An altitude encoder which provides a digital readout from a barometric sensor comprised of an aneroid bellows linked mechanically with a means to control the frequency of a sense oscillator. The sense oscillator produces a frequency proportional to altitude which constitutes an output signal to a counter. The output of a counter represents altitude and is stored for readout or fed into a transponder for transmission to the ground.

An apparatus to continuously monitor a preset altitude for a pilot of an aircraft. It senses a change in altitude and an audible as well as a visible alarm tells the pilot that he has deviated from his preset altitude by a given height. Increase in altitude is signaled by a high pitch tone and by a yellow light while a decrease in altitude is signaled by a low pitch tone and a red light. The invention can also be used to warn a small boat operator of a pressure drop.

An altitude reporter comprising an altimeter, electrooptical means for tracking the position of the indicator of the altimeter first means including a register for registering the position of the indicator and providing pulse group series output corresponding to such a position, and second means for operatively connecting the first means to the electrooptical tracking means. This second means is effective, when the indicator moves in one direction, to operate the register to add increments of su...

Apparatus for providing a digital signal for an aircraft transponder indicating aircraft altitude with a unique sensor forming part of an oscillator, a counter which accumulates counts from the sensor during a predetermined gating period, a ROM which is addressed during a further gating period to apply a sequence of digital numbers to a comparator. The address indicating one thousand foot increments a second counter which receives pulses from the sensor together with the first counter after the ...

A system, method, apparatus, and computer program product for avoiding aircraft collisions with stationary obstacles. The aircraft is provided with a simplified uncluttered onboard display of all objects which are in or proximate to the projected path of the aircraft at its particular altitude plus or minus a predetermined increment, such as 100 feet constituting a hazard zone. The display presents the hazards in that zone in geographical relationship to the position and path of the aircraft. In...

A training mask for replicating the decrease in oxygen density and the increased breathing effort at higher altitudes. The mask has a nasal portion for covering the user's nose and a lower portion for covering the user's mouth. A peripheral edge conformable with the face forms a chamber with the user's mouth and nose contained therein. A valve-controlled air channel presents a first exterior aperture in communication with the outside ambient air and a second interior aperture positioned adjacent...

In a method for the piloting of an aircraft, enabling low-altitude flight by setting up a tangent with the relief to be overflown, the aircraft pilot determines the goals to be attained on a cartographic screen. This is done in enabling a computer, using altimetrical data, to define a ground profile and then a set of straight lines at a tangent to said ground profile. A method of this kind has the advantage of enabling an optimized flight plan to be reconfigured directly, when the pilot comes up...

A flying height tester that can vary an air pressure and measure an air bearing height between a slider and a substrate. The substrate is located within a chamber that has an air pressure. The tester includes a loader which places a slider adjacent to the substrate. An optical system computes the air bearing height from a light beam that is directed through the substrate and reflected off of the slider. The chamber is coupled to a pressure control system that can vary the pressure of the air sur...

In order to ensure correction for altitude for the carburetor used on a internal combustion engine, a control system for the pressure within the fuel bowl (8) is incorporated. This control system consists of a pressure splitter (11) that is connected, on the one hand, with the lower pressure of the venturi throat (4) in the area in which the fuel delivery line (7) opens out and, on the other hand, with the induction pressure in the area of the inlet end (10) of the air flow passage (4), said pre...

A wastegate valve for a turbocharger system in an engine of a work machine, vehicle or the like particularly suitable for operation at changing altitudes. The wastegate valve includes a spring operating against an adjustable spring seat. The adjustable spring seat is adjusted in response to ambient pressure changes to alter the installed length of the spring.