Bizarre Patents
User-operated amusement apparatus for kicking the user's buttocks
An apparatus including a user-operated and controlled apparatus for self-infliction of repetitive blows to the user's buttocks by a plurality of elongated arms bearing flexible extensions that rotate under the user's control.
PatentStorm News
Make the Most of Our Site
See this month's Top Inventors and Most Cited Patents.
Stay on top of the latest innovations by subscribing to an RSS feed.
Registered users: Manage your profile.
| Number | Title | Issue Date |
| 6348460 | 1,2,3-thiadiazole derivatives, plant disease controller and method for using the same A 1,2,3-thiadiazole derivative represented by general formula (I): ##STR1## [wherein R1 is hydrogen atom, halogen atom, (C1 -C6) alkyl, phenyl, etc., R2 is the following group (A) or group (B): ##STR2## (wherein... | 02/19/2002 |
| 6336472 | Pipe repair and replacement apparatus and method A pipe replacement apparatus includes a housing having upper and lower walls that are sealed together about a pipe section to be replaced; on the interior surfaces of the walls, tracks are provided for clamps with engage the original pipe and also carry t... | 01/08/2002 |
| 6334297 | Combuster arrangement A combustor arrangement (8) for a gas turbine engine (3) comprising a combustion chamber, fuel nozzles(52a,52b), and a bled diffuser (7) located upstream of said combustion chamber to, in use, direct an airflow from an upstream compressor (6) into the com... | 01/01/2002 |
| 6332798 | RJ-45 jack module with simultaneous plug release A device is provided for receiving RJ-45 plugs in corresponding jacks. Each RJ-45 plug has a lever arm movable from a locked position, locking the plug to a corresponding jack, to a released position permitting the plug to be removed from the correspondin... | 12/25/2001 |
| 6312224 | Relating to bladed structures for fluid flow propulsion engines A component (24) for a gas turbine engine rotor assembly comprises a wall member (26) for at least partially bridging a space between adjacent rotor blades (18) and a root member (42) for insertion into a groove in the rotor disc (18) of the rotor assembl... | 11/06/2001 |
| 6289667 | Combustion chamber and a method of operation thereof A catalytic combustion chamber is provided with at least two cataleptic combustion zones arranged in flow series, In a first mode of operation fuel is supplied from first fuel injectors, positioned upstream of the first catalytic combustion zone, into the... | 09/18/2001 |
| 6286361 | Method and apparatus for remotely detecting pressure, force, temperature, density, vibration, viscosity and speed of sound in a fluid An apparatus for detecting pressure in a hollow fan blade of a turbofan gas turbine engine comprises a magnetostriction transducer arranged in a sub chamber of the fan blade which is interconnected to a main chamber. A magnetic coil is arranged in the fan... | 09/11/2001 |
| 6283713 | Bladed ducting for turbomachinery An axial flow turbomachine has at least one circumferential row of aerofoil members in which at least one of the two end walls (33) between successive blades (30) is given a non-axisymmetric profile to modify the boundary layer flow at the wall. In one fo... | 09/04/2001 |
| 6283707 | Aerofoil blade damper An aerofoil blade damper comprising an elongate member which is inserted within a core passage of the blade and extends within the blade with the damper retained therein at one end which is closest to the blade root with the remainder of the damper free t... | 09/04/2001 |
| 6273135 | Fuel flow control apparatus A high pressure fuel system includes tapped high pressure flows (22,24) with restrictors (44,46) to provide low pressure flows with which, via a valve (50) to enable either a low pressure flow to bias a main, high pressure fuel cut off valve (16) to close... | 08/14/2001 |
| 6267381 | Resilient strip seal arrangement A seal for effecting a seal between two components (2,4) to inhibit a flow of fluid, between the two components, in a sealing direction (22) from an upstream side (24) of the seal to a downstream side (26) of the seal. The downstream side (26) of the seal... | 07/31/2001 |
| 6254344 | Seal An annular seal comprising a mass of bristles (10) packed together in a layer axially adjacent to an annular backing plate (12). The bristles (12) and backing plate (14) are mounted on and extend from a radially outer member (4) towards and around a cylin... | 07/03/2001 |
| 6253555 | Combustion chamber comprising mixing ducts with fuel injectors varying in number and cross-sectional area A three stage lean burn combustion chamber (28) comprises a primary combustion zone (36), a secondary combustion zone (40) and a tertiary combustion zone (44). Each of the combustion zones (36,40,44) is supplied with premixed fuel and air by respective fu... | 07/03/2001 |
| 6241468 | Coolant passages for gas turbine components A gas turbine engine component, typically either a turbine blade or vane or combustor, comprising a wall (40) with a first surface (39) which is adapted to be supplied with a flow of cooling air, and a second surface (38) which is adapted to be exposed to... | 06/05/2001 |
| 6240732 | Fluid manifold A fluid manifold (41) comprises two annular chambers (42 and 46) in flow series and having a barrier (45) therebetween. A fluid is fed into the first larger annular chamber (42) and circulates circumferential therethrough before being passed through a plu... | 06/05/2001 |
| 6237343 | Combustion chamber and a method of operation thereof A gas turbine engine (10) combustion chamber (28) comprises a primary combustion zone (36) and a secondary combustion zone(40) in which lean mixtures of fuel and air are burned. Air is supplied to a first mixing duct (50) through a swirler (52). Air is su... | 05/29/2001 |
