45results about How to "Small inclination" patented technology

An airbag configuration for braking the landing impact of flying payloads has a central airbag (17) and at least one torus ring (11, 12, 13) surrounding the central airbag. A payload (L) is attachable on the central airbag (17). A stabilizing device (19) is provided which extends from the lowermost portion of the at least one torus ring (11, 12, 13) to the central airbag (17). The central airbag provides primarily vertical braking of the landing impact while the torus ring provides primarily horizontal braking of the landing impact.

The present invention relates to a method for producing a structure serving as an etching mask on the surface of a substrate. In this case, a first method involves forming a first partial structure on the surface of the substrate, which has structure elements that are arranged regularly and are spaced apart essentially identically. A second method involves forming spacers on the surface of the substrate, which adjoin sidewalls of the structure elements of the first partial structure, cutouts being provided between the spacers. A third method step involves introducing filling material into the cutouts between the spacers, a surface of the spacers being uncovered. A fourth method step involves removing the spacers in order to form a second partial structure having the filling material and having structure elements that are arranged regularly and are spaced apart essentially identically. The structure to be produced is composed of the first partial structure and the second partial structure.

In an angular position adjusting apparatus, tooth profiles of an internal gear 31 and an external gear 21 are formed according to loop shapes 74a and 84a of predetermined trochoid curves 74 and 84.

A wheel suspension with a transverse leaf spring (1a–1c) which is articulated at both ends on wheel carriers. The transverse leaf spring shaped symmetrically to the vehicle longitudinal axis (L) has a curved profile with a middle region (1a) offset parallel to the wheel axis. The transverse leaf spring is supported on the vehicle body by means of two transverse leaf spring bearings (2) with high lateral rigidity. The curved profile of the transverse leaf spring with four arcs (1d, 1e) allows for a bending of the middle region (1a) to take place essentially without a change in the tread width.

A multirotor aircraft with an airframe and a thrust producing units arrangement, wherein the thrust producing units arrangement comprises a predetermined number of thrust producing units for producing thrust in a predetermined direction, and wherein a flexible suspension unit is rigidly mounted to the airframe, wherein the flexible suspension unit comprises at least one bearing that mechanically couples the thrust producing units arrangement to the airframe such that the thrust producing units of the predetermined number of thrust producing units are inclinable in relation to the airframe.

A case main body and an upper plate are reliably fitted together, a seal is formed between the fitting surfaces, and a magnetic circuit is prevented from malfunctioning. A solenoid-controlled valve, which connects a solenoid section (2) and a valve section (30), comprises a cylindrical case main body (3) having a solenoid coil (4) housed therein and having a connecting section (3A) at one end, an upper plate (6) having a locking surface (6B) adapted to be fitted to the connecting section (3A), and a connector (5) integrally provided with the upper plate (6). A seal section (20) is joined to an outer surface between the fitting surfaces of the connecting section (3A) and the upper plate (6).

A distortion compensation apparatus and method for a power amplifier enable accurate distortion compensation, even if frequency amplitude deviation and group delay error are present in the power amplifier. A reverse distortion coefficient is read from a reverse distortion coefficient table. A distortion compensation process is performed on an incoming signal using the read reverse distortion coefficient. The distortion compensated signal is amplified and transmitted by the power amplifier, and the reverse distortion coefficient table is updated based on the incoming signal before distortion compensation, and the output signal of the power amplifier. The relation between the phase of the time difference value and the reverse distortion coefficient is obtained from the reverse distortion coefficient corresponding to a linear operation domain of the power amplifier. A frequency characteristic of a frequency characteristic compensation filter, to which the distortion compensated signal is supplied, is set such that inclination of the phase of the reverse distortion coefficient becomes small, thereby accurate distortion compensation can be performed even if frequency amplitude deviation is present in the power amplifier.

A motion conversion mechanism includes a shaft having an external thread and a cylinder having an internal thread that is screwed with the external thread. The motion conversion mechanism converts rotating motion of one of the shaft and the cylinder into linear motion of the other of the shaft and the cylinder. The cylinder is provided with two internal thread portions, each having the internal thread, such that a threadless portion is interposed between the two internal thread portions in an axial direction.

An image reading apparatus includes a transport path that is inclined downwardly as advancing from an upstream side to a downstream side, an image reading section disposed in a middle of the transport path, a cover member that is bent to cause downward inclination of a face on the downstream side of the transport path to be larger than an inclination of a face on the upstream side, a support member having a plate form, the support member disposed on a rear face of the cover member and protruding toward the upstream side from a proximity of a position where the cover member is bent in the face on the downstream side, and a pressing member in which another end is supported by the support member to cause one end to be contactable with the image reading section, thereby pressing the transported medium against the image reading section.

To solve tangle problems that a fishing line before passing a line guide ring is tightened around a fishing line guide just after casting and that the fishing line passing through the line guide ring of the fishing line guide goes around a rear side of the line guide ring due to “line slack” or the like so as to be tightened around the fishing line guide, the guide is designed such that a line guide ring (3) is inclined to a tip side, and an angle of junction between the line guide ring (3) and side support legs (9, 11) is made smaller at a butt side than at a tip side, and a hook concave portion on which a fishing line is caught so as to be turned back is not formed between the line guide ring (3) and the side support legs (9, 11).

The invention provides a loading method of a ship, which is applied to loading of the ship. The ship comprises a ship bow positioned at the front end, a ship stern positioned at the back end as well as a plurality of cabins positioned between the ship bow and the stern; the forefront cabin is the first cabin; and the hindmost cabin is the second cabin. The loading method of the ship comprises thefollowing steps: S1, loading cargoes in each cabin according to the preset loading total weight A of the ship, wherein the total weight of the cargoes loaded in all the cabins is B and B is less thanA; S2, calculating the weight E of the cargoes needing to be loaded in the first cabin as well as the weight F of the cargoes needing to be loaded in the second cabin according to the preset final immersion depth C2 of the ship bow and the preset final immersion depth D2 of the stern; and S3, loading the cargoes in the first cabin and the second cabin correspondingly according to the weight E of the cargoes needing to be loaded in the first cabin as well as the weight F of the cargoes needing to be loaded in the second cabin in the step S2. The loading method of the ship is higher in safety.

To obtain a magnetic sensor unit in which the deviations or the inclinations of magnetic resistance elements and a permanent magnet are low and which has substantially equivalent electric resistance values of magnetic resistance elements, by imparting equivalent magnetic fields to both of a pair of two magnetic resistance elements; and to intend to reduce the changing amount of a mid-point voltage due ot a temperature change. Many magnetic resistance elements are formed on an unmagnetized permanent magnet material, and are cut together with the permanent magnet material accurately by a dicing machine or the like. The magnetic resistance elements divided into a plurality are individually taken out, and the permanent magnet material is magnetized to a permanent magnet. The center of the magnetized permanent magnet material substantially coincides with that of the pair of two magnetic resistance elements, and equivalent magnetic fluxes can be imparted to both of the pair of two magnetic resistance elements.