surface of articulated seat is provided with first backstop portion, the aircraft nose is provided with second backstop portion, first backstop portion can with the cooperation of second backstop portion backstop, in order to restrict the aircraft nose by second state free rotation extremely first state.

2. The cooking appliance of claim 1,

3. The cooking appliance of claim 2,

4. The cooking appliance of claim 3,

the stop projection is provided with a guide arc surface along the moving direction of the machine head.

5. The cooking appliance of claim 1,

the surface of articulated seat is provided with the joint bar position, first backstop portion set up in the joint bar position, the one end of joint bar position with articulated seat links firmly, just the subregion of joint bar position periphery with articulated seat between seted up the spread groove.

6. The cooking appliance of claim 5,

7. The cooking appliance of claim 1,

8. The cooking appliance of claim 7,

9. The cooking appliance of claim 1,

10. The cooking appliance according to any one of claims 1 to 9,

still be provided with steam generator in the fuselage, the fuselage has the culinary art chamber, the pot cover is provided with steam channel and stretches into the steam drainage spare in the culinary art intracavity, so that steam generator to culinary art intracavity delivery steam.