55 results about "Planform" patented technology

Principles described herein allow for wings to be optimized for aerodynamic and structural efficiency while reducing planform compromises required to address wing tip stall problems. All-moving outboard wings allow the outboard wing local angle of attack to be changed relative to the inner wing region to avoid tip stall at high aircraft angles of attack, such as that which is required for low-speed flight. During high-speed cruise flight, at low aircraft angle of attack, the outboard wing local angle of attack can be increased to achieve an ideal elliptical lift distribution.

A flight craft comprises: an intermediate member, which has an annular shape in a plan view and has a flat cross-sectional shape when cut along a plane that includes a straight line in a direction of the plan view; a plurality of gores, each of which extends from an outer side to an inner side of the intermediate member in the plan view, passes through an inner opening of the intermediate member, is folded back, and then extends from the inner side to the outer side of the intermediate member in the plan view; a front side member, which is positioned on a front side of the intermediate member, where the front side is defined as a side facing outward in the plan view, and a rear side is defined as a side opposite to the front side; a rear side member that is positioned on a rear side of the intermediate member; and a tightening mechanism that tightens the front side member and the rear side member in a direction that brings them closer to each other.

As shown in the attached drawings below, the design relates to a coupe-type scale model car and a spider-type scale model car in an open / closed form. Figure 2.1 is a front perspective view of the spider-type scale model car according to the design in an open form. Figure 2.2 is a rear perspective view thereof. Figure 2.3 is a front view thereof. Figure 2.4 is a side view thereof, and the side view on the opposite side is symmetrical to it. Figure 2.5 is a rear view thereof. Figure 2.6 is a plan view thereof. Figure 2.7 is a bottom view thereof. Views that most fully show the design: front and rear perspective views. 2.1) Front perspective view; 2.2) Rear perspective view; 2.3) Front view; 2.4) Side view; 2.5) Rear view; 2.6) Plan view; 2.7) Bottom view

To provide a vapor chamber capable of efficiently cooling a heating element even when the vapor chamber is placed in an inclined manner.SOLUTION: A vapor chamber 1 includes a chamber body 10. The chamber body 10 includes a front surface 11, a bottom surface 24, a first inclined surface 25, a second inclined surface 26 and a top surface 27. The front surface 11 includes a placement region 17 where a heating element 2 is placed. In plan view of the front surface 11, the first inclined surface 25 and the second inclined surface 26 are inclined with respect to the bottom surface in such a manner that a sealed space spreads gradually from the bottom surface 24 toward the top surface 27. In plan view of the front surface 11, the placement region 17 is located between the first inclined surface 25 and the second inclined surface 26.SELECTED DRAWING: Figure 2

To propose a combine capable of preventing deterioration in quality of grains separated by a thresher due to heating.SOLUTION: At the back side of a silencer (36) for reducing an exhaust sound of an exhaust gas burned by an engine (E), a tail pipe (37) is connected, and in a plan view, the tail pipe (37) is linearly extended in the frontward / backward direction by having a predetermined interval from a right wall of a thresher (4) and a left wall of a hopper (7), and in a side view, the tail pipe (37) is formed by a front side part (37A) extending in a rear upward direction from a front end part, an intermediate part (37B) linearly extending backward from a rear part of the front side part (37A), and a rear side part (37C) extending linearly from a rear part of the intermediate part (37B) and reaching a further rear side than a rear wall of the hopper (7). A front part of the intermediate part (37B) is fixed to a grain lifting cylinder (26), and a rear part of the rear side part (37C) is supported so as to be attached to / detached from a second transverse frame (24).SELECTED DRAWING: Figure 3

To provide a truck in which a wheel part is hardly rotated and a stacked state is easily stabilized in a state that trucks are vertically stacked.SOLUTION: A base part 2 of a carriage 1 has a wheel storage recessed part 4 recessed from a placing surface 20 and storing a wheel part 31 of a caster part 3. The wheel accommodation recess 4 has a bottom surface portion 41 having a circular shape in a plan view, and an annular inclined surface portion 42 inclined at a gradient angle of less than 90 degrees from an outer edge portion 412 of the bottom surface portion 41 to the placement surface 20. The wheel accommodation recess 4 has a central protrusion 5 and a turn regulation protrusion 6. The central convex portion 5 protrudes upward at the central portion 411 of the bottom surface portion 41 and restricts the movement of the wheel portion 31 accommodated in the wheel accommodation concave portion 4. The turning restriction protrusion 6 protrudes upward in the outer edge portion 412 of the bottom surface portion 41 and the inclined surface portion 42, and restricts the turning of the wheel portion 31 accommodated in the wheel accommodation recess 4. The rotation restriction protruding portion 6 has a ridge line 60 extending from a vertex 61 at an upper portion of the inclined surface portion 42 toward the bottom surface portion 41.SELECTED DRAWING: Figure 1

A flying apparatus includes a main body assembly, an arm extending away from the main body assembly in a planar view, and a rotor attached to the arm. The arm is rotatable downward from a predetermined position in which the arm is to be when the flying apparatus flies.

A device for transporting engine parts, characterized in that: comprising a lower support frame; the projection of the lower support frame is U-shaped in plan view; a vertical core support frame is fixedly attached to the rear part of the lower support frame; A lifting mechanism is firmly attached to the middle and upper part of the vertical core support frame; The lifting mechanism consists of a rear vertical plate body; the rear vertical plate body is arranged vertically; the upper and lower parts of the rear vertical plate body are each provided with an upper and a lower rotating arm for rotation via a hinge connection; the extension direction of the upper rotating arm and the extension direction of the lower rotating arm are parallel to each other; the length of the upper rotating arm is equal to the length of the lower rotating arm; the ends of the upper and lower rotating arms are hingedly connected to rotate with a front vertical plate body; the front vertical plate body, the upper rotating arm, the lower rotating arm and the rear vertical plate body form a parallelogram structure; A front bracket is fixedly attached to the front of the front vertical plate body; a slide track is fixedly attached to the bottom of the front bracket; A sliding block is arranged on the slideway and is provided with a carrying hook; An electric winch is permanently mounted on top of the vertical core support frame; the end of the hoist rope on the electric hoist extends to the center front of the upper rotating arm and is permanently connected to the center front of the upper rotating arm.

The article according to the present design is used to construct the framework of a cargo handling machine such as a chain conveyor, as shown in the reference plan view showing the state of use and the reference side view showing the state of use.

The characteristic elements of the design consist of three-dimensional features including the shape of the basic article. The design for which registration is sought is shown by solid lines. The drawings include shading of the solid lines to improve the disclosure of the design for which registration is sought. The dashed lines that are directly adjacent to the area representing the shading clarify the boundary of the design for which registration is sought and do not form part of the design for which registration is sought. The dashed lines indicating the remainder of the article represent subject matter not sought for registration and do not form part of the design for which registration is sought. 1.1) Perspective view; 1.2) Perspective view; 1.3) Front view; 1.4) Rear view; 1.5) Right side view; 1.6) Left side view; 1.7) Plan view

The embodiment of the present application provides an inducer and a turbopump, which are used for further improving the cavitation erosion resistance of the inducer. The inducer is suitable for a liquid rocket engine, and the inducer comprises a rotating shaft and blades fixed to the rotating shaft; a first development surface corresponding to the blades comprises a first region, and a part of the first development surface located in the first region is in a curve shape; the first development surface is a planar pattern obtained by unfolding a first section surface of the blades which is cut by a cylindrical surface of the rotating shaft on a shaft radius. The inducer and the turbopump provided by the embodiment of the present application can further improve the cavitation erosion resistance of the inducer.

A flight device according to the present invention comprises a body section 1 that has a plurality of vertices 4, 5 positioned on the same circumscribed circle or circumscribed ellipse in a plan view and a plurality of side parts 2, 3 connected across adjacent vertices 4, 5, and the body section 1 being formed in a polygonal shape in plan view. The flight device also comprises arm parts 11, 21 that have frames 12, 13, 22, 23 extended outward from the vertices 4, 5 on one side and the vertices 4, 5 on the other side of the side parts 2, 3. A rotor attached to the arm parts 11, 21 is also provided.

A casing rotator includes control means configured to perform control of leveling a lifting frame, four lifting cylinders are hydraulic cylinders that are arranged at four corners of a virtual quadrilateral defined along an outer edge of the lifting frame in a plan view and that are capable of performing a contracting action and an extending action of applying a press-in force and a pull-out force to a casing, the control means includes a tilt sensor configured to detect a change angle of tilt of the lifting frame with respect to a leveled state, four variable throttle valves forming pairs with the four lifting cylinders and provided in flow passages through which a hydraulic oil flows out from the lifting cylinders in a contracting action state thereof, and a control unit configured to individually adjust throttling degrees of the variable throttle valves based on the detected change angle.

To provide a drag type turbine device which enables improvement of performance and strength of the device.SOLUTION: A drag type turbine device 1A includes: a support shaft 3; a plurality of support members 4 fixed to the support shaft 3 at predetermined intervals in an axial direction of the support shaft 3; and a plurality of pressure receiving members 5 which are symmetrically disposed around the support shaft 3 while making a pair and supported by the support members 4. The pressure receiving member 5 includes, as a wall surface part extending between an outer end 53 and an inner end 54, an outer wall surface part 50 which extends from the outer end 53 and is formed in a curved surface form, an intermediate wall surface part 51 extending from the outer wall surface part 50 and formed into a flat surface form, and an inner wall surface part 52 extending from the intermediate wall surface part 51 to the inner end 54 and formed in the flat surface form. When the pair of pressure receiving members 5 is symmetrically disposed, the inner end 54 of one of the pressure receiving members 5 is disposed in a first area enclosed by a first straight line ZL1, a second straight line ZL2, a third straight line ZL3, and a fourth straight line ZL4 in a plan view.SELECTED DRAWING: Figure 5

Aircraft (1), in particular an eVTOL aircraft, the aircraft (1) comprising: an aircraft fuselage (2); a main wing (3) connected to the aircraft fuselage (2); a plurality of bar-shaped rotor supports (11, 12, 13, 14) connected to the main wing (3), which extend at least substantially parallel to the aircraft longitudinal axis (x) in a plan view of the aircraft (1); wherein a plurality of rotors (20) are provided on each of the rotor supports (11, 12, 13, 14), and wherein the main wing (3), in particular the span of the main wing (3), defines the diameter of an imaginary circle (K) in the plan view of the aircraft (1), and all components, in particular all parts of the aircraft (1), are arranged within the imaginary circle (K) in the plan view of the aircraft (1).

Method and watercraft (1), in particular a glider, comprising: a hull (2), a main drive (1A), preferably an electric drive, in particular at least one rear electric motor, an air nozzle unit (3) with a compressor (4), in particular with a radial compressor, for generating an air flow, with an air supply line (12) carrying the air flow, and with an air nozzle (5) connected to the compressor (4) via the air supply line (12) for applying the air flow to the outside of the hull (2), that a flat nozzle (6A) is provided as the air nozzle (5), which extends outwards, preferably also rearwards, from a central region of the hull (2), viewed in plan view, that the flat nozzle (6A) has an elongated air outlet gap (9) at the rear end for the outlet of the air flow, and that the flat nozzle has a water separation edge (12) at the rear end,so that behind the elongated air outlet gap (9) of the flat nozzle (6A) an air film can be formed along the outside of the fuselage (2).

A hub model automatic generation method, system, device and storage medium, the method comprises the following steps: generating a rim section contour according to a rim attribute parameter and a vehicle load value, the rim attribute parameter comprising a rim nominal diameter; rotating the rim section contour around a hub center axis to obtain a rim model according to the rim nominal diameter; generating a mounting portion model according to a mounting portion attribute parameter, the mounting portion attribute parameter comprising a mounting portion thickness; determining the relative position of the mounting portion model and the rim model according to a mounting portion position parameter; generating a web section contour according to the relative position of the mounting portion and the rim, the mounting portion thickness, rotating the web section contour around the hub center axis to obtain a spoke contour model; generating a spoke plane figure according to a spoke style parameter; projecting the spoke plane figure on the spoke contour model to obtain a spoke model; taking a Boolean union of the rim model, the mounting portion model and the spoke model to obtain a hub model.

Electric motor (50) comprising a housing, a rotor (1) and a stator (16), wherein the rotor (1) has a shaft (66), the shaft (66) is mounted in the housing by a fixed bearing (11) and a loose bearing (44), wherein the floating bearing (44) is arranged to be axially movable and the shaft (66) has shaft sections with different diameters, whereby the transitions of the shaft sections form shaft diameter steps, wherein a spring element (41) is arranged axially between the floating bearing (44) and a housing part, in particular a bearing plate (42), wherein a ring of the floating bearing (44) is pressed by the spring element (41) against a shaft diameter step, wherein the spring element (41) is pressed against an outer ring of the floating bearing (42) and an inner ring of the floating bearing (42) is pressed against the shaft diameter step, wherein the spring element (41) is corrugated in the circumferential direction and is annular, wherein the spring element (41) forms a ring with a cloverleaf-shaped inner edge, in particular in axial plan view, and a corresponding outer edge, wherein the bearing plate (42) has, in the end face facing away from the stator housing (52), two grooves running around the passage of the shaft (66), wherein an annular circumferential lip (39) is formed on the fan wheel (36) around the fastening area (37) provided for attachment to the shaft (66), and the lip (39) is directed towards the bearing plate (42) and projects out to form a non-contact seal, wherein the lip (39) projects into one of the grooves of the bearing plate (42), an air gap being provided between the lip (39) and the groove, wherein the groove is deeper than an axial distance between a bearing shield-side end face of the floating bearing (44) and a support surface of the spring element on the bearing shield (42), wherein the remaining opening of the passage of the bearing plate (42) is sealed by a shaft seal (30), wherein an axial receiving area of ​​the shaft sealing ring (30) in the bearing plate (42) is longer in the axial direction than a depth of the grooves in the bearing plate (42), wherein a fan cover (35) is placed at least partially overlapping onto the bearing plate (42), wherein the fan cover (35) has the shape of an approximately square shell with rounded corners and a flat bottom, wherein L-shaped recesses are arranged in wall sections of the rounded corners on the stator housing side, which are surrounded by further C-shaped recesses.

This product is used in vehicle wheels. The dashed lines indicate areas that do not form part of the design sought to be registered. The dashed lines indicate the boundaries of the enlarged view and do not form part of the design sought to be registered. In Design 3, the right side view is mirrored to the left side view. The top and bottom views are the result of rotating the left side view 90°. 3.1) Perspective view; 3.2) Front view; 3.3) Rear view; 3.4) Plan view; 3.5) Enlarged view

As shown in the attached drawings, the design relates to a scale model automobile, and in the figures: Figure 1.1 is a perspective front view of the scale model automobile of the design. Figure 1.2 is its perspective rear view. Figure 1.3 is its front view. Figure 1.4 is its side view, and the side view on the opposite side is symmetrical to it. Figure 1.5 is its rear view. Figure 1.6 is its plan view. Figure 1.7 is its bottom view. Figures that most fully show the design: Front and rear perspective views. 1.1) Perspective front view; 1.2) Perspective rear view; 1.3) Front view; 1.4) Side view; 1.5) Rear view; 1.6) Plan view; 1.7) Bottom view