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B64C31/024： ..带有辅助动力装置的

序号	专利名	申请号	申请日	公开（公告）号	公开（公告）日	发明人
41	FLEXIBLE AIRFOILS AND METHOD	US10869106	2004-06-15	US20050274847A1	2005-12-15	Richard Charron
An airfoil for use in kites, movable wing aircraft and fixed wing aircraft has a straight spar inserted into a sleeve in the arcuate leading edge of a flexible wing panel. The resultant forces on the spar dynamically shape the airfoil. The airfoil is reinforced by battens between the leading edge and the trailing edge of the wing panel. Flight control is maintained through control lines warping the airfoil.
42	FLIER STRUCTURE	US09985196	2001-11-02	US20020130217A1	2002-09-19	Ming-Ta Wei
A flier structure including a fuselage extending from front side to rear side and a weight body connected with front end of the fuselage. A port wing and a starboard wing respectively leftward and rightward extend from the fuselage. A left tailfin and a right tailfin respectively extend from rear sides of the port wing and starboard wing. The bottoms of front edges of the port wing and starboard wing are respectively connected with a left and a right flow deflecting wings. The rear sides of the left and right flow deflecting wings are respectively spaced from the port wing and starboard wing by a predetermined distance. The left and right flow deflecting wings are respectively connected with the left and right sides of the fuselage. The disconnected portions between the left flow deflecting wing and port wing and the right flow deflecting wing and starboard wing respectively form two flow deflecting spaces.
43	Aircraft structure for take-off and landing on a pilot's feet	US6489	1987-01-23	US4773619A	1988-09-27	Erno Rubik
The invention relates to an aircraft structure to make possible take-off and landing on a pilot's feet. The aircraft structure according to the invention can be regarded as a category between kite-shaped aircraft structures and light structures. The gist of the aircraft structure of the invention consists in providing freely supported or outerly reinforced wings (12) adapted to be moved by a pilot (15) actuated mechanism, in their own plane during flight.
44	Thermal navigator	US557745	1983-12-02	US4591111A	1986-05-27	Joseph S. Laughter
An apparatus for use in an ultralight aircraft, glider, or sailplane to detect and navigate within thermal updrafts is disclosed. The apparatus includes a right temperature sensor and a left temperature sensor mounted on the wings of the aircraft. A difference circuit and difference indicator measure and indicate whether the right or left sensor is warmer and indicate a measured temperature difference. A derivative circuit and derivative indicator measure and indicate whether the air temperature is increasing or decreasing and indicate a rate of temperature change. The derivative circuit may be responsive to any of the right temperature sensor, the left temperature sensor, both the right and left temperature sensors, or to a third temperature sensor mounted on the aircraft. The apparatus detects thermal updrafts and indicates to the pilot when and how rapidly to turn to obtain the maximum lift from the thermal updraft.
45	Wind-powered flying boat	US652386	1976-01-26	US3987982A	1976-10-26	James L. Amick
A water-based sailing vehicle that is able to accelerate from rest under wind power, become airborne, and fly above the water. At low speeds, the vehicle performs as a displacement sailboat. At higher speeds, the weight of the vehicle is supported by a combination of hydrodynamic lift from the planing hull and aerodynamic lift from the wings, or by aerodynamic lift alone. The wings are set at a large dihedral angle, so that with one wing-tip float immersed, the horizontal wing provides a lifting force, while the raised wing provides a horizontal side force for sailing, plus some additional lift. The wings and tail have airplane-type control surfaces which give complete control both in the sailing mode and in free flight.
46	Self-launching glider	US437187	1974-01-28	US3966143A	1976-06-29	Gordon R. Smith
An aircraft of variable geometry and certain unique features which allow its operation along the surface of water, ice or the ground under sail power provided by tilting the wings up into a cross-wind to attain sufficient speed to be self launched into gliding flight in two modes -- while close to the surface in wind shear, circling and climbing in a regenerative flight path powered by changes in wind speed with altitude until sufficient altitude is attained to soar on rising air currents.
47	Integral control system for sailplanes	US3801045D	1972-06-29	US3801045A	1974-04-02	JONES E
An internal control system is provided for sailplanes for dynamic soaring. This system permits coordinated movement between any two of three elements, namely the wing, elevator, and control stick, independent of the third, and provides a means of aileron control on a pivotable wing without externally exposed wires or struts to create drag. Any change of pitch of the wing is countered by a change of pitch of the elevator without changing the position of the control stick. If the wing is held fixed, for example, in landing, the stick will move the elevator. If the elevator is held fixed or becomes jammed, the control stick can be used to change the pitch of the wing to maintain control. This coordinated movement is made possible by differential linkages provided in the controls.
48	Swept wing variable pitch sailplane	US3561702D	1968-11-01	US3561702A	1971-02-09	JONES EDWARD B
A sailplane is provided in which the line-of-lift of the wing is swept back from the longitudinal elastic axis to give an automatic wing twist with change of lifting force. In operation, a reduction in the angle of incidence from an updraught wind results in a trade of lift for greater forward thrust. An increase in angle of incidence from a downdraught wind results in a trade of forward momentum for greater lift. This is most effective under turbulent air conditions.
49	Wing structure	US30299263	1963-08-19	US3174711A	1965-03-23	SULLIVAN MATTHEW A

50	Flying machine	US58069331	1931-12-12	US1912775A	1933-06-06	KOCH ERICH E

51	Glider aeroplane	US67203323	1923-11-01	US1565953A	1925-12-15	JEAN PONSOLLE; MARCEL VERGNOU

52	Glider	US63829123	1923-05-11	US1492262A	1924-04-29	LOUIS PEYRET

53	Aeroplane.	US1908455435	1908-09-30	US924833A	1909-06-15	ROGERS JAMES HARRIS

54	Aeroplane.	US1905257403	1905-04-26	US831173A	1906-09-18	MONTGOMERY JOHN J

55	Means for aerial flight	US582757D		US582757A	1897-05-18

56	Teeeitoey	US376937D		US376937A	1888-01-24

57	무인 글라이더를 활용한 해양 탄성파 굴절법 탐사 시스템 및 방법	KR1020160182531	2016-12-29	KR101766916B1	2017-08-11	김영준; 구남형; 정순홍; 천종화; 이호영; 김정기; 황규덕
본발명은해양탄성파탐사방법중 글라이더에수진기를장착하여굴절파를취득하는글라이더를활용한해양탄성파굴절법탐사시스템및 방법에관한것으로서, 음향을발생시키는음원을탑재한탐사선; 및해상에표류하거나수중에서동작하며상기탐사선에매달려이동하거나, 원격조정에의해양력과회전력을발생시켜원하는위치로이동가능하며상기탐사선에서발생된상기음원이굴절된탄성파를수신하는수진기를구비하며상기탄성파를기록하는글라이더;를포함하여구성되어,해양무인관측시스템인글라이더에하이드로폰및 스트리머그리고이를기록할수 있는기록시스템을탑재하여해양탄성파굴절법탐사에활용하려는것으로서, 이를통하여탄성파굴절법자료를취득할수 있는효과가있다.
58	낙하산 구명 장비	KR1020090051224	2009-06-08	KR1020090131247A	2009-12-28	김영천
PURPOSE: A parachute life equipment is provided to help a user escape from a building safely as soon as possible upon firing. CONSTITUTION: A parachute life equipment includes a para-glider(10) into which the air is injected, a life guarding kit(20) into which the air is injected, a rope(30) which connects the para-glider with the life guarding kit, and a control knob(28) which controls the rope. The para-glider includes a thick and wide space part(11), a thin and narrow space part(12) formed in the outer side of the wide space part, and an air duct(13) integrally formed on the para glider.
59	학습용 모형 비행기의 앞날개 고정장치	KR2020070005597	2007-04-05	KR200441150Y1	2008-07-29	이훈상
본 고안은 학습용 모형비행기의 앞날개 고정장치에 관한 것으로서, 모형 비행기 동체의 상면에 고무줄로 묶어 앞날개를 지지하는 앞날개 지지대를 구비한 학습용 모형비행기의 앞날개 고정장치에 있어서, 상기 앞날개 지지대(50)는 그 전방 및 후방측에 각각 1차 상반각(α)이 형성된 제1 알루미늄관(3)이 삽입되도록 형성된 홀(51)과, 상기 제1 알루미늄관(3)의 양측에 각각 삽입된 직댓살(4)을 고무밴드(6)로 함께 묶어 1차 상반각(α)을 유지하는 앞, 뒤댓살고정부재(60, 70)가 각각 삽입되도록 상기 양측 홀(51)의 내측에는 각각수평으로 형성된 앞, 뒤사각장공(52, 53)을 포함하여 구성된 것을 특징으로 한다. 이와 같이 구성된 본 고안은 직댓살(4)이 1차 상반각(α)이 형성된 앞, 뒤댓살고정부재(60, 70)와 같이 묶어짐으로써, 직댓살(4)이 각각 형성하는 1차 상반각(α)이 좌우 대칭으로 형성되어 앞날개의 앞부분과 뒤부분이 서로 수평을 이루게 되고, 상기 앞, 뒤댓살고정부재(60, 70)가 수평으로 형성된 앞, 뒤사각장공(52, 53)에 각각 삽입되어 직댓살(4)을 고정하므로, 바람의 영향으로 직댓살(4)이 이루는 1차 상반각(α)이 틀어지지 않게 되어 모형 비행기가 좌우 및 전방으로 급강하하는 현상이 발생하지 않게 되는 효과가 있다.
60	Single Use Logistic Glider	US15715016	2017-09-25	US20180086449A1	2018-03-29	Martinus M. Sarigul-Klijn; Maurice P. Gionfriddo; Nesrin Sarigul-Klijn
A disposable airdropped glider. The glider body is constructed from precut panels cut from (MDO) or (HDO) plywood and assembled with pocket-screw joinery or piano hinges. A skid board forms a landing surface and a cargo deck roll-off surface. The glider has pivoting wings and struts. The glider has a triple-tail, a flat nose and honeycomb paperboard panels between the nose and the cargo. Wings are pivoted from a position overlying the fuselage to a flying position by gas springs in wing spars which are compressed by a chain attached to the fuselage through a rotating bracket such that the gas springs are compressed when the wings are folded. The airfoils are plastic extrusions with openings that hold the wing spars and co-formed jury spars which attach the upper and lower surface of the wing. A parachute uses a part of the tail structure to form a deployment drogue.

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