1
Gregory H Matthias: Thrust reverser for fan jet aircraft engines. Rohr, P J Schlesinger, Frank Gilliam, September 14, 1993: US05243817 (42 worldwide citation)

A fail-safe pivot door-type aircraft turbine engine thrust reverser which includes a plurality of pairs of pivoting doors on the blocker and deflector sides of openings in a fan jet nacelle. The doors form a flush surface along the nacelle exterior and the fan duct flow path when stowed during norma ...


2
Rosenthal Herman A: Swirl anti-ice system. Rohr, P J Schlesinger, F D Gilliam, August 25, 1987: US04688745 (39 worldwide citation)

A system for circulating heated gases within the circular leading edge of a jet engine housing to prevent ice build-up thereon, or to remove accumulated ice thereform. Hot gases such as air from a hot, high pressure section of the jet-engine are directed through a conduit. The conduit enters the ann ...


3
James F Steckbeck, Sharad Naik: Aerodynamic stiffening ring for an aircraft turbine engine mixer. Rohr, P J Schlesinger, Frank Gilliam, November 30, 1993: US05265807 (30 worldwide citation)

A mixing nozzle for an aircraft turbine engine having an improved aerodynamic stiffening ring secured to the lobes of the mixer. Aircraft turbine engines having a rearwardly discharging nozzle are often provided with a mixer having a generally circular forward end adapted to be attached to an engine ...


4
Dale W R Lawson: Aircraft turbine engine thrust reverser. Rohr, P J Schlesinger, Frank Gilliam, July 27, 1993: US05230213 (28 worldwide citation)

A thrust reverser for use with turbo-fan aircraftt engines; in particular engines mounted on an aircraft fuselage. Four radially spaced openings around the engine each is closed by a stowed door. An actuator is provided to move each door to a deployed position extending through the opening, near the ...


5
Yogendra C Bhatt: Overhead lighting fixture. Rohr, P J Schlesinger, F D Gilliam, June 5, 1979: US04157584 (27 worldwide citation)

An overhead lighting fixture with the housing having an open bottom, a resilient hinge pivotally fastening a first side of the light transmitting panel to a first side of the housing adjacent the open bottom of the housing, and a latch assembly for detachably securing a second side of the light tran ...


6
Gregory H Matthias: Cascade type thrust reverser for fan jet engines. Rohr, P J Schlesinger, Frank D Gilliam, May 10, 1994: US05309711 (26 worldwide citation)

A cascade type fan jet engine thrust reverser system. A radially arranged opening is provided along the aft edge the of fan cowl of a fan jet engine. Cascade sets each including a plurality of turning vanes are fixedly positioned in each opening. A blocking door and an actuating linkage system are p ...


7
Jihad I Remlaoui: Hinge with offset pivot line. Rohr, P J Schlesinger, Frank Gilliam, April 20, 1993: US05203525 (24 worldwide citation)

A hinge system for a curved surface that has several first hinges arranged along a straight hinge line and at least one second hinge offset from the hinge line. In a preferred embodiments, these hinges are fastened to a pylon and support a curved portion of an aircraft jet engine cowl, which may con ...


8
Branko Sarh: Method of manufacturing an advanced composite duct having integral ribs. Rohr, P J Schlesinger, F D Gilliam, J C Cantor, July 6, 1993: US05225016 (20 worldwide citation)

A method of making ducts having outwardly extending ribs formed integrally with the duct structure. Two tubes are formed from fiber reinforced resin materials, a uniform inner tube and a ribbed outer tube, then the inner tube is bonded with in the outer tube to form a high strength ribbed duct. An o ...


9
Robert M Castro, James M Adee: Apparatus and method for selectively increasing density and thermal conductivity of honeycomb structures. Rohr, P J Schlesinger, F D Gilliam, May 26, 1992: US05116689 (18 worldwide citation)

A locally reinforced honeycomb core panel having a honeycomb core, at least one coiled insert in at least one honeycomb cell and at least one face sheet. These components are formed from high temperature resistant metals. Elongated foil strips are coiled into cylindrical shapes having diameters slig ...


10
James M Adee, John A Frye: Grit blast drilling of advanced composite perforated sheet. Rohr, P J Schlesinger, F D Gilliam, September 23, 1986: US04612737 (18 worldwide citation)

A method and resulting product produced by attaching a prepared maskant of a desired perforation pattern to cured compound contoured or flat advanced composite materials, directing a narrow stream of highly abrasive grit material of a selected particle size range through a relatively large nozzle un ...