Abstract: An arrangement for suppressing aerodynamic noise generated by cavity effect interaction between a wing flap shroud and one or more partially deployed trailing edge flaps. Noise suppression vanes are so positioned with respect to the shroud lower trailing edge and the leading edge of the wing flaps at partial deployment that eddies and vortices resulting from airflow separation at the shroud lower surface are diverted sufficiently by the noise suppression vanes to avoid significant noise inducing impingement of the separated flow on the flap leading edge.

Abstract: Disclosed is a parawing with an automatic canopy withdrawing mechanism having a canopy, a frame to which the canopy is fastened and on which a pilot can be carried, a propeller mounted on the frame, and a plurality rows of suspension lines interconnecting the canopy and the frame. Also mounted on the frame is an automatic canopy withdrawing mechanism including a reel which may be operated to pull back the suspension lines for withdrawing the canopy. Further, a front pulling rope interconnecting the reel and two rows of suspension lines near the leading edge of the canopy, a rear pulling rope interconnecting the reel and the trailing edge of the canopy, and a plurality of guide rollers for guiding the movement of the front pulling rope and the rear pulling rope are provided so that the suspension lines and the canopy may be withdrawn by the automatic canopy withdrawing mechanism. With the canopy and the suspension lines being withdrawn.

Abstract: A fire hose containing an electrical wire therein for transmitting signals. Terminals for connecting cable ways are mounted at both ends of the wire. Therefore, when one hose containing the wire is connected to another similar hose, terminals are also connected to terminals in another hose so as to make a single cable way. The use of such a hose enables a fireman holding a nozzle of the hose to control a pump located apart from the nozzle.

Abstract: The system for stabilizing a support to be stabilized comprises a working rotor mounted on the support via bearings and fixed to a working member having at least one parameter associated with the rotation of the working rotor and which is variable as a function of time. A servo-controlled first electric motor is interposed between the support and the working rotor and serves to rotate the working rotor in a first direction. A reaction rotor is mounted on the support by means of bearings and independently from the working rotor, while being coaxial therewith.

Abstract: A fire sprinkler including a body defining an inlet adapted for connection to a supply of fire extinguishing fluid and an outlet adapted for placement in a zone to be sprinkled; a valve retained by the body and movable between a closed position providing a fluid tight seal between the inlet and the outlet and an open position allowing fluid flow therebetween; an actuator for moving the valve from the closed position to the open position in response to a predetermined condition; and a deflector disposed to disperse into the zone fluid discharged from the outlet; the deflector comprising a plurality of deflector elements each adapted to deflect fluid discharged from the outlet. Also included is a coupling between the deflector elements and adapted to permit adjustment in the relative positions of the deflector elements so as to selectively change the pattern in which fluid discharged from the outlet is dispersed into the zone.

Abstract: An alignment mechanism for independently adjusting the deployable aerosurfaces of an aerospace vehicle in both the stowed and deployed positions. The alignment mechanism includes a guide means having a slot with both a constant width portion and a variable width portion. A slide, interconnected to the deployable aerosurfaces, is pivotally engaged to the guide means so that it travels along the length of the slot. The slide is capable of pivotal movement when the slide is engaged in the slot's variable width portion and incapable of pivotal movement when it is engaged in the slot's constant width portion. An actuator is employed to selectively position the slide along the slot.

Abstract: A hatch opener mechanism mounted flush with a skin panel having a rotatable disk with subjacent spindles and actuator rods, activated by rotating the disk with tool insertable into a socket with a spring biased cover at the center of the disk.

Abstract: A glider, comprising a tubular body open at each end and having a leading edge and a trailing edge, has a two-ring frame assembly disposed about the perimeter of the leading edge to provide body shape and rigidity. A two-ring frame assembly comprises a base ring and a clamping ring configured to matingly engage the base ring. The base ring is placed about the inner perimeter of the leading edge of the tubular body and the clamping ring is placeable about the outer perimeter of the leading edge of the tubular body to retain the tubular body between the base and the clamping ring when the rings are matingly engaged.

Abstract: A ground retaining device for pilotless, radio controlled, miniature model airplanes; comprising horizontal stabilizer engaging bar means, hinged joint means, ground securing plate means.

Abstract: An apparatus for controlling quad-line stunt kites of a type having a pair of handles with lines connected to each end of each handle. This is essentially all the control that is used during the normal kite flying procedure, but when it is desired to bring the kite line in or to let the line out, pick-up and/or pay-out structures are used in conjunction with the control handles. Specifically this pick-up and pay-out structure includes a first rod which extends through a pair of openings in the top of each of the control handles respectively and has a crank portion on one end thereof. A second rod extends through a pair of aligned openings in the lower portion of each of the control handles respectively. An axle, which is adapted to be rotated about an axis, is attached to one end of the first and the second rod and a tubular member is adapted to slide over the axle so that a person can grasp the tubular member in one hand and the crank in the other hand to rotate both rods and both handles about the axis.

Abstract: The invention relates to a process for dispensing indentical pieces having a symmetry of revolution about an axis, such as rivets; this process comprises arranging the pieces one after another in a tube (2) which has a hollow center (2a) adapted to assure the guiding thereof, admitting a compressed fluid into the tube behind the last piece (1D), and distributing said fluid along the length of the tube toward the hollow center (2a) thereof, to the interior of one or several longitudinal passageways (2b), such that the fluid pressure is exerted along the hollow cetner in the spaces (E) separating the pieces, up to the first piece (1P) on which the pressure acts for assuring its transfer. The process of the invention permits dispensing a very great number of pieces without risk of jamming in the tube and with a precise guiding permitting maintaining the alignment of the axes of the pieces.

Abstract: The disclosed invention provides a main landing gear (12, 14, 16, 18) for a high speed (supersonic) aircraft (10) which may be wing-stowed and -mounted in a relatively thin wing (22, 24). The main landing gear (12, 14, 16, 18) is characterized by an inboard gear (12, 14) including a post (58) having a transverse trunnion (52) at a first end (56 or 54) operably mounted on the wing (22, 24). The trunnion (52) is journalled for rotation about an axis for movement of the post (58) between operative and stowed positions. This axis is substantially transverse to the body of the aircraft for forward rotation of the inboard gear (12, 14). A wheel assembly (78, 80) is operably attached at a second end of the post (58). The wheel assembly (78, 80) has a plane of rotation which when stowed in the wing (22, 24) is substantially vertical. In combination with the inboard gear (12, 14) is an outboard gear (16, 18) which includes a post (90) having a skewed trunnion (92) at a first end operably mounted on the wing (22, 24).

Abstract: In order to fill the cryogenic engines of a launcher with propellents up to the time of launcher lift-off, an apparatus is proposed which has a tube section (20) connecting pipes on the ground and on board the launcher (12). A weakened zone (22) of said tube section is automatically broken during lift-off by a mechanism (24,38) applying a tensile stress to the section. This mechanism comprises several assemblies of links (26,28) bearing on the tube section on either side of the weakened zone and a bearing surface (38a,38b) formed in a sleeve (38) fixed with respect to the ground and with which is in contact a protuberance (26a) formed on one of the links of each assembly (26,28).

Abstract: An end tube assembly for the outlet gate of a railroad hopper car includes an end tube and an end tube cap for closing the end tube. The cap is pivotally connected to the end tube and there is a diametrically opposed latch between the cap and end tube. The cap has a guide which extends toward and over the end tube and there is a ramp on the end tube in alignment with the guide to coaxially direct the guide and cap on the end tube during closure. There is a lock on the end tube adjacent the ramp to prevent relative circumferential movement between the cap and end tube. The end tube mounts a gasket which faces the end tube cap. The cap has a rim extending outwardly therefrom for contact with the gasket. The extension of the rim gradually varies from at least one area of greatest extent to at least one area of lesser extent to compensate for distortion of the cap when it is latched onto the end tube.

Abstract: A lock for the end tube assembly and gate valve for the outlet gate of a railroad hopper car includes an elongated flexible cable and a locking element. The end tube assembly includes an end tube and an end tube cap for closing the end tube. There is a pivotal connection and a latch between the cap the end tube. The latch includes a latch member having an opening therein. The gate valve includes a valve member and an operating handle. The operating handle has an opening therein and is located adjacent to the latch member. The elongated cable, which forms a portion of the lock, passes through the handle opening and the latch member opening and has opposite ends thereof secured together by the locking element.