A cap comprising a crown (102) and a visor (104) attached to the crown.
A piston including a crown and a skirt extending generally axially away from the crown.
A pair of adjustment clasps (30) are affixed near each temple of the crown to alter the size of the circumferential portion of the crown.
The cap includes a multi gore shell that forms the crown portion and a bill that connects to the crown.
The stiffener is spaced from the crown to define a cavity within the bill between the stiffener and the crown.
A bayonet type welding-free energy saving lamp cap includes a lamp cap main portion (1), a lamp cap cover (2), a steel pin (3), and copper caps (4).
A bearing cap shaft (26) is provided on the center of the bearing cap (1) and projected out of the center of the bearing cap (1).
An elongate flexible strap member (19) extends from the cap member.
The flexible strap member comprises a distal end couplable to the cap member.
A cap is obtained which, in terms of its strength characteristics, is the equal of a cap that has been produced by casting.
The top comprises a cover in the form of a spherical cap.
radius of the dome of the indentor
A dome loudspeaker (100) has a dome diaphragm (10), a moving coil (12) and a magnet.
The invention also relates to a pressure dome comprising the membrane.
These containers are characterized by at least a bottom having the shape of a bulging dome (1) integral with a cylindrical coaxial flange (8) extending on either side of the dome (1).
The duct nozzle includes a primary duct (120) attached to the exhaust casing (110) and a secondary nozzle (130) arranged about the primary nozzle.
A ducted fan turbine engine (2) includes an inner discharge nozzle (18) and an outer discharge nozzle (8) surrounding the inner discharge nozzle.
The invention relates to a high-pressure injection nozzle that comprises a nozzle body (1) and a nozzle chamber (4) that is configured in the nozzle body and that is connected to a supply duct at the inlet side.
The inventive extrusion nozzle head (1) further comprises at least one heating element (14) by means of which the nozzle gap (3) can be heated.
The distal end of the extendable fly has a nozzle bracket assembly (132) with a nozzle bracket, flexible hose and nozzle tip.
A small wear resistant sleeve for tuyere of blast furnace comprises tuyere cap (1) made of copper, a tuyere seat (2), and a water channel (3).
tuyere injection of slag correction
A tuyere cooling system which includes a coolant circuit for a body section and nose section.
The system includes an oil cooler, eductor primary nozzle, oil cooler nozzle, and surge air dump nozzle.
c. Movable engine or nozzle
A passive exhaust system may include an array of ducts with each duct having a primary (20, 22, 24) and secondary (40, 42, 44) nozzle.
In some embodiments, the nozzle (108) comprises a two-dimensional converging-diverging Laval nozzle geometry.
A nozzle is disposed in the middle of the cylinder so that the nozzle pierces the wall of the cylinder.
jet area control device
The burner is provided with a jet pipe (7), located downstream of the inlet (2), the outer jacket of said pipe having a plurality of passages (8).
The gripper shuttle is designed to permit air to pass through from the jet nozzle (36) to the suction nozzle (40).
The jet nozzle (36) is associated with a suction nozzle (40) located on the other side of the gripper shuttle (20, 22).
In the second variant of the jet nozzle the ledges (6) have the form of a screw thread and make in the nozzle cross-section the cogged form.
The top supporting part and the band for hooping the periphery of heads are set in the shell.
Distortion free area and black top (5
Distortion free area and black top
Distortion free area and black top (7
The inner seal member is a cup seal.
hexagonal blind nut with calotte
The invention is characterised in that the cover (4) has a substantially uniform thickness and at least one reinforcement device of the cover (4) is set in the centre and on the concave side of the cover.
In one embodiment, a conduit is provided having a distal top which is more preferably a ball top, wire top, flare top or flip-down top.
In a method of making the aerosol container cover, the cover is attached to a container body by conventional seaming processing.
A coupling member and sealing cap assembly 10 includes a fluid coupling member 11 and a sealing cap 12.
The invention relates to a plastic protector element, for example a helmet cap comprising a mesh-type and/or honeycomb-type plastic cap body.
The adapter cap has two sets of threads.
The cap may include a base and an outer shell.
Under the floor cap (6) of the steel container, there are several supporting disks (5), which are embodied in such a way that the upper surface thereof matches the shape of the floor cap (6).
Said disks are arranged at an equidistance to the floor cap (6).
Furthermore, the cap (20) and the skirt (12) have respective claw-formed catching means (14, 16, 18) which are adapted to fix the cap (20) in relation to the skirt (12) and allow the cap (20) to swing from a first to a second position.
The hood or shell so shaped is provided with support straps (6 - 8) and the like for holding of the hood or the shell on the head of a person.
The handbag is made of a hard material and has a spherical or truncated sphere shape; its cover (2) is a portion of the sphere or a flattened portion of the sphere and is articulated to the body (1) of the handbag by means of a hinge.
A cock has a handle (17) for rotating the cock plug (3) by means of a stem (5), and between the handle (17) and the stem (5) a gear transmission (22, 37) is arranged.
Helmet formed by a calotte (1) surrounding the head and provided with a removable chinpiece (4) which is fixed to the calotte and which may be replaced by protection members (5).
Each cushioning lug assembly comprises a resilient cushioning block (18) composed of an elastomeric material, a cap (19) mounted on the cushioning block and a tensioned cable (26) secured between the cap (19) and a respective one of the track shoes (11).
A housing cap (107) is joined to the peripheral metallization coating (106) of the bottom of the housing in a soldered or welded connection.
A second connection pin is fixed to the outher casing thereof.
The invention relates to a shoulder prosthesis comprising a stem (10), a cap (20) and a spacer (30), which can be attached to the proximal end (12) of the stem (10) and to which the cap (50) can be attached.
A convex stop cap (40) which can be supported on an axial stop surface (32, 34) is formed on at least one front side (28, 30) of the shaft (22) by means of material displacement.
The body of the helmet comprises a top of the helmet, a brim of the helmet, a visor extending from the brim of the helmet, and many warps for jointing the top and the brim at intervals.
At least three supporting disks are used, arranged in the form of a star in relation to the centre of the floor cap, without being arranged below the centre thereof.
Each of the stator segment assemblies includes a stack of stator plates forming a stator segment core, an end cap assembly, and winding wire wound around the stator segment core and the end cap assembly.
The lining (4) has a lining part (41) which is fixed to the hood (3), and at least one edge part (42) which is loose from the hood (3).
A cap (1), preferably in the form of a baseball cap, comprises a hood (3) with a hood edge (33, 34), as well as a lining (4) which extends along at least a part of the inner surface of the cap (3).
A first microphone (16) is arranged outside the dust cap (15) of a speaker unit (14), while a second microphone (17) is arranged inside the dust cap (15).
The invention relates to protective helmet that comprises a shell (1) and an interior trimming that can be adapted to the head shape of the wearer, as well as a helmet peak (2) formed integrally with the shell (1).
The duct extends axially.
The tail pipe (20) is sealed.
A rocket engine Laval nozzle comprises a nozzle throat, a first expansion section (1), connected to the throat, and a second expansion section (2) joined to the first expansion section.
On the outer circumference side of the nozzle section (8), a nozzle attachment (9) having a nozzle inserting section (21) to be connected to the fuel cell is removably mounted.
The exhaust system further includes a means for directly attaching the secondary nozzle (130) to the exhaust casing (110), the secondary nozzle being held by the exhaust casing independently from the primary nozzle (120).
At least one of the fan nozzle and core nozzle includes circumferentially fixed chevrons that provide a fixed exit area throughout engine operation.
The nozzle axle (49) protrudes from one edge surface (58) of a nozzle vane (45) and fits into the axle hole (53), leaving a gap but rotatably supporting the nozzle vane (45).
CFV Critical flow venturi
CFV Critical flow venturi
Critical-flow venturi option.
turbine gas temperature indicator
turbine gas temperature indicator
air blast nozzle fitted to the exhaust pipe
CFV Critical Flow Venturi
The engine also includes a nozzle (12).
The nozzle is subsonic or supersonic.
The motive nozzle has an exit (110).
A fluid, such as air is supplied to the ejection nozzle (5), and grain-containing air to the nozzle (3) or (4).
A turbocharger comprises a variable nozzle device and an exhaust housing being mechanically and/or thermally decoupled from the variable nozzle device.
The aerodynamic design of the stages is optimised in order to prevent turbulence, by fixing the distance from the nozzle to the collector such that it is comparable to the diameter of the nozzle.
The apparatus preferably includes at least one nozzle diverter member (108) extending from an inner surface of the discharge nozzle (40).
The invention relates to a method for extending a nozzle for a rocket drive, whereby at least one second region (5) of the contour of the nozzle is arranged in the form of an extension of a first region (1) of the contour of the nozzle.
The activation door is rotatably mounted to the nozzle support, and the actuation strap extends from the nozzle.
The thread (18) is retained upstream of the nozzle mouthpiece (14) in an eccentric position relative to the rod axis and extends through the nozzle mouthpiece (14).
A quick disconnect nozzle comprising a nozzle body, a spray tip, and an annular sealing member interposed therebetween.
The nozzle (60) includes an outer nozzle structure (62) which is mounted immediately downstream of the pump diffuser vanes (48).
A pump fluidly associated with the nozzle is energized to move fluid with respect to the nozzle.