The invention provides a probe for an aircraft including a strut having an interior passage accommodating a plurality of pneumatic lines, a probe head extending from the strut and having at least one inlet opening communicating with the pneumatic lines, a baseplate situated below the strut for attaching the probe to the aircraft, and a manifold situated below the baseplate for communicating with the pneumatic lines, wherein the baseplate is adapted and configured so that the pneumatic lines comm...

A nautical instrument that can be repetitively mounted to and removed from a surface within a ship without the use of tools or other instruments. The nautical instrument incorporates a mounting system that achieves slidable locking engagement of the nautical instrument to a bulkhead plate that is permanently secured to the surface of the ship. In one embodiment, the invention comprises: a housing containing a gauge; a back plate connected to the housing and having a rear surface; a bracket assem...

An instrumented device for the study of airflow over a structure (10), comprises a support (16) forming a thin plate (24) adapted to be applied and shaped to the contour of a predetermined region of the structure. Connection structure (22) cements a portion of an inner surface of the support to that predetermined region, leaving a space (36) of low height between an inner surface of the plate (24) of the support and that predetermined region. This height is substantially equal to the thickness o...

The invention is a method for determining anemobaroclinometric parameters on board an aircraft. The air speed vector (Vp), the static pressure (Ps), and the impact temperature (Ti) are measured, and the other parameters are calculated on the basis of the aforementioned measurements.

SURFING PARAMETERS GAUGE AND TRANSFER APPARATUS is a velocity, time and space covered by a surfboard measurement apparatus or any other similar solid body, comprising a multifunction module(2) enclosing a sensor adapted to pick up the surfboard displacement related to the water, transforming the data into electrical signals and send them to processing data unit. The multifunction module(2) comprising a housing(11) embedded in the surfboard(1) hull having inside a capsule(10) swiveling related to...

An apparatus and method for measuring the vertical motion of a floating platform e.g. a survey vessel, caused by wave action. The apparatus includes a sensor having three accelerometers (11,12,13) arranged on mutually perpendicular axes (Ax,Ay,Az) so that one accelerometer acts in a vertical plane and the other two act in a horizontal plane. Output signals (S1,S2,S3) from the accelerometers are continually sampled through a multiplexer (14) and are passed through an ADC (19) and a shift register...

A method of land vehicle suspension evaluation and design through roll angle analysis. The method is based on predicting front roll angle and rear roll angle for a given road bank angle and lateral vehicle force. Method steps include determining a vehicle front section sprung weight, determining a vehicle rear section sprung weight, predicting a front roll angle, predicting a rear roll angle, comparing the predicted front roll angle XXXX to the predicted rear roll angle, and changing suspension ...

An orientation monitoring apparatus includes an inner spherical shell rigidly fixed within an outer spherical shell, and a spherical ball positioned between the two shells. The inner shell has a polar coordinate grid impressed on it so that the position of the ball relative to the grid is seen from above. An inertial platform is rotationally interfaced with the inner shell. This platform supports a video camera with a view of the grid and ball. As well, the platform supports a motor driven fly-w...

The invention relates to a method for detecting that the design loads of an aircraft have been exceeded during landing. According to the invention: --in a preliminary step: the load criteria (C1, C2, . . . , Cp) are defined; and the laws of variation of the allowable values (C1ad, C2ad, . . . , Cpad) of these load criteria (C1, C2, . . . , Cp) are determined, as a function of input parameters (P1, P2, . . . , Pn); and --at the moment of landing: the values of the said input parameters (P1, P2, ....

A gyroscopic navigational installation for land and sea vehicles for provng characteristics of the trajectory of the vehicle. The installation in one embodiment includes a gimbal mounted on the vehicle and pivotable about an axis. A first gyro is rotatably supported by the gimbal about a rotational axis such that a gyro azimuth sensitivity axis is orthogonal to the longitudinal axis of the vehicle and a gyro rolling sensitivity axis is parallel to the vehicle longitudinal axis. A controlled acce...