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序号	专利名	申请号	申请日	公开（公告）号	公开（公告）日	发明人
21	Aircraft control system	US37474473	1973-06-28	US3830451A	1974-08-20	FOSNESS J
Apparatus is disclosed for advantageously developing longitudinal, lateral, and directional attitude control and also lift control in improved manners in aircraft systems of the type capable of vertical, hovering, transitional, and conventional modes of flight operation. The aircraft system, having both a principal power plant which produces high-energy primary flow fluid and a fuselage which has attached, fixed aerodynamic liftproducing airfoils, is provided with fluid-reaction liftproducing ejector assemblies in the airfoils at locations symmetrically positioned relative to and laterally distant from the aircraft longitudinal axis and alternatively additionally at a location or locations laterally distant from such longitudinal axis and longitudinally distant from the system center of gravity. Each included airfoil lift ejector assembly is comprised of an airfoil-shaped after injector flap member, a forward ejector flap member which is spaced apart from but operated in combination with the after injector flap member in modes of flight operation other than conventional flight, a core injector essentially centered between the injector flap members, and a conduit conducting high-energy primary flow fluid from the principal power plant to a nozzle in the core injector and to Coanda-blowing slot devices in each system injector flap member during non-conventional modes of system flight. A pilot-operated control device is provided in the system for varying the divergence angles of the lift ejector diffuser sections defined by the flap members in each ejector by coordinated actuation and rotation to thereby vary the system longitudinal, lateral, and directional attitudes and also the system lift control selectively during vertical, hovering and transitional flight while perferably operating the principal power plant at substantially constant power.
22	Improvements in or relating to aircraft controls	US3785596D	1972-05-26	US3785596A	1974-01-15	CHINCHESTER MILES I
A flying control system in a VTOL or V/STOL aircraft comprises a mechanical analoque ''model'' of the lift and propulsion plant of the aircraft. Vertically-disposed electromechanical transducers represent, respectively, the lift engines of the aircraft, each transducer being vertically extendible and also tiltable in the fore-and-aft direction and delivering two electrical output signals, indicating vertical extension and tilt respectively, to control respectively the throttle opening and thrust deflection of the respective engine. The transducers are actuated by a mechanical assembly that receives pilots'' command and autostabiliser inputs and is caused to ''''yaw'''', ''''roll'''' and ''''pitch'''' by movement of the rudder pedals and control column, and to translate vertically and horizontally fore-and-aft by movements of a lift control lever.
23	Mechanical stability augmentation system	US3534930D	1969-02-24	US3534930A	1970-10-20	GARREN JOHN F JR; KELLY JAMES R

24	Valve control apparatus	US3505817D	1968-03-21	US3505817A	1970-04-14	CANTWELL HUGH FRANCIS

25	Variable diameter propellers	US3501248D	1968-05-14	US3501248A	1970-03-17	BROCKER FRIEDRICH W

26	Inflatable structures	US3494380D	1966-07-27	US3494380A	1970-02-10	MARTIN ERWIN HERBERT ERHARD

27	Aircraft closure flaps	US74608868	1968-07-19	US3486721A	1969-12-30	MYCZINSKI ALFRED

28	Helicopter having in horizontal flight the characteristics of an airplane	US61714167	1967-02-20	US3420472A	1969-01-07	BOUDES JACQUES

29	Coupling device for v. t. o. l. aircraft	US55556466	1966-06-06	US3393882A	1968-07-23	JEAN SOULEZ-LARIVIERE; RENE PHILIPPOT

30	Thermal gas flow comparator	US42804565	1965-01-26	US3374676A	1968-03-26	CLAUDE BRENOT

31	Valve devices	US37554464	1964-06-16	US3365165A	1968-01-23	MARIE GIRE ETIENNE YVES JEAN
998,417. Valves. SOC. NATIONALE D'ETUDE ET DE CONSTRUCTION MOTORS D'AVIATION. April 4, 1962 [April 7, 1961], No. 13012/62. Heading F2V. [Also in Division B7] Means for distributing fluid between a plurality of receiving apparatuses, such as altitude control nozzles on an aircraft, comprises a plurality of pipes in parallel between a valve and each apparatus, the valve comprising ganged obturators so that in one valve position, flow is divided equally between the apparatuses, in another position flow is to one apparatus only, and in intermediate positions flow is apportioned between the apparatuses, at least one obturator providing an unobstructed flow passage. In Fig. 1, a valve body 1a contains a part cylindrical member with parts 6, 7, of cross-sections which are unequal arcs as seen in Fig. 2. These parts are secured to an endplate 9 rotatable by a servomotor 11 to control the admission of pressure fluid, received through duct 1, to ducts 2, 3 leading to one apparatus and ducts 4, 5, leading to another. In all positions, the fluid consumption is constant. Fig. 5 shows cross-section of a valve in which two parts 6 and two parts 7, all of differing angular extents, control admission to ducts 2, 3, 21, 31, leading to one set of jet reaction nozzles, and to ducts 4, 5, 41, 51, leading to another set.
32	Control systems	US47752965	1965-08-05	US3330477A	1967-07-11	STEPHENS ARTHUR V

33	Flight control arrangement	US35079964	1964-03-10	US3272459A	1966-09-13	GERO MADELUNG; LEONHARD BRAUER; BENEDIKT EMMERICH

34	Attitude control system for an aeronautical propeller	US28090263	1963-05-16	US3261406A	1966-07-19	GOODMAN ROBERT B; FISCHER RICHARD L

35	Control apparatus for vertical take-off aircraft	US39854664	1964-09-23	US3259343A	1966-07-05	ROPPEL CLARENCE L

36	Thrust means for powering aircraft	US31350363	1963-10-03	US3212735A	1965-10-19	NIKOLAUS LAING

37	Pivotal shock absorbing pad assembly	US41694164	1964-12-08	US3208707A	1965-09-28	BLUMRICH JOSEF F

38	Control system for vtol vehicles	US15028861	1961-11-06	US3205728A	1965-09-14	MORRIS WILLIS B; IVAN SAWOROTNOW

39	Signal mixing system for servo actuators	US25296563	1963-01-21	US3204893A	1965-09-07	SHEAR JR HERBERT J; ROHRS HENRY E A

40	Automatic transition-control device for v.t.o.l. aircraft	US18047762	1962-03-19	US3193218A	1965-07-06	GONTIER ERNST ADOLPHE OTTON; JOSEPH JARDINIER JEAN PAUL; JANOS RONA

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